[{"section":"Page","title":"About AANTC","url":"/","summary":"","meta":"","search_text":"about aantc centre center mission hkust","order":0,"static_url":"/"},{"section":"Page","title":"Research","url":"/research/all/","summary":"","meta":"","search_text":"research aerodynamics aeroacoustics low-altitude aircraft sports aerodynamics performance","order":1,"static_url":"/research/all/"},{"section":"Page","title":"Low noise UAM in modern cities","url":"/research/low-altitude-air-mobility/","summary":"","meta":"","search_text":"low noise uam in modern cities urban air mobility uam drones environmental noise acoustic measurement computational fluid dynamics rotor noise source imaging bvi route planning","order":2,"static_url":"/research/low-altitude-air-mobility/"},{"section":"Page","title":"Facilities & software","url":"/facility/all/","summary":"","meta":"","search_text":"facilities & software experimental facilities measurement platforms computational methods","order":3,"static_url":"/facility/all/"},{"section":"Page","title":"Team","url":"/team/","summary":"","meta":"","search_text":"team faculty research assistants fellows students alumni","order":4,"static_url":"/team/"},{"section":"Page","title":"Publications","url":"/publications/all/","summary":"","meta":"","search_text":"publications journal articles conference papers book chapters","order":5,"static_url":"/publications/all/"},{"section":"Page","title":"News","url":"/post/all/","summary":"","meta":"","search_text":"news research activity project visits collaborations","order":6,"static_url":"/post/all/"},{"section":"Page","title":"Opportunities","url":"/career/all/","summary":"","meta":"","search_text":"opportunities academic research professional vacancies careers","order":7,"static_url":"/career/all/"},{"section":"Page","title":"Contact AANTC","url":"/contact/","summary":"","meta":"","search_text":"contact aantc address visit hkust map","order":8,"static_url":"/contact/"},{"section":"Page","title":"Privacy","url":"/privacy/","summary":"","meta":"","search_text":"privacy privacy cookies local storage analytics personal data","order":9,"static_url":"/privacy/"},{"section":"Page","title":"Accessibility","url":"/accessibility/","summary":"","meta":"","search_text":"accessibility accessibility keyboard screen reader zoom reduced motion","order":10,"static_url":"/accessibility/"},{"section":"Research","title":"Contra-rotating rotor PIV measurements","url":"/research/62/","summary":"Contra-rotating rotors in advanced unmanned aerial vehicles (UAVs) can offer enhanced aerodynamic performance and pose significant aeroacoustics challenges. This study experimentally investigates the far-field noise characteristics and flow-field of a 21.8 cm diameter contra-rot…","meta":"Aeroacoustics","search_text":"contra-rotating rotor piv measurements contra-rotating rotors in advanced unmanned aerial vehicles (uavs) can offer enhanced aerodynamic performance and pose significant aeroacoustics challenges. this study experimentally investigates the far-field noise characteristics and flow-field of a 21.8 cm diameter contra-rotating rotors system during axial descent with the effects of varying rotational speeds (60–100 rps) and descent rates (vd from 0 m/s to 12 m/s). experimental results show that the contra-rotating rotor noise increase slightly at low descent rates, decrease sharply at descent ratio vd/vh around 1.8 (vd/vh is defined as descent speed divided by induced speed while hovering), and rise again when vd/vh>2. directivity results exhibit a dipole characteristic. tonal noise i aeroacoustics contra-rotating rotors in advanced unmanned aerial vehicles (uavs) can offer enhanced aerodynamic performance and pose significant aeroacoustics challenges. this study experimentally investigates the far-field noise characteristics and flow-field of a 21.8 cm diameter contra-rotating rotors system during axial descent with the effects of varying rotational speeds (60–100 rps) and descent rates (vd from 0 m/s to 12 m/s). experimental results show that the contra-rotating rotor noise increase slightly at low descent rates, decrease sharply at descent ratio vd/vh around 1.8 (vd/vh is defined as descent speed divided by induced speed while hovering), and rise again when vd/vh>2. directivity results exhibit a dipole characteristic. tonal noise i cheng cao, zhida ma, xiangtian li, wangqiao chen, peng zhou and xin zhang","order":11,"static_url":"/research/62/"},{"section":"Research","title":"An experimental study of rotor aeroacoustics with aeroelastic effects under edgewise flight conditions","url":"/research/61/","summary":"Rotor blades in eVTOL aircraft are often assumed rigid in noise studies, but their thin, slender design makes them prone to large aeroelastic deformations during edgewise forward flight. Measurements in an anechoic wind tunnel showed that a thin-root variant (lower flapwise stif…","meta":"Aeroacoustics","search_text":"an experimental study of rotor aeroacoustics with aeroelastic effects under edgewise flight conditions rotor blades in evtol aircraft are often assumed rigid in noise studies, but their thin, slender design makes them prone to large aeroelastic deformations during edgewise forward flight. measurements in an anechoic wind tunnel showed that a thin-root variant (lower flapwise stiffness) of a 229 mm baseline rotor experiences significantly greater time-varying deformations, resulting in a reduced broadband noise compared to the baseline. wavelet-based beamforming confirmed the advancing blade as the dominant noise source, with the broadband reduction linked to weakened blade-vortex interactions, improving understanding of how blade flexibility affects evtol rotor acoustics. aeroacoustics rotors are the primary noise contributors in evtol aircraft. investigations into rotor noise problems often assume that rotor blades are rigid, neglecting their aeroelastic effects. however, rotor blades are typically designed to be thin and slender for improved aerodynamic efficiency. this makes them highly susceptible to aeroelastic deformations, especially during edgewise forward flight. in this work, we investigate the aerodynamic and aeroacoustic performance of a baseline rotor with a diameter of 229 mm and its thin-root variant, which has significantly lower flapwise stiffness. the measurements were conducted in an anechoic wind tunnel under edgewise forward flight conditions. first, deformation measurements reveal that the thin-root rotor experiences significantly larger time varying deformations. then, acoustic measurements indicate that the thin-root rotor produces a higher blade-passing frequency (bpf) tone and a lower broadband noise level compared with the baseline. next, results from a wavelet-based beamforming method show that the advancing blade is the primary noise source, with the reduction in broadband noise attributed to weakened blade-vortex interaction (bvi). these findings enhance our understanding of the impact of rotor blade deformation on evtol rotor acoustics. zhenjun peng, wangqiao chen, bao chen, puyuan wang, peng zhou, xin zhang contours of axial deflection for the thin-root rotor and the baseline rotor at tilt angles phase-averaged acoustic imaging results from t = 0.2t to t = 0.3t. phase-averaged acoustic imaging results from t = 0.2t to t = 0.4t.","order":12,"static_url":"/research/61/"},{"section":"Research","title":"Windsurfing CFD","url":"/research/54/","summary":"AANTC has developed an efficient computational fluid dynamics (CFD) platform for sports aerodynamics research, including windsurfing. The windsurfing project focuses on the equipment that will be used for the 2024 Olympics. The specificity of this new windsurfing equipment is th…","meta":"Sports Aerodynamics","search_text":"windsurfing cfd aantc has developed an efficient computational fluid dynamics (cfd) platform for sports aerodynamics research, including windsurfing. the windsurfing project focuses on the equipment that will be used for the 2024 olympics. the specificity of this new windsurfing equipment is that the submerged hydrofoil provides vertical lift and allows the windsurfer and the board to lift above the water surface and hence attain faster speeds. the robust large-scale simulations evaluate both the aerodynamic and hydrodynamic performances of the sail, athlete, and hydrofoil. sports aerodynamics aantc has developed an efficient computational fluid dynamics (cfd) platform for sports aerodynamics research, including windsurfing. the windsurfing project focuses on the equipment that will be used for the 2024 olympics. the specificity of this new windsurfing equipment is that the submerged hydrofoil provides vertical lift and allows the windsurfer and the board to lift above the water surface and hence attain faster speeds. the robust large-scale simulations evaluate both the aerodynamic and hydrodynamic performances of the sail, athlete, and hydrofoil. the simulations have the capabilities and specifications of: ─ simulation of sail motion; ─ high-quality dynamically deforming mesh; ─ two-phase flow simulation for the sail and the hydrofoil; ─ advanced simulation and post-processing schemes;","order":13,"static_url":"/research/54/"},{"section":"Research","title":"Low-noise UAM planning in the community","url":"/research/59/","summary":"Drones are promising transport means for the last-mile deliveries in urban communities. However, low-altitude aviation can cause severe noise pollution, leading to the requirement of rational operational strategies to minimize noise emissions. In this work, the noise impact on a…","meta":"Aeroacoustics","search_text":"low-noise uam planning in the community drones are promising transport means for the last-mile deliveries in urban communities. however, low-altitude aviation can cause severe noise pollution, leading to the requirement of rational operational strategies to minimize noise emissions. in this work, the noise impact on an urban community of delivery drones is assessed using a virtual flight platform that contains noise generation and projection modules. both the tonal and broadband noise components are taken into account via analytical and semi-empirical prediction methods, and the noise propagation in the urban environment is computed by an efficient gaussian beam tracing method. aeroacoustics drones are promising transport means for the last-mile deliveries in urban communities. however, low-altitude aviation can cause severe noise pollution, leading to the requirement of rational operational strategies to minimize noise emissions. in this work, the noise impact on an urban community of delivery drones is assessed using a virtual flight platform that contains noise generation and projection modules. both the tonal and broadband noise components are taken into account via analytical and semi-empirical prediction methods, and the noise propagation in the urban environment is computed by an efficient gaussian beam tracing method.","order":14,"static_url":"/research/59/"},{"section":"Research","title":"Acoustic liners for modern aero-engine noise reduction","url":"/research/58/","summary":"Attenuating the low-frequency component of aero-engine noise is challenging due to the mass and volume constraints when applying conventional noise mitigation techniques using liners and foams. To address it, acoustic liners constructed by Helmholtz resonators with extended neck…","meta":"Acoustic materials","search_text":"acoustic liners for modern aero-engine noise reduction attenuating the low-frequency component of aero-engine noise is challenging due to the mass and volume constraints when applying conventional noise mitigation techniques using liners and foams. to address it, acoustic liners constructed by helmholtz resonators with extended necks (hrens) are developed. an analytical noise reduction model of this kind of liners are established through combining the equivalent medium model and the transfer matrix method, based on which inhomogeneous liners design methodology for maximizing the attenuation capability was developed. to investigate the aerodynamic and aeroacoustic performance of the liners subjected to high-intensity incidence, an advanced grazing flow tube was built up with the incident spl acoustic materials attenuating the low-frequency component of aero-engine noise is challenging due to the mass and volume constraints when applying conventional noise mitigation techniques using liners and foams. to address it, acoustic liners constructed by helmholtz resonators with extended necks (hrens) are developed. an analytical noise reduction model of this kind of liners are established through combining the equivalent medium model and the transfer matrix method, based on which inhomogeneous liners design methodology for maximizing the attenuation capability was developed. to investigate the aerodynamic and aeroacoustic performance of the liners subjected to high-intensity incidence, an advanced grazing flow tube was built up with the incident spl","order":15,"static_url":"/research/58/"},{"section":"Research","title":"Acoustic meta-surface development","url":"/research/57/","summary":"A series of acoustic metasurfaces with periodic structures are proposed using porous materials including meta-based fibrous materials and polymer foam to refract an incidence wave in an anomalous yet controllable way.","meta":"Acoustic materials","search_text":"acoustic meta-surface development a series of acoustic metasurfaces with periodic structures are proposed using porous materials including meta-based fibrous materials and polymer foam to refract an incidence wave in an anomalous yet controllable way. acoustic materials a series of acoustic metasurfaces with periodic structures are proposed using porous materials including meta-based fibrous materials and polymer foam to refract an incidence wave in an anomalous yet controllable way. in one period, there are several elements responding to incident wave differently. through carefully designing the individual elements, the reflected or refracted waves can be manipulated. the anomalous behaviours are predicted theoretically and validated by numerical simulations and laboratory tests. based on the capability of wave manipulation, the acoustic energy can be prevented from radiating into the far field, resulting in effective noise control. considering aeroacoustic applications, e.g. acoustic liners in engines, the studies on the effects of grazing-incidence acoustic waves and flow on the metasurfaces are being implemented.","order":16,"static_url":"/research/57/"},{"section":"Research","title":"Computational Aerodynamics of Cyclists","url":"/research/56/","summary":"This research combines numerical simulation with controlled wind-tunnel measurements to investigate cycling aerodynamics. The computational work resolves flow structures around cyclist-bicycle configurations and examines how posture, crosswinds, wheel design and cyclist spacing …","meta":"Sports Aerodynamics","search_text":"computational aerodynamics of cyclists this research combines numerical simulation with controlled wind-tunnel measurements to investigate cycling aerodynamics. the computational work resolves flow structures around cyclist-bicycle configurations and examines how posture, crosswinds, wheel design and cyclist spacing affect aerodynamic forces and wake behaviour. the results support the interpretation of experiments and the aerodynamic assessment of cycling equipment and race configurations. sports aerodynamics aantc uses computational fluid dynamics to study airflow around cyclists, bicycles and cycling equipment. numerical flow fields reveal wake development and aerodynamic interactions associated with riding posture, leg position, wheel configuration and the relative position of cyclists. computational models provide three-dimensional descriptions of the flow around cyclist-bicycle systems. the simulations identify flow separation, vortical structures and wake development around the rider and bicycle, giving physical context to measured forces. related studies address complete cyclist geometries, individual wheel configurations and aerodynamic interactions between cyclists. wind-tunnel measurements provide an experimental reference for selected numerical studies. published work compares computed and measured aerodynamic forces, and uses wake measurements to examine the corresponding flow structures. particle image velocimetry provides an additional comparison for studies of cycling-wheel wakes. together, these methods connect computed flow fields with measurable aerodynamic behaviour and support the careful assessment of posture, equipment and race configurations.","order":17,"static_url":"/research/56/"},{"section":"Research","title":"High-accuracy wind tunnel test","url":"/research/55/","summary":"The cycling aerodynamic test rig was designed and built in 2018. It incorporates the knowledge and experience of more than twenty years’ R&D effort in aerospace engineering and racing car engineering, led by Prof. Xin Zhang. The test rig is used to measure the aerodynamic forces…","meta":"Sports Aerodynamics","search_text":"high-accuracy wind tunnel test the cycling aerodynamic test rig was designed and built in 2018. it incorporates the knowledge and experience of more than twenty years’ r&d effort in aerospace engineering and racing car engineering, led by prof. xin zhang. the test rig is used to measure the aerodynamic forces acting on a cyclist in the wind. a custom-built, high-accuracy balance is used to withstand the large unsteady pedalling force exerted by the athlete and resolve small changes in aerodynamic forces. the test rig has been used to evaluate cycling equipment and athlete performance. in addition, by combining with the cycling mannequin developed by the team in 2019, new cycling skinsuits and equipment were evaluated using the test rig. sports aerodynamics the cycling aerodynamic test rig was designed and built in 2018. it incorporates the knowledge and experience of more than twenty years’ r&d effort in aerospace engineering and racing car engineering, led by prof. xin zhang. the test rig is used to measure the aerodynamic forces acting on a cyclist in the wind. a custom-built, high-accuracy balance is used to withstand the large unsteady pedalling force exerted by the athlete and resolve small changes in aerodynamic forces. the test rig has been used to evaluate cycling equipment and athlete performance. in addition, by combining with the cycling mannequin developed by the team in 2019, new cycling skinsuits and equipment were evaluated using the test rig. the rig has the following capability: ─ six-component high-accuracy balance; ─ instrumentation for rotational torque measurement; ─ low-interference aero bike supporting struts; ─ suitable for both athlete and cycling equipment tests; ─ embedded turbo trainer for realistic test condition.","order":18,"static_url":"/research/55/"},{"section":"Research","title":"Aerodynamic design of sports equipment","url":"/research/53/","summary":"The CFD simulation platform and the wind tunnel test rig are seamlessly integrated for equipment development, following established procedures in aerospace engineering and racing car engineering. The automated CFD platform is used to run a multitude of simulations, between which…","meta":"Sports Aerodynamics","search_text":"aerodynamic design of sports equipment the cfd simulation platform and the wind tunnel test rig are seamlessly integrated for equipment development, following established procedures in aerospace engineering and racing car engineering. the automated cfd platform is used to run a multitude of simulations, between which the geometry of the cycling is modified for aerodynamic improvement. prototypes are then fabricated and tested in the wind tunnel. design iterations are conducted to provide incremental gains of the aerodynamic performance while satisfying structural requirements. sports aerodynamics the cfd simulation platform and the wind tunnel test rig are seamlessly integrated for equipment development, following established procedures in aerospace engineering and racing car engineering. the automated cfd platform is used to run a multitude of simulations, between which the geometry of the cycling is modified for aerodynamic improvement. prototypes are then fabricated and tested in the wind tunnel. design iterations are conducted to provide incremental gains of the aerodynamic performance while satisfying structural requirements.","order":19,"static_url":"/research/53/"},{"section":"Research","title":"Owl inspired material for trailing edge noise control","url":"/research/25/","summary":"Owls are known as silent predators of the night. Compared to other famous raptors such as falcons and kestrels, owls are not fast at all. Instead, after millions of evolution, owls have special adaptations which enable them to approach to their prey with little noise. In particu…","meta":"Aeroacoustics","search_text":"owl inspired material for trailing edge noise control owls are known as silent predators of the night. compared to other famous raptors such as falcons and kestrels, owls are not fast at all. instead, after millions of evolution, owls have special adaptations which enable them to approach to their prey with little noise. in particular, owls’ feathers have three unique features: leading edge serrations, trailing edge fringes, as well as the hairy dorsal surface. the function of the last feature is not well understood, and no related application is known. aeroacoustics the evolution in the past millions of years enables owls to reduce their flight noise efficiently, especially in the high-frequency range, where their preys are most sensitive. owls’ feathers have three unique features: leading edge serrations, trailing edge fringes, as well as the hairy dorsal surface. in this research, artificial hairy structures are fabricated to resemble owls' downy feather. these structures are attached to a flat plate test model to study there effect on trailing edge noise. the hairy coating can significantly reduce the high-frequency noise generated at the trailing edge. a theoretical model was developed to predict the noise radiation with the turbulence information obtained by the wake measurement using the hot-wire. peng zhou and gonam lui the microstructure of the velvet structure on an eagle owl's primary feather. setup of the acoustic measurement in the anechoic wind tunnel. comparison of the third-octave acoustic images of the clean and hairy flat plate models.","order":20,"static_url":"/research/25/"},{"section":"Research","title":"Sliding grid simulation of cascade noise","url":"/research/30/","summary":"Turbofan engines are commonly used on modern commercial aircrafts and have become a significant source of noise pollution. The tonal noise generated by turbofan engines has been extensively studied, and noise reduction approaches such as acoustic liners have been developed. The …","meta":"Aeroacoustics","search_text":"sliding grid simulation of cascade noise turbofan engines are commonly used on modern commercial aircrafts and have become a significant source of noise pollution. the tonal noise generated by turbofan engines has been extensively studied, and noise reduction approaches such as acoustic liners have been developed. the dominant source of broadband noise is due to the turbulent fan-wake interacting with the leading edges of the outlet guide vanes (ogv) aeroacoustics the rotational motion of the fan blades was considered, by applying a high-order hybrid sliding interface between the turbulence injection region and the ogvs. the effect of the advance ratio and turbulence properties of the fanwakes, such as the wake width and turbulent integral length scale, on the sound power level, were investigated. the sound power level obtained are compared to analytical predictions. the wake rotation speed has no significant effect on the noise generated by the cascade, due to the similar levels of averaged turbulence intensity across each case. this will remain true, as long as the separation between adjacent wakes is a constant. the changes in the wake width have a significant influence on the upstream and downstream sound power levels. wider wakes tend to increase the pwl at low frequencies and decrease the levels at high frequencies. similar effects were observed for the downstream pwl spectra. wei ying, ryu fattah","order":21,"static_url":"/research/30/"},{"section":"Research","title":"Rotor aeroacoustics","url":"/research/49/","summary":"Systematic rotor noise study is conducted in AANTC including analytical measurement, numerical simulation and experimental measurements. Theoretical noise prediction models are developed to compute the noise radiation from propellers at different working conditions. Recently, th…","meta":"Aeroacoustics","search_text":"rotor aeroacoustics systematic rotor noise study is conducted in aantc including analytical measurement, numerical simulation and experimental measurements. theoretical noise prediction models are developed to compute the noise radiation from propellers at different working conditions. recently, the effects of unsteady motions and uncertainty factors are considered in the theoretical model. aeroacoustics systematic rotor noise study is conducted in aantc including analytical measurement, numerical simulation and experimental measurements. theoretical noise prediction models are developed to compute the noise radiation from propellers at different working conditions. recently, the effects of unsteady motions and uncertainty factors are considered in the theoretical model. the numerical simulation is mainly based on the acoustic-wave preserved artificial compressibility method to compute the sound generation in different working conditions. the study leads to low-noise blade designs. the experimental study is based on the anechoic facilities in the group. the effects of blade geometry, low-noise treatment and wind conditions are systematic different rotors are designed in aantc, and the aerodynamic and aeroacoustic performances are measured. some data study are available for academic purposes upon reasonable request.","order":22,"static_url":"/research/49/"},{"section":"Research","title":"Drone noise measurements","url":"/research/50/","summary":"The noise radiation from unmanned aerial vehicles is measured in both anechoic chamber and outdoor environments. The effects of microphone arrangement, data processing method, requirements on whether condition, flight accuracy are studied. The effect of the working different wor…","meta":"Aeroacoustics","search_text":"drone noise measurements the noise radiation from unmanned aerial vehicles is measured in both anechoic chamber and outdoor environments. the effects of microphone arrangement, data processing method, requirements on whether condition, flight accuracy are studied. the effect of the working different working conditions, and weight and the imbalance are measured. the noise sources and the directivity patterns are measured. the outcome of the measurement partly supports the development of iso standard on noise assessment led by the research group. aeroacoustics the noise radiation from unmanned aerial vehicles is measured in both anechoic chamber and outdoor environments. the effects of microphone arrangement, data processing method, requirements on whether condition, flight accuracy are studied. the effect of the working different working conditions, and weight and the imbalance are measured. the noise sources and the directivity patterns are measured. the outcome of the measurement partly supports the development of iso standard on noise assessment led by the research group. the outcome of the measurement partly supports the development of iso standard on noise assessment led by the research group.","order":23,"static_url":"/research/50/"},{"section":"Research","title":"Bluff-body aerodynamic drag and noise reduction","url":"/research/51/","summary":"Aerodynamic and aeroacoustic characteristics of a cylinder with longitudinal grooves were studied in an anechoic wind tunnel, emphasizing on drag and noise attenuation. The parallel mounted load cells and a single microphone measured the aerodynamic resistance and noise of a cir…","meta":"Sports Aerodynamics","search_text":"bluff-body aerodynamic drag and noise reduction aerodynamic and aeroacoustic characteristics of a cylinder with longitudinal grooves were studied in an anechoic wind tunnel, emphasizing on drag and noise attenuation. the parallel mounted load cells and a single microphone measured the aerodynamic resistance and noise of a circular cylinder with longitudinal grooves at reynolds number ranging from 5.84 × 10^4 to 8.48 × 10^4, covering the flow regimes from the sub-critical to the post-critical states. the results show that longitudinal grooves can effectively trigger the boundary-layer transition started at a reynolds number around 5.84 × 10^4, causing the so-called drag crisis. during the transition process, a drag reduction over 50% and a maximum noise attenuation over 15 db can be achieved sports aerodynamics aerodynamic and aeroacoustic characteristics of a cylinder with longitudinal grooves were studied in an anechoic wind tunnel, emphasizing on drag and noise attenuation. the parallel mounted load cells and a single microphone measured the aerodynamic resistance and noise of a circular cylinder with longitudinal grooves at reynolds number ranging from 5.84 × 10^4 to 8.48 × 10^4, covering the flow regimes from the sub-critical to the post-critical states. the results show that longitudinal grooves can effectively trigger the boundary-layer transition started at a reynolds number around 5.84 × 10^4, causing the so-called drag crisis. during the transition process, a drag reduction over 50% and a maximum noise attenuation over 15 db can be achieved","order":24,"static_url":"/research/51/"},{"section":"Research","title":"Aeroacoustics of obstructions in turbulent boundary layers","url":"/research/52/","summary":"The aerodynamic noise generated by a two-dimensional large obstacle in a turbulent boundary layer. The obstacles have different shape and height emerged in the turbulent boundary layer of the flat plate. The spectra of turbulence and sound in a wide velocity range of 20-50m/s wa…","meta":"Aeroacoustics","search_text":"aeroacoustics of obstructions in turbulent boundary layers the aerodynamic noise generated by a two-dimensional large obstacle in a turbulent boundary layer. the obstacles have different shape and height emerged in the turbulent boundary layer of the flat plate. the spectra of turbulence and sound in a wide velocity range of 20-50m/s was tested. scaling laws of the turbulence and acoustic results are conducted, and the noise generation mechanisms are analysed. aeroacoustics the aerodynamic noise generated by a two-dimensional large obstacle in a turbulent boundary layer. the obstacles have different shape and height emerged in the turbulent boundary layer of the flat plate. the spectra of turbulence and sound in a wide velocity range of 20-50m/s was tested. scaling laws of the turbulence and acoustic results are conducted, and the noise generation mechanisms are analysed.","order":25,"static_url":"/research/52/"},{"section":"Research","title":"Sound Extrapolation Method for Turbulent Flows","url":"/research/26/","summary":"In aeroacoustics, the far-field directivity is often computed using the integral solution of the acoustic analogy equations. The sound prediction can be rendered when the turbulent eddies move across the integration surface, and the expensive volume integral terms are neglected.","meta":"Aeroacoustics","search_text":"sound extrapolation method for turbulent flows in aeroacoustics, the far-field directivity is often computed using the integral solution of the acoustic analogy equations. the sound prediction can be rendered when the turbulent eddies move across the integration surface, and the expensive volume integral terms are neglected. aeroacoustics in computational aeroacoustics (caa), the acoustic directivity patterns using the so-called hybrid methods. the near-field fluid/acoustic field is resolved using the high-accuracy numerical simulations while the sound extrapolation methods (or sometimes it is called sound projection methods) to account for the sound radiation processes. usually, the integral solution of the well-known ffowcs-williams and hawkings (fw-h) equation (proc. r. soc. a., vol. 264, no. 1151, p. 321-342, 1969), which is one of the most important equations in the subject of aeroacoustics, is often employed for the hybrid computation. it is an exact rearrangement of the fluid governing equations, and it could provide the exact acoustic solution in case that the equation is exactly solved. however, in practical applications, the volume integral term is often omitted to save the computational expense and to avoid the difficulty of “cause-and-effect” issue (that unknowns appear in the source terms). one consequence of neglecting the volume terms is that the predicted sound field can be contaminated when the permeable integration surface is located in the turbulent flows. there were fw-h equation-based methods such as using on-body or open integration surfaces, which, however, have limitations in certain circumstances. at aantc, a series of studies were conducted to propose new sound projection methods that are suitable for turbulent flow applications. the key idea of the trend of studies is to filter out the non-acoustic (or acoustically inefficient) components in the turbulent flows before the various are employed for acoustic far-field computation. the idea is based on our understanding of that the turbulent flow fluctuations can be decomposed into the acoustical, vortical and entropy components (kovasznay, j. aero. sci., vol. 20, no. 1 the initial study focused on filtering out the vortical components by developing a variant of the lighthill’s acoustic analogy (proc. r. soc. a., vol. 211, p. 546-578, 1952), in which the mean flow is considered, and the fluctuations are defined based on the local mean flow components. in the source term, divergence and convection operators are acting on the velocity components such that the vortical velocities are filtered out. the method is suitable for the turbulent flow dominated by the vortical components, and it was applied to the airfoil-gust interaction problems, in both subsonic and transonic flows [1]. siyang zhong","order":26,"static_url":"/research/26/"},{"section":"Research","title":"Aircraft airframe noise: Aerodynamics and aeroacoustics of a flap side-edge","url":"/research/44/","summary":"An experimental and computational investigation was carried out to determine the aerodynamics and aeroacoustics of a flap side-edge.","meta":"Aeroacoustics","search_text":"aircraft airframe noise: aerodynamics and aeroacoustics of a flap side-edge an experimental and computational investigation was carried out to determine the aerodynamics and aeroacoustics of a flap side-edge. aeroacoustics an experimental and computational investigation was carried out to determine the aerodynamics and aeroacoustics of a flap side-edge. a porous side-edge treatment was applied to the flap side-edge in an attempt to reduce airframe noise. the application of a porous flap side-edge had two favourable effects. firstly, it reduced the magnitude of vorticity in the turbulent shear layer and the vortex. this reduced the magnitude of the hydrodynamic instabilities induced by the flap side-edge vortex. secondly, it displaced the vortex further away from the flap surface due to the finite mass flux allowed through the porous material. this reduced the magnitude of the disturbances that interacted with the solid flap surface by moving them further away. this research was focused on understanding noise generation mechanisms associated with the flowfield around a flap-side edge and their reduction. previous investigations identified a noise reduction of up to 4 db in the far-field, within a limited band of frequencies, by replacing part of a flap side-edge with an open cell porous material. the physics responsible for this were not discussed. this work employed a variety of experimental and numerical techniques to understand the physics responsible for noise production at the flap side-edge and the mechanism by which a porous material applied to the flap side-edge reduced the noise.","order":27,"static_url":"/research/44/"},{"section":"Research","title":"Variable impedance liners for aero-engines","url":"/research/29/","summary":"Acoustic liners application within the nacelle walls is a well established passive noise damping technique in modern turbofan engine. Improved acoustic liners should be developed to improve the maximum noise attenuation induced by acoustic liners and broaden the attenuation freq…","meta":"Aeroacoustics","search_text":"variable impedance liners for aero-engines acoustic liners application within the nacelle walls is a well established passive noise damping technique in modern turbofan engine. improved acoustic liners should be developed to improve the maximum noise attenuation induced by acoustic liners and broaden the attenuation frequency range by using non-uniform acoustic liners. aeroacoustics the high bypass ratio of modern turbofan engine results in that the tonal noise decrease while the broadband noise is becoming a more and more important contributor in engine noise. thus improved acoustic liners should be develop to: 1. improve the maximum noise attenuation induced by acoustic liners. 2. broaden the attenuation frequency range by using non-uniform acoustic liners. engine intake noise radiation: in the m24n1 case study with no acoustic liner treatment, the bulk of the acoustic energy is concentrated towards the upper wall. as the wave propagates across the inlet there is no change in the acoustic wavelength. however, the wave is diffracted by duct lip. non-uniform liner distribution: the possibility of reducing radiated noise by varying the liner properties along the duct in both axial and circumferential directions was investigated. a serrated joint liner distribution was proposed jingwen guo and ryu fattah pressure contour of a lined intake duct for m24n1 directivity comparison of rigid wall and","order":28,"static_url":"/research/29/"},{"section":"Research","title":"Racing car aerodynamics: Aerodynamics of oscillating wings","url":"/research/33/","summary":"Wings in pitching motion can reach very large incidences, often overshooting the static stall angle. In those cases, the unsteady motion can be beneficial to the aerodynamic performance of the wing.","meta":"Sports Aerodynamics","search_text":"racing car aerodynamics: aerodynamics of oscillating wings wings in pitching motion can reach very large incidences, often overshooting the static stall angle. in those cases, the unsteady motion can be beneficial to the aerodynamic performance of the wing. sports aerodynamics wings in pitching motion can reach very large incidences, often overshooting the static stall angle. in those cases, the unsteady motion can be beneficial to the aerodynamic performance of the wing. lift can be enhanced and stall can be delayed to higher angles of attack. that process is known as dynamic stall. the dynamic stall process is not limited to an overshoot of lift at incidences above the static stall angle. exceeding that angle results in a leading edge vortex being formed (dynamic stall vortex) and convected downstream. the vortex induces an even lower pressure region on the suction surface, further increasing the lift but also creating a large pitching-down moment and increased drag. once the dynamic stall vortex is shed into t","order":29,"static_url":"/research/33/"},{"section":"Research","title":"Racing car aerodynamics: Aerodynamic interaction between a wing and wheels","url":"/research/34/","summary":"What is the influence of an upstream-mounted wing on the aerodynamic characteristics of a wheel and vice versa? How does the aerodynamic interaction between these components of the configuration depend on vertical, streamwise and spanwise position variations of the wing relative…","meta":"Sports Aerodynamics","search_text":"racing car aerodynamics: aerodynamic interaction between a wing and wheels what is the influence of an upstream-mounted wing on the aerodynamic characteristics of a wheel and vice versa? how does the aerodynamic interaction between these components of the configuration depend on vertical, streamwise and spanwise position variations of the wing relative to the wheel? which flow mechanisms and phenomena cause the observed behaviour and what would be the main factors of influence for these physics? would it be possible to reproduce the qualitative (flow features and phenomena) and quantitative (correlation with experimental results) aspects of wing-wheel interaction with the use of current, 'state-of-the-art' cfd simulations? sports aerodynamics what is the influence of an upstream-mounted wing on the aerodynamic characteristics of a wheel and vice versa? how does the aerodynamic interaction between these components of the configuration depend on vertical, streamwise and spanwise position variations of the wing relative to the wheel? which flow mechanisms and phenomena cause the observed behaviour and what would be the main factors of influence for these physics? would it be possible to reproduce the qualitative (flow features and phenomena) and quantitative (correlation with experimental results) aspects of wing-wheel interaction with the use of current, 'state-of-the-art' cfd simulations?","order":30,"static_url":"/research/34/"},{"section":"Research","title":"Racing car aerodynamics: Wheel aerodynamics","url":"/research/35/","summary":"Forty percent of the total drag on a Formula 1 car comes from the wheels. Wheels have an influence on the aerodynamics of the car as a whole, the front and rear wings, the under-body and the diffuser. The wheels are a source of noise above 40 miles per hour and they are the domi…","meta":"Sports Aerodynamics","search_text":"racing car aerodynamics: wheel aerodynamics forty percent of the total drag on a formula 1 car comes from the wheels. wheels have an influence on the aerodynamics of the car as a whole, the front and rear wings, the under-body and the diffuser. the wheels are a source of noise above 40 miles per hour and they are the dominant source of road vehicles. sports aerodynamics forty percent of the total drag on a formula 1 car comes from the wheels. wheels have an influence on the aerodynamics of the car as a whole, the front and rear wings, the under-body and the diffuser. the wheels are a source of noise above 40 miles per hour and they are the dominant source of road vehicles.","order":31,"static_url":"/research/35/"},{"section":"Research","title":"Racing car aerodynamics: Large-scale source term modelling of vortex generation","url":"/research/36/","summary":"For efficiency/affordability, the wind tunnel testing is expensive and comprehensive testing is impractical. Computational fluid dynamics (CFD) is useful while adapting grids are difficult and time consuming. In this case we do not mesh the vortex generating device but model its…","meta":"Sports Aerodynamics","search_text":"racing car aerodynamics: large-scale source term modelling of vortex generation for efficiency/affordability, the wind tunnel testing is expensive and comprehensive testing is impractical. computational fluid dynamics (cfd) is useful while adapting grids are difficult and time consuming. in this case we do not mesh the vortex generating device but model its effects via source terms (body forces) as an easy optimisation. sports aerodynamics for efficiency/affordability, the wind tunnel testing is expensive and comprehensive testing is impractical. computational fluid dynamics (cfd) is useful while adapting grids are difficult and time consuming. in this case we do not mesh the vortex generating device but model its effects via source terms (body forces) as an easy optimisation.","order":32,"static_url":"/research/36/"},{"section":"Research","title":"Aircraft airframe noise: Computational aeroacoustics of bogie noise","url":"/research/37/","summary":"Airframe noise is one of the main noise sources during the approach phase. Flight tests have shown that for large aircraft the main landing gear (MLG) is a dominant airframe noise source . The design of landing gear is primarily focussed on its mechanical function, which results…","meta":"Aeroacoustics","search_text":"aircraft airframe noise: computational aeroacoustics of bogie noise airframe noise is one of the main noise sources during the approach phase. flight tests have shown that for large aircraft the main landing gear (mlg) is a dominant airframe noise source . the design of landing gear is primarily focussed on its mechanical function, which results in a shape that is not very aerodynamic. this creates a lot of separated and turbulent flow and thus a lot of aeroacoustic noise. wind tunnel tests have revealed that the bogie beam as one of the most important noise sources of the main landing gear. the main objective of the project is to investigate the influence of bogie beam inclination angle on the flow field around the main landing gear and the noise generated by this flow. aeroacoustics airframe noise is one of the main noise sources during the approach phase. flight tests have shown that for large aircraft the main landing gear (mlg) is a dominant airframe noise source . the design of landing gear is primarily focussed on its mechanical function, which results in a shape that is not very aerodynamic. this creates a lot of separated and turbulent flow and thus a lot of aeroacoustic noise. wind tunnel tests have revealed that the bogie beam as one of the most important noise sources of the main landing gear. the main objective of the project is to investigate the influence of bogie beam inclination angle on the flow field around the main landing gear and the noise generated by this flow.","order":33,"static_url":"/research/37/"},{"section":"Research","title":"Aircraft airframe noise: Effect of bogie inclination on the unsteady flow field and noise production","url":"/research/38/","summary":"Computational methods are used to determine the flow field around a simplified landing gear geometry and the far field noise levels generated by this flow. The focus of this research is on the influence of bogie inclination angle on the flow features and the far field noise leve…","meta":"Aeroacoustics","search_text":"aircraft airframe noise: effect of bogie inclination on the unsteady flow field and noise production computational methods are used to determine the flow field around a simplified landing gear geometry and the far field noise levels generated by this flow. the focus of this research is on the influence of bogie inclination angle on the flow features and the far field noise levels. a high quality hybrid grid of eight million cells was generated around a simplified main landing gear geometry. a structured grid consisting of 5.5 million cells are applied to regions near the geometry where complex flow features are expected. aeroacoustics computational methods are used to determine the flow field around a simplified landing gear geometry and the far field noise levels generated by this flow. the focus of this research is on the influence of bogie inclination angle on the flow features and the far field noise levels. a high quality hybrid grid of eight million cells was generated around a simplified main landing gear geometry. a structured grid consisting of 5.5 million cells are applied to regions near the geometry where complex flow features are expected. the unstructured grid of 2.5 million cells are applied to extend the domain so that appropriate boundary conditions to be applied. a hybrid grid provides a high resolution of the flow features near the bluff body geometry, and minimizes the cell count required to extend the domain to the outer edges where free stream boundary conditions can be applied.","order":34,"static_url":"/research/38/"},{"section":"Research","title":"Aircraft airframe noise: Noise control of landing gear using perforated fairings","url":"/research/39/","summary":"Landing gear noise can be the dominant component of airframe noise, especially for larger aircraft. The interaction of the airflow with protrusions and cavities gives rise to unsteady flow phenomena constituting a potent sound generating mechanism. Shielding landing gear compone…","meta":"Aeroacoustics","search_text":"aircraft airframe noise: noise control of landing gear using perforated fairings landing gear noise can be the dominant component of airframe noise, especially for larger aircraft. the interaction of the airflow with protrusions and cavities gives rise to unsteady flow phenomena constituting a potent sound generating mechanism. shielding landing gear components with fairings and thereby preventing this interaction has been considered before. high speed flow deflection onto other components and fairing self-noise are disadvantages of these fairings. bleeding air through the fairings by making them porous can reduce the impact of these effects and result in a noise reduction. aeroacoustics landing gear noise can be the dominant component of airframe noise, especially for larger aircraft. the interaction of the airflow with protrusions and cavities gives rise to unsteady flow phenomena constituting a potent sound generating mechanism. shielding landing gear components with fairings and thereby preventing this interaction has been considered before. high speed flow deflection onto other components and fairing self-noise are disadvantages of these fairings. bleeding air through the fairings by making them porous can reduce the impact of these effects and result in a noise reduction.","order":35,"static_url":"/research/39/"},{"section":"Research","title":"Aircraft airframe noise: Large-eddy simulation of jet interaction with a wing","url":"/research/40/","summary":"Jet engines and airframes are the two main contributors to aircraft noise, with the latter including both high-lift devices and landing gears. To achieve reductions in aircraft noise, it is necessary to reduce the noise from all components that contribute significantly to the to…","meta":"Aeroacoustics","search_text":"aircraft airframe noise: large-eddy simulation of jet interaction with a wing jet engines and airframes are the two main contributors to aircraft noise, with the latter including both high-lift devices and landing gears. to achieve reductions in aircraft noise, it is necessary to reduce the noise from all components that contribute significantly to the total noise and noise due to the interactions between components. aeroacoustics jet engines and airframes are the two main contributors to aircraft noise, with the latter including both high-lift devices and landing gears. to achieve reductions in aircraft noise, it is necessary to reduce the noise from all components that contribute significantly to the total noise and noise due to the interactions between components. noise generation by the vortical flow from jet engine interacting with airframe structures, such as high-left devices when the wing is at landing configuration with flap deployed, is a fundamental problem affecting the design and performance of an aircraft and its system. understanding of the installation effect would help to design more efficient and more environmentally friendly aircraft. the main objectives for this study were to: 1. investigate aerodynamic noise due to the interaction of the vortical flow from a jet engine with high-lift devices; 2. perform les for the turbulent flow around wings, with and without the influence from the jet. understand flow physics and noise generation mechanisms for the phenomenon of jet wing interaction; 3. investigate the radiated noise to far field due to jet-wing interaction using the fw-h method for sound wave propagation, to compare predicted far veld noise with experimental data.","order":36,"static_url":"/research/40/"},{"section":"Research","title":"Aircraft airframe noise: Slat noise attenuation with acoustic liner treatment","url":"/research/41/","summary":"The significant contribution of the flows around the leading edge slat on the wing of a commercial aircraft to the airframe noise during approach and landing motivates this research project to identify the mechanisms of leading edge slat noise and passively control these acousti…","meta":"Aeroacoustics","search_text":"aircraft airframe noise: slat noise attenuation with acoustic liner treatment the significant contribution of the flows around the leading edge slat on the wing of a commercial aircraft to the airframe noise during approach and landing motivates this research project to identify the mechanisms of leading edge slat noise and passively control these acoustic sources. aeroacoustics the significant contribution of the flows around the leading edge slat on the wing of a commercial aircraft to the airframe noise during approach and landing motivates this research project to identify the mechanisms of leading edge slat noise and passively control these acoustic sources. several flow phenomena take place due to the separated flow in the slat cove region and its interaction with the surrounding flow such as, low-speed recirculation flow, free shear layer, and ejections of large-scale structures merging with the slat wake. other important phenomena can also exist, such as, the interaction of the slat wake with the wing boundary layer, referred to as the confluent boundary layer, and slat trailing edge vortex shedding. all of these may cause the noise generation. to understand the physics and mechanisms behind these phenomena and to find a way to reduce the slat noise, accurate simulations of the complex unsteadiness flow of the high-lift wing are needed. to develop and apply computational aeroacoustic methods using the sotoncaa code to reveal the mechanism of the slat noise generation and demonstrate the feasibility of controlling the slat noise using acoustic liners.","order":37,"static_url":"/research/41/"},{"section":"Research","title":"Aircraft airframe noise: Investigation of aircraft noise in steep approach","url":"/research/42/","summary":"Airframe noise has been found to be the dominant source of noise for an aircraft on approach to landing. Airframe noise is made up of the HLD noise and landing gear noise. In order to reduce noise on the ground steep approach landing procedures can be used.","meta":"Aeroacoustics","search_text":"aircraft airframe noise: investigation of aircraft noise in steep approach airframe noise has been found to be the dominant source of noise for an aircraft on approach to landing. airframe noise is made up of the hld noise and landing gear noise. in order to reduce noise on the ground steep approach landing procedures can be used. aeroacoustics airframe noise has been found to be the dominant source of noise for an aircraft on approach to landing. airframe noise is made up of the hld noise and landing gear noise. in order to reduce noise on the ground steep approach landing procedures can be used. figure 1 shows a typical steep approach trajectory. steep approach utilises a steeper glide slope than the conventional -3 deg glide slope. as a result the aircraft flies at a higher altitudes over residential areas close to the airport. increasing distance to the ground reduces the noise on the ground significantly according to the inverse square law. in order to meet the decent velocity requirement for landing, spoilers are used as air brakes to slow down the aircraft. the aim is to understand the underlying flow dynamics of noise generation on a hld with deflected spoilers in steep approach landing configuration. based on the results we aim to develop noise reduction techniques that can be applied to the hld configuration to reduce the noise impact due to deflected spoilers. a high-order time accurate aeroacoustics code sotoncaa is being used to perform the simulations.","order":38,"static_url":"/research/42/"},{"section":"Research","title":"Aircraft airframe noise: Blowing for bluff-body noise control","url":"/research/43/","summary":"Landing gear noise is a major contributor to airframe noise. Wakes from upstream components impinging on downstream components are a significant source of noise. This work investigates the use of flow control to reduce the noise generated by bluff bodies.","meta":"Aeroacoustics","search_text":"aircraft airframe noise: blowing for bluff-body noise control landing gear noise is a major contributor to airframe noise. wakes from upstream components impinging on downstream components are a significant source of noise. this work investigates the use of flow control to reduce the noise generated by bluff bodies. aeroacoustics landing gear noise is a major contributor to airframe noise. wakes from upstream components impinging on downstream components are a significant source of noise. this work investigates the use of flow control to reduce the noise generated by bluff bodies. after the bluff body demonstration case the flow control was applied to an aircraft main landing gear. the aim of this work was to assess and develop local blowing flow control methods for bluff body noise reduction. the first demonstration case was on isolated components, i.e., a cylinder and an h-beam. a tandem configuration of an h-beam and a cylinder was used to investigate interaction noise between two bluff bodies. for the isolated components a pneumatic split plate was investigated. a small jet was applied on the rearward face 180 deg. from the stagnation line of two bluff bodies to provide an analogous reduction in bluff body noise to that achieved with a physical split plate. for the interaction case the flow control was applied to the cylinder to break down the large flow structures and to displace the peak turbulence away from the surface of the downstream component.","order":39,"static_url":"/research/43/"},{"section":"Research","title":"Aircraft Engine Studies: Modelling next generation CROR aircraft","url":"/research/45/","summary":"Contra-rotating open rotors (CRORs) show promise for use in future aircraft propulsion systems, but suffer from high noise emissions. Both tonal and broadband noise emissions are produced by CRORs.","meta":"Aeroacoustics","search_text":"aircraft engine studies: modelling next generation cror aircraft contra-rotating open rotors (crors) show promise for use in future aircraft propulsion systems, but suffer from high noise emissions. both tonal and broadband noise emissions are produced by crors. aeroacoustics contra-rotating open rotors (crors) show promise for use in future aircraft propulsion systems, but suffer from high noise emissions. both tonal and broadband noise emissions are produced by crors. historically, tonal noise has been more extensively studied because it was thought to be the dominant noise type. however, recent studies have shown that broadband noise is also significant. therefore, research is needed to better understand the generation of cror broadband noise. the project concentrates on two areas of cror broadband noise. firstly, analytic models are being developed to improve industrial modelling of the noise. secondly, the assumptions which are made in the analytic models are being tested with the use of high-order computational aeroacoustic (caa) methods.","order":40,"static_url":"/research/45/"},{"section":"Research","title":"Aircraft Engine Studies: Development of a whole-aircraft noise model","url":"/research/46/","summary":"We develop an advanced computer program to estimate aircraft noise, both far-field radiation and scattering on fuselage.","meta":"Aeroacoustics","search_text":"aircraft engine studies: development of a whole-aircraft noise model we develop an advanced computer program to estimate aircraft noise, both far-field radiation and scattering on fuselage. aeroacoustics we develop an advanced computer program to estimate aircraft noise, both far-field radiation and scattering on fuselage. the program can calculate noise scattering using workstation efficient and accurately. the code allows integration of different kinds of noise sources, such as, propeller noise, jet noise and airframe noise. the method is in frequency domain; but due to its short execution time, it has the potential to be applied for broadband noise. with its low computation costs and flexibility for integrating different noise sources, this model has the potential to be a useful engineering tool on noise analysis and relative design optimisation.","order":41,"static_url":"/research/46/"},{"section":"Research","title":"Aircraft Engine Studies: Efficient computation of sound radiation on adaptively refined mesh","url":"/research/47/","summary":"A new computational tool was developed to efficiently predict sound radiation with block-structured adaptive mesh refinement (AMR) algorithm.","meta":"Aeroacoustics","search_text":"aircraft engine studies: efficient computation of sound radiation on adaptively refined mesh a new computational tool was developed to efficiently predict sound radiation with block-structured adaptive mesh refinement (amr) algorithm. aeroacoustics a new computational tool was developed to efficiently predict sound radiation with block-structured adaptive mesh refinement (amr) algorithm. the basic idea was to use grids of fine resolution only for the area where sound propagates. as a result the required grid number is reduced and the computational efficiency can be increased. the work includes parallel implementation of the amr algorithm, a high-order solver, and linear models for acoustics. practical problems, such as spinning modal radiation from an aero engine duct, were studied with the tool. compared to the computation performed on a fixed mesh, the computational efficiency by the amr method is increased extensively while the accuracy of the solution is still maintained.","order":42,"static_url":"/research/47/"},{"section":"Research","title":"Aircraft Engine Studies: Modelling of aircraft sound propagation","url":"/research/48/","summary":"A suite of high-order, time-domain computational aeroacoustic programs have been developed to model sound propagation and radiation from airframe components and aero engine intake and bypass/exhaust ducts.","meta":"Aeroacoustics","search_text":"aircraft engine studies: modelling of aircraft sound propagation a suite of high-order, time-domain computational aeroacoustic programs have been developed to model sound propagation and radiation from airframe components and aero engine intake and bypass/exhaust ducts. aeroacoustics a suite of high-order, time-domain computational aeroacoustic programs have been developed to model sound propagation and radiation from airframe components and aero engine intake and bypass/exhaust ducts. the method is based on multi-block, structured grids and high-order compact schemes and is capable of modelling the effect of liner, bifurcation, etc. simulations have been performed of noise propagation/radiation problems associated with high lift devices (hlds), e.g. slats, flaps, spoilers, and both engine intake and bypass ducts. new features are being implemented including efficient computation of broadband noise content for engine applications. new formulations of linearised euler and acoustic perturbation equations are also being developed.","order":43,"static_url":"/research/48/"},{"section":"Research","title":"Stable time-domain LEE simulations","url":"/research/28/","summary":"Linearized Euler equations (LEE) are often used in a CAA simulation, with a strong mean-velocity gradient, numerical Kelvin-Helmholtz (K-H) instabilities may appear using the LEE. Vortical instabilities can grow exponentially and contaminate the solution.","meta":"Aeroacoustics","search_text":"stable time-domain lee simulations linearized euler equations (lee) are often used in a caa simulation, with a strong mean-velocity gradient, numerical kelvin-helmholtz (k-h) instabilities may appear using the lee. vortical instabilities can grow exponentially and contaminate the solution. aeroacoustics to developing new instability suppression methods and compare the accuracy and computation cost of the proposed methods with previous methods. in this case, a time-harmonic acoustic wave propagates across a 2- d domain, and the sound is refracted across a finite shear layer. the solution field obtained the lee is clearly contaminated by the numerical instability, while the proposed adt method can an untouched acoustic filed. in this case, a time-harmonic acoustic wave propagates across a 2- d domain, and the sound is refracted across a finite shear layer. comparing with the lee solution, where the k-h instabilities appears and large spurious wave can be observed, the proposed method can provide uncontaminated results in acoustics near field and far field. yuhao sun and ryu fattah","order":44,"static_url":"/research/28/"},{"section":"Research","title":"Anisotropic filter for synthetic turbulence","url":"/research/27/","summary":"A technique of synthetic turbulence is proposed by developing a general form of anisotropic filter, which can realize the desired velocity spectra of three-dimensional anisotropic turbulence. The anisotropic filter can be directly implemented instead of obtaining the non-Gaussia…","meta":"Aeroacoustics","search_text":"anisotropic filter for synthetic turbulence a technique of synthetic turbulence is proposed by developing a general form of anisotropic filter, which can realize the desired velocity spectra of three-dimensional anisotropic turbulence. the anisotropic filter can be directly implemented instead of obtaining the non-gaussian energy spectra through gaussian superposition, which is then combined with linearised euler equations to predict the leading edge noise. aeroacoustics to develop a new method of synthetic anisotropic turbulence by deriving a general form of anisotropic filter that generates the homogeneous anisotropic turbulence. to investigate the influence of anisotropy on turbulence-airfoil interaction noise by applying various stretching ratios. the effectiveness of pseudo three-dimensional anisotropic filter is verified by comparing with amiet’s analytical solution. the turbulent velocity field induced by the anisotropic filters can be regarded as the pseudo three-dimensional anisotropic turbulence, which will reproduce the major statistics of three-dimensional turbulence through an integral solution of the three-dimensional fw-h equation, the far-field spl spectra is obtained, which shows good agreement with the theoretical solution, to within 1.5 db accuracy. it can be concluded that doubling of the tangential turbulent length scale leads to 9 db increase in spl spectra, which is attributed to the octupling of one-dimensional energy in the transverse direction. zhen shen synthesized anisotropic and three-dimensional turbulence validation of the anisotropic filter using analytical solutions. validation of the anisotropic filter using analytical solutions.","order":45,"static_url":"/research/27/"},{"section":"Research","title":"The Aeroacoustic Characteristics of a Heaving Airfoil","url":"/research/24/","summary":"Airfoil oscillation is a widely observed phenomenon in real applications, such as natural flyers, helicopter and drone blades, etc. This work studies the aeroacoustic characteristics of a heaving airfoil by experimental methods","meta":"Aeroacoustics","search_text":"the aeroacoustic characteristics of a heaving airfoil airfoil oscillation is a widely observed phenomenon in real applications, such as natural flyers, helicopter and drone blades, etc. this work studies the aeroacoustic characteristics of a heaving airfoil by experimental methods aeroacoustics airfoil oscillation is a widely observed phenomenon in real applications, such as natural flyers, helicopter and drone blades, etc. the instantaneous flow pattern on a pitching airfoil is acquired by a high-speed piv system. all measurements were conducted in the low-speed open-jet facility in the hong kong university of science and technology. the tunnel outlet has a dimension of 0.4m × 0.4m, and the largest wind speed of 70m/s. a straight wing model with the profile naca 0012 was tested, and it had a 100mm chord and 399mm span. the heaving motion was actuated by a voice coil motor. the far-field noise was measured by three microphones placed along an arc centered at the trailing edge of the airfoil a comparison of the noise spectra between the stationary and heaving cases at flow speeds of 10m/s and 40m/s are given in the figures below, respectively. the following observations can be obtained: 1. the heaving motion suppresses the height of the primary tone and enhances the secondary peaks 2. when the flow speed is 10m/s, a broadband hump in the vicinity to the primary tone raises due to the heaving motion. teng zhou and yuhao sun figure 1: the setup of the experiment. comparison of the time-frequency analysis between the static and heaving cases. : comparisons of the spectra obtained under the static and heaving conditions.","order":46,"static_url":"/research/24/"},{"section":"Research","title":"Non-Reflective Boundary Conditions for CAA","url":"/research/22/","summary":"Non-reflective boundary conditions are essential for accurate computational aeroacoustic (CAA) simulations. Benchmark test cases were developed to quantify the reflections generated by outgoing acoustic and vortical disturbances. These test cases were used to develop a new blend…","meta":"Aeroacoustics","search_text":"non-reflective boundary conditions for caa non-reflective boundary conditions are essential for accurate computational aeroacoustic (caa) simulations. benchmark test cases were developed to quantify the reflections generated by outgoing acoustic and vortical disturbances. these test cases were used to develop a new blended zonal characteristic boundary condition (cbc) with optimized parameters to maximise the solution accuracy. aeroacoustics a zonal characteristic boundary condition was developed from two benchmark test cases. the acoustic plane wave tests accurately quantify the reflections generated a boundary condition across a range of mach number, wave angle, and streamwise and transverse wave numbers. the other benchmark test case used synthetic turbulence to model the vorticity disturbances. several tests were conducted to evaluate the performance of various methods. the free parameters in the zonal characteristic method were optimized to minimize the acoustic reflections for both acoustic and vortical cases. the final result is a near-perfect non-reflective boundary condition. finally, the optimal methods from both benchmark cases were blended into a generalized formula a zonal characteristic boundary condition was developed from two benchmark test cases. the acoustic plane wave tests accurately quantify the reflections generated a boundary condition across a range of mach number, wave angle, and streamwise and transverse wave numbers. the other benchmark test case used synthetic turbulence to model the vorticity disturbances. several tests were conducted to evaluate the performance of various methods. the free parameters in the zonal characteristic method were optimized to minimize the acoustic reflections for both acoustic and vortical cases. the final result is a near-perfect non-reflective boundary condition. finally, the optimal methods from both benchmark cases were blended into a generalized formulation that automatically switches depending on the local vorticity magnitude. ryu fattah and james gill with non-reflective boundary conditions withoutr non-reflective boundary conditions incident plane wave","order":47,"static_url":"/research/22/"},{"section":"Facilities & software","title":"Multirotor hover noise calculator","url":"/tools/vtol-noise/","summary":"Estimate unweighted tonal, broadband and total hover OASPL directly below a multirotor aircraft, using geometry, mass, rotor thrust coefficient and solidity. Use known values or input ranges, and view total-level polar directivity. Available in English, Simplified Chinese and Tr…","meta":"Computational aeroacoustics and software","search_text":"multirotor hover noise calculator estimate unweighted tonal, broadband and total hover oaspl directly below a multirotor aircraft, using geometry, mass, rotor thrust coefficient and solidity. use known values or input ranges, and view total-level polar directivity. available in english, simplified chinese and traditional chinese. computational aeroacoustics and software","order":48,"static_url":"/tools/vtol-noise/"},{"section":"Facilities & software","title":"Navier-Stokes Solver","url":"/facility/32/","summary":"High-order CAA and low-order CFD codes are used by the research group to study the complex flow fields around streamlined and bluff bodies. The high-order solver employs the same numerical schemes and non-reflective boundary conditions that are used in the LEE and Euler solvers.…","meta":"Computational aeroacoustics and software","search_text":"navier-stokes solver high-order caa and low-order cfd codes are used by the research group to study the complex flow fields around streamlined and bluff bodies. the high-order solver employs the same numerical schemes and non-reflective boundary conditions that are used in the lee and euler solvers. a hybrid rans/les strategy is typically applied to complex geometries to resolve the wide range of flow structures that are critical to the radiated noise level. in some cases, we employ a low-order open-source cfd code, which was used to develop the video. in the video, the complex flow structures around an aircraft nose landing gear are illustrated. computational aeroacoustics and software","order":49,"static_url":"/facility/32/"},{"section":"Facilities & software","title":"Advanced synthetic turbulence methods","url":"/facility/31/","summary":"Synthetic turbulence methods are developed in AANTC to reproduce turbulence with specific turbulence spectra. A new method of synthetic anisotropic turbulence by deriving a general form of anisotropic filter that generates the homogeneous anisotropic turbulence. To investigate t…","meta":"Computational aeroacoustics and software","search_text":"advanced synthetic turbulence methods synthetic turbulence methods are developed in aantc to reproduce turbulence with specific turbulence spectra. a new method of synthetic anisotropic turbulence by deriving a general form of anisotropic filter that generates the homogeneous anisotropic turbulence. to investigate the influence of anisotropy on turbulence-airfoil interaction noise by applying various stretching ratios. ref. zhen shen, xin zhang, direct anisotropic filter method of generating synthetic turbulence applied to turbulence-airfoil interaction noise prediction, journal of sound and vibration, vol. 458, pp. 544-564, 2019. computational aeroacoustics and software","order":50,"static_url":"/facility/31/"},{"section":"Facilities & software","title":"Efficient boundary element method","url":"/facility/30/","summary":"An efficient boundary element method (BEM) solver has been developed at AANTC to compute the sound scattering from the objects, which can be acoustical hard or impedance walls. Reduced order modelling technologies are employed to improve the computational efficiency, and special…","meta":"Computational aeroacoustics and software","search_text":"efficient boundary element method an efficient boundary element method (bem) solver has been developed at aantc to compute the sound scattering from the objects, which can be acoustical hard or impedance walls. reduced order modelling technologies are employed to improve the computational efficiency, and special treatments are conducted to remove the unphysical instability modes. the solver has been applied to drone fuselage scattering and acoustic window performance estimation. ref. hanbo jiang, et al., boundary element analysis on fuselage scattering of drone noise, international journal of aeroacoustics, pp. 1-14, 2022. computational aeroacoustics and software","order":51,"static_url":"/facility/30/"},{"section":"Facilities & software","title":"Rotor noise prediction methods","url":"/facility/29/","summary":"A rotor noise prediction method based on the Hanson model was developed to compute the tonal noise of rotors. The effects of unsteady modes on the noise radiation are considered. Also, the broadband noise is computed using the empirical models of trailing edge noise. The rotatio…","meta":"Computational aeroacoustics and software","search_text":"rotor noise prediction methods a rotor noise prediction method based on the hanson model was developed to compute the tonal noise of rotors. the effects of unsteady modes on the noise radiation are considered. also, the broadband noise is computed using the empirical models of trailing edge noise. the rotation effects are accounted for in the prediction models. the aerodynamic variables are estimated using a cost-effective blade element and moment theory solver. the prediction results match well with the experiments. ref: siyang zhong, et al., a revisit of the tonal noise of small rotors, proceedings of the royal society a., vol. 476, pp. 20200491, 2020. computational aeroacoustics and software","order":52,"static_url":"/facility/29/"},{"section":"Facilities & software","title":"Acoustic preserved artificial compressibility (APAC) method","url":"/facility/28/","summary":"In AANTC, an acoustic preserved artificial compressibility method is developed to compute the sound generation and propagation at low Mach numbers. It can account for the compressibility, which is related to the sound generation process, at equivalent computational cost with the…","meta":"Computational aeroacoustics and software","search_text":"acoustic preserved artificial compressibility (apac) method in aantc, an acoustic preserved artificial compressibility method is developed to compute the sound generation and propagation at low mach numbers. it can account for the compressibility, which is related to the sound generation process, at equivalent computational cost with the incompressible solvers. it efficiently models the noise from rotors and flying vehicles. ref. hanbo jiang, xin zhang, “an acoustic-wave preserved artificial compressibility method for low-mach number aeroacoustic simulations”, journal of sound and vibration, vol. 516, 116505, 2022. computational aeroacoustics and software","order":53,"static_url":"/facility/28/"},{"section":"Facilities & software","title":"An environmental noise assessment code based on Gaussian beam tracing","url":"/facility/27/","summary":"An environmental noise assessment EnvARC is developed in AANTC to study the noise impact on the urban environment. It is based on a Gaussian beam tracing method. Different source models can be introduced as input, and the city model can be input from the geographic information s…","meta":"Computational aeroacoustics and software","search_text":"an environmental noise assessment code based on gaussian beam tracing an environmental noise assessment envarc is developed in aantc to study the noise impact on the urban environment. it is based on a gaussian beam tracing method. different source models can be introduced as input, and the city model can be input from the geographic information system. the effect of atmospheric condition and acoustic features on the geometric surface are introduced. ref. haoyu bian, et al., an efficient rectilinear gaussian beam tracing method for sound propagation modelling in a non-turbulent medium, journal of acoustical society of america, vol. 148, pp. 4037-4048, 2020. computational aeroacoustics and software","order":54,"static_url":"/facility/27/"},{"section":"Facilities & software","title":"Rotor noise test platform","url":"/facility/26/","summary":"A rotor aerodynamic and aeroacoustic measurement platform is developed in AANTC to study rotor aerodynamics and aeroacoustics. The rotor locations are accurately controlled by a high-resolution 2D transverse, and the 20 microphones are used to measure the noise properties. The a…","meta":"Experimental aerodynamics","search_text":"rotor noise test platform a rotor aerodynamic and aeroacoustic measurement platform is developed in aantc to study rotor aerodynamics and aeroacoustics. the rotor locations are accurately controlled by a high-resolution 2d transverse, and the 20 microphones are used to measure the noise properties. the aerodynamic forces are measured using high-accuracy load cells. ref: han wu et al., a rotor blade aeroacoustics test platform at hkust, internoise 2020, vol. 261, pp. 2476-2484, 2020. experimental aerodynamics","order":55,"static_url":"/facility/26/"},{"section":"Facilities & software","title":"Airfoil noise measurement platform","url":"/facility/25/","summary":"An airfoil noise measurement platform is developed in AANTC based on the anechoic wind tunnel. A microphone array with 56 microphone is used for sound source detection. The diameter is 0.7m and the frequency range is 50-10000 Hz. A laser profiler is used to measure the deformati…","meta":"Experimental aerodynamics","search_text":"airfoil noise measurement platform an airfoil noise measurement platform is developed in aantc based on the anechoic wind tunnel. a microphone array with 56 microphone is used for sound source detection. the diameter is 0.7m and the frequency range is 50-10000 hz. a laser profiler is used to measure the deformation of flexible airfoils. ref: peng zhou, siyang zhong, xin zhang, on the effect of velvet structures on trailing edge noise: experimental investigation and theoretical analysis, journal of fluid mechanics, vol. 919, a11, 2021 experimental aerodynamics","order":56,"static_url":"/facility/25/"},{"section":"Facilities & software","title":"Phased Microphone Array","url":"/facility/24/","summary":"Phased microphone array is used in AANTC to detect the aerodynamic sound sources. The array contains 56 Brüel & Kjær microphones and different beamforming algorithms are available for data processing.","meta":"Experimental aerodynamics","search_text":"phased microphone array phased microphone array is used in aantc to detect the aerodynamic sound sources. the array contains 56 brüel & kjær microphones and different beamforming algorithms are available for data processing. experimental aerodynamics","order":57,"static_url":"/facility/24/"},{"section":"Facilities & software","title":"Spinning mode duct test rig","url":"/facility/23/","summary":"A duct mode detection facility is developed in AANTC to evaluate the noise reduction in engine ducts. It is also used for duct mode detection method. The rig has a diameter of 200 mm, the flow speed is 10-60m/s, and the maximum working frequency is 8000 Hz. More details: H. Bu, …","meta":"Experimental aerodynamics","search_text":"spinning mode duct test rig a duct mode detection facility is developed in aantc to evaluate the noise reduction in engine ducts. it is also used for duct mode detection method. the rig has a diameter of 200 mm, the flow speed is 10-60m/s, and the maximum working frequency is 8000 hz. more details: h. bu, x. huang, x. zhang, an overview of testing methods for aeroengine fan noise, progress in aerospace sciences, vol. 124, 100722, 2021. experimental aerodynamics","order":58,"static_url":"/facility/23/"},{"section":"Facilities & software","title":"Impedance tubes","url":"/facility/22/","summary":"Different impedance tubes are used to measure the acoustic impedance of sound absorption materials. It can characterize the sound transmission loss and surface impedance as well. The working frequencies of the commercial Brüel & Kjær Type 4206 impedance tube are 50-1600 Hz (with…","meta":"Experimental aerodynamics","search_text":"impedance tubes different impedance tubes are used to measure the acoustic impedance of sound absorption materials. it can characterize the sound transmission loss and surface impedance as well. the working frequencies of the commercial brüel & kjær type 4206 impedance tube are 50-1600 hz (with diameter of 100 mm) and 500-6400 hz (with diameter of 29 mm), respectively. a fabricated impedance tube has square cross-section of 50x50 mm, and the working frequency range is 500-3430 hz. experimental aerodynamics","order":59,"static_url":"/facility/22/"},{"section":"Facilities & software","title":"Grazing flow tube","url":"/facility/21/","summary":"There are two flow tube facilities in AANTC to study the effects of grazing flows on acoustic liners. Impedance eduction methods are conducted for different types of sound absorption materials. The dimensions of tubes are 50x50 mm and the working frequency is 400-3400 Hz. The ma…","meta":"Experimental aerodynamics","search_text":"grazing flow tube there are two flow tube facilities in aantc to study the effects of grazing flows on acoustic liners. impedance eduction methods are conducted for different types of sound absorption materials. the dimensions of tubes are 50x50 mm and the working frequency is 400-3400 hz. the maximum mach and sound pressure levels for a are 0.1 and 120 db, respectively. the test rig is upgraded to enable wide test range. the mach number ad spl limits are 0.3 and 140 db, respectively. more details: wei yi, et al., acoustic impedance measurements using an advanced grazing flow tube facility, 28th international congress on sound and vibration, 2022. experimental aerodynamics grazing flow tube grazing flow tube","order":60,"static_url":"/facility/21/"},{"section":"Facilities & software","title":"Low Noise Low Speed Wind tunnel facility","url":"/facility/20/","summary":"The low-noise low-speed wind tunnel contains two test sections. Both sections have a cross-section of about 2.5 m wide and 2 m high and the test wind speed ranges from 15 m/s to 40 m/s. In aerodynamic test section, a model support is designed for studying the wind loading on air…","meta":"Experimental aerodynamics","search_text":"low noise low speed wind tunnel facility the low-noise low-speed wind tunnel contains two test sections. both sections have a cross-section of about 2.5 m wide and 2 m high and the test wind speed ranges from 15 m/s to 40 m/s. in aerodynamic test section, a model support is designed for studying the wind loading on aircraft model, uav, propeller model, etc. the support is capable of changing the pitch, yaw and roll angle of model. the flow at the aerodynamic test section is a uniform smooth flow with turbulence less than 0.12%. in structural/environmental test section, it is typically used for detailed model tests, such as high frequency force balance tests, pressure tests and pedestrian level wind environment. the test section has a fetch length of 6 m and is fitted with 93 computer controlled, pneumatically operated roughness elements that allow fine control of the simulated turbulence characteristics. more details: https://aaf.ust.hk/fac/1/ experimental aerodynamics","order":61,"static_url":"/facility/20/"},{"section":"Facilities & software","title":"Anechoic wind tunnel","url":"/facility/11/","summary":"he anechoic wind tunnel houses an open-jet inflow duct of 0.4m (W) by 0.4m(H), and an outlet that has a cross-section of 0.6m (W) by 0.6m (H). The test section is enclosed within an anechoic chamber that has dimensions of 3.3m(L) x 3.1m(W) x 2.0m(H). The wind tunnel speed ranges…","meta":"Experimental aerodynamics","search_text":"anechoic wind tunnel he anechoic wind tunnel houses an open-jet inflow duct of 0.4m (w) by 0.4m(h), and an outlet that has a cross-section of 0.6m (w) by 0.6m (h). the test section is enclosed within an anechoic chamber that has dimensions of 3.3m(l) x 3.1m(w) x 2.0m(h). the wind tunnel speed ranges from 10m/s to 70m/s. more details: yi et al., design and characterization of a multifunctional low-speed anechoic wind tunnel at hkust, aerospace science and technology, vol. 115, pp. 106814, 2021. experimental aerodynamics anechoic wind tunnel","order":62,"static_url":"/facility/11/"},{"section":"Facilities & software","title":"Linearised Euler solver","url":"/facility/15/","summary":"We use a high-order Linearised Euler Equation (LEE) solver to study specific aeroacoustic problems that are not governed by nonlinear and viscous effects. An LEE solver is significantly faster than a Navier-Stokes solver, and it has been used to understand how sound propagates i…","meta":"Computational aeroacoustics and software","search_text":"linearised euler solver we use a high-order linearised euler equation (lee) solver to study specific aeroacoustic problems that are not governed by nonlinear and viscous effects. an lee solver is significantly faster than a navier-stokes solver, and it has been used to understand how sound propagates in complex environments. in the video, the lee solver illustrates how sound generated inside an aircraft engine propagates towards the bypass outlet and scatters around the engine walls. high-order numerical schemes and non-reflective boundary conditions are applied to minimise the numerical error and to maximise the computational efficiency. computational aeroacoustics and software linearised euler solver","order":63,"static_url":"/facility/15/"},{"section":"Facilities & software","title":"Euler solver with shock capturing","url":"/facility/16/","summary":"We use a high-order Euler solver to study aeroacoustic problems that have nonlinear physics. In the video, the Euler solver shows what happens when a turbulent field impinges on the leading edge of a transonic aerofoil. This kind of problem is relevant for aircraft engine compon…","meta":"Computational aeroacoustics and software","search_text":"euler solver with shock capturing we use a high-order euler solver to study aeroacoustic problems that have nonlinear physics. in the video, the euler solver shows what happens when a turbulent field impinges on the leading edge of a transonic aerofoil. this kind of problem is relevant for aircraft engine components that operate at high speeds and that are subjected to oncoming flow disturbances. a shock-wave formed near the mid-chord of the aerofoil interacts strongly with the incoming turbulent field (shown in the bottom right corner of the video). the resulting noise radiated from the leading edge and the shock-wave is illustrated in the video. the solver employs high-order numerical schemes and non-reflective boundary conditions, together with a local artificial diffusivity model for the shock capturing. computational aeroacoustics and software euler solver with shock capturing","order":64,"static_url":"/facility/16/"},{"section":"Facilities & software","title":"2D Acoustic plane wave test rig","url":"/facility/12/","summary":"This facility was designed and fabricated at HKUST, and it is used to evaluate prototype acoustic materials. Test samples are sandwiched tightly between two paralleled Plexi glass plates (2.4 m x 1.2 m x 0.02 m), which provide a two-dimensional (2D) waveguide environment below 5…","meta":"Experimental aerodynamics","search_text":"2d acoustic plane wave test rig this facility was designed and fabricated at hkust, and it is used to evaluate prototype acoustic materials. test samples are sandwiched tightly between two paralleled plexi glass plates (2.4 m x 1.2 m x 0.02 m), which provide a two-dimensional (2d) waveguide environment below 5700 hz. foam wedges are applied along the sides of the test region to ensure an anechoic environment. the incident sound field is generated by an array of twenty pui audio as04008cor loud speakers, and it is measured by a g.r.a.s type 46be microphone. another g.r.a.s microphone is used to measure the transmitted/refracted sound field. the microphones are mounted onto a parker hannifin 2d traverse system which allows the entire incident and transmitted/refracted sound field to be studied. more details: yi fang et al, sound transmission through an acoustic porous metasurface with periodic structures, applied physics letter, vol. 110, 171904, 2017. experimental aerodynamics 2d acoustic plane wave test rig","order":65,"static_url":"/facility/12/"},{"section":"Facilities & software","title":"Large aerodynamic wind tunnel","url":"/facility/14/","summary":"WWTF's wind tunnel contains two test sections that are specifically designed for aerospace engineering and structural/environmental engineering. Both sections have a cross-section of about 2.5 m wide and 2 m high and the test wind speed ranges from 15 m/s to 40 m/s. In aerodynam…","meta":"Experimental aerodynamics","search_text":"large aerodynamic wind tunnel wwtf's wind tunnel contains two test sections that are specifically designed for aerospace engineering and structural/environmental engineering. both sections have a cross-section of about 2.5 m wide and 2 m high and the test wind speed ranges from 15 m/s to 40 m/s. in aerodynamic test section, a model support is designed for studying the wind loading on aircraft model, uav, propeller model, etc. the support is capable of changing the pitch, yaw and roll angle of model. the flow at the aerodynamic test section is a uniform smooth flow with turbulence less than 0.12%. in structural/environmental test section, it is typically used for detailed model tests, such as high frequency force balance tests, façade pressure tests and pedestrian level wind environment. the test section has a fetch length of 6 m and is fitted with 93 computer controlled, pneumatically operated roughness elements that allow fine control of the simulated turbulence characteristics. experimental aerodynamics large aerodynamic wind tunnel","order":66,"static_url":"/facility/14/"},{"section":"Facilities & software","title":"B&K Type 4206 Four-microphone Impedance Measurement Tube","url":"/facility/13/","summary":"This device is used to characterise the impedance and transmission loss properties of materials, in the frequency range of 50Hz-6.4kHz. Material samples with a diameter of 29mm and 100mm can be evaluated in the frequency range of 500Hz-6.4kHz and 50Hz-1.6kHz, respectively. The a…","meta":"Experimental aerodynamics","search_text":"b&k type 4206 four-microphone impedance measurement tube this device is used to characterise the impedance and transmission loss properties of materials, in the frequency range of 50hz-6.4khz. material samples with a diameter of 29mm and 100mm can be evaluated in the frequency range of 500hz-6.4khz and 50hz-1.6khz, respectively. the acoustic impedance and admittance are measured with this device. the sound absorption, reflection, and transmission loss coefficients are also obtained from this system. experimental aerodynamics four-microphone impedance measurement tube","order":67,"static_url":"/facility/13/"},{"section":"Facilities & software","title":"Performance Sports Test Rig","url":"/facility/18/","summary":"The experimental test is conducted in the wind tunnel in combination with the test rig. The wind tunnel is exclusively designed for speed racing purpose with low turbulence intensity and steady dynamic pressure. The test rig is a platform consists of 6-component balance, motor, …","meta":"Experimental aerodynamics","search_text":"performance sports test rig the experimental test is conducted in the wind tunnel in combination with the test rig. the wind tunnel is exclusively designed for speed racing purpose with low turbulence intensity and steady dynamic pressure. the test rig is a platform consists of 6-component balance, motor, cadence and torque sensor. the experiment facility can be applied in the measurement of full-scale cycling drag, the cloth drag test, yaw angle effect, etc. experimental aerodynamics performance sports test rig","order":68,"static_url":"/facility/18/"},{"section":"Facilities & software","title":"Sound extrapolation method for turbulent flows","url":"/facility/19/","summary":"In aeroacoustics, the far-field directivity is often computed using the integral solution of the acoustic analogy equations. The sound prediction prediction can be rendered when the turbulent eddies move across the integration surface, and the expensive volume integral terms are…","meta":"Computational aeroacoustics and software","search_text":"sound extrapolation method for turbulent flows in aeroacoustics, the far-field directivity is often computed using the integral solution of the acoustic analogy equations. the sound prediction prediction can be rendered when the turbulent eddies move across the integration surface, and the expensive volume integral terms are neglected. computational aeroacoustics and software sound extrapolation method for turbulent flows","order":69,"static_url":"/facility/19/"},{"section":"Facilities & software","title":"Acoustic Plane Wave Test Rig","url":"/facility/8/","summary":"This facility was designed and fabricated at HKUST, and it is used to evaluate prototype acoustic materials. Test samples are sandwiched tightly between two paralleled Plexi glass plates (2.4 m x 1.2 m x 0.02 m), which provide a two-dimensional (2D) waveguide environment below 5…","meta":"Experimental aerodynamics","search_text":"acoustic plane wave test rig this facility was designed and fabricated at hkust, and it is used to evaluate prototype acoustic materials. test samples are sandwiched tightly between two paralleled plexi glass plates (2.4 m x 1.2 m x 0.02 m), which provide a two-dimensional (2d) waveguide environment below 5700 hz. foam wedges are applied along the sides of the test region to ensure an anechoic environment. the incident sound field is generated by an array of twenty pui audio as04008cor loud speakers, and it is measured by a g.r.a.s type 46be microphone. another g.r.a.s microphone is used to measure the transmitted/refracted sound field. the microphones are mounted onto a parker hannifin 2d traverse system which allows the entire incident and transmitted/refracted sound field to be studied. experimental aerodynamics plane wave test rig","order":70,"static_url":"/facility/8/"},{"section":"Team","title":"Hongsen Bao","url":"/people/56/","summary":"Mr. Hongsen Bao obtained his Bachelor’s Degree in Physics from Xi’an Jiaotong University in 2014, and Master’s Degree in Mechanical Engineering from University of Michigan in 2016. He joined HKUST AANTC in 2022, and his current research focuses on sound propagation and ray acous…","meta":"PhD Candidate","search_text":"hongsen bao mr. hongsen bao obtained his bachelor’s degree in physics from xi’an jiaotong university in 2014, and master’s degree in mechanical engineering from university of michigan in 2016. he joined hkust aantc in 2022, and his current research focuses on sound propagation and ray acoustics. phd candidate mr. hongsen bao obtained his bachelor’s degree in physics from xi’an jiaotong university in 2014, and master’s degree in mechanical engineering from university of michigan in 2016. he joined hkust aantc in 2022, and his current research focuses on sound propagation and ray acoustics.","order":71,"static_url":"/people/56/"},{"section":"Team","title":"Celia Bertin","url":"/people/4/","summary":"CFD, CAD modelling, Experimental testing","meta":"Research Assistant in Aerodynamics and Performance Sports Engineering","search_text":"celia bertin cfd, cad modelling, experimental testing research assistant in aerodynamics and performance sports engineering miss celia bertin obtained her bachelor degree in mechanical engineering at the hong kong university of science and technology in june 2018. for her final year project, she led a team working on the design, manufacture, and development of a robotic five-axis additive manufacturing system. in september 2019, she graduated from the university of sheffield (united kingdom) with an msc in advanced mechanical engineering with first-class honours. during her research project entitled \"computational and experimental study of flow control methods applied to fixed-wing mavs\", she conducted multiple computational fluid dynamics 3d simulations to compare the aerodynamic effects of vortex generators and boundary layer suction devices on low aspect ratio wings at low reynolds numbers. the results were validated by wind tunnel experiments. in october 2019, she joined aantc as a research assistant in aerodynamics and performance sports engineering. at aantc, she is performing high-resolution cfd simulations to study the aerodynamics of drone propellers and fuselage interaction, as well as the aerodynamics and hydrodynamics in track cycling and windsurfing, working in collaboration with the hong kong olympic teams. cfd, cad modelling, experimental testing","order":72,"static_url":"/people/4/"},{"section":"Team","title":"Haoyu Bian","url":"/people/39/","summary":"","meta":"PhD in Mechanical Engineering, HKUST","search_text":"haoyu bian phd in mechanical engineering, hkust","order":73,"static_url":"/people/39/"},{"section":"Team","title":"Huanxian Bu","url":"/people/21/","summary":"Experimental aerodynamics and aeroacoustics, aero-engine fan noise testing, drone noise testing.","meta":"Associate Professor, Northwestern Polytechnical University","search_text":"huanxian bu experimental aerodynamics and aeroacoustics, aero-engine fan noise testing, drone noise testing. associate professor, northwestern polytechnical university dr. huanxian bu joined aantc in 2016 and obtained the phd degree in hong kong university of science and technology in 2020, after he got the bachelor's and master's degrees in nanjing university of aeronautics and astronautics. his research mainly focuses on experimental aerodynamics and aeroacoustics, including aeroengine fan noise testing, uav rotor noise testing, etc. experimental aerodynamics and aeroacoustics, aero-engine fan noise testing, drone noise testing.","order":74,"static_url":"/people/21/"},{"section":"Team","title":"Xiaoyi Cai","url":"/people/66/","summary":"","meta":"PhD Student","search_text":"xiaoyi cai phd student","order":75,"static_url":"/people/66/"},{"section":"Team","title":"Sinforiano Cantos","url":"/people/16/","summary":"Aeroacoustics, CFD, rotor acoustics, optimization, sports engineering","meta":"Postdoctoral Fellow, The Hong Kong Polytechnic University","search_text":"sinforiano cantos aeroacoustics, cfd, rotor acoustics, optimization, sports engineering postdoctoral fellow, the hong kong polytechnic university sinforiano cantos obtained his bachelor’s degree in aerospace engineering from polytechnic university of valencia (spain) in 2017. for his final-year research project, he studied flutter in an airfoil using numerical simulations and experiments. he received his master’s degree in aeronautical engineering from polytechnic university of valencia in 2019. in 2018, he was an exchange student in hkust, while in 2019 he was a research trainee in the von karman institute for fluid dynamics (belgium), where he developed his final-year project. after graduation, he joined aantc as a research assistant in 2019, working on aerodynamics and sports-engineering simulations and experiments. he started his phd in september 2020. aeroacoustics, cfd, rotor acoustics, optimization, sports engineering","order":76,"static_url":"/people/16/"},{"section":"Team","title":"Cheng Cao","url":"/people/59/","summary":"","meta":"PhD Candidate","search_text":"cheng cao phd candidate","order":77,"static_url":"/people/59/"},{"section":"Team","title":"Runzhen Cao","url":"/people/61/","summary":"Runzhen Cao earned his BEng degree in Aerospace Engineering from the School of Aeronautics and Astronautics at Shanghai Jiao Tong University. In the fall of 2024, he joined AANTC as a PhD student. His research interests include noise reduction design for both aircraft systems an…","meta":"PhD Candidate","search_text":"runzhen cao runzhen cao earned his beng degree in aerospace engineering from the school of aeronautics and astronautics at shanghai jiao tong university. in the fall of 2024, he joined aantc as a phd student. his research interests include noise reduction design for both aircraft systems and subsystems, ray-tracing algorithms for low-altitude vehicle sound propagation in urban environments, and aircraft airworthiness standards within the context of low-altitude economics. phd candidate runzhen cao earned his beng degree in aerospace engineering from the school of aeronautics and astronautics at shanghai jiao tong university. in the fall of 2024, he joined aantc as a phd student. his research interests include noise reduction design for both aircraft systems and subsystems, ray-tracing algorithms for low-altitude vehicle sound propagation in urban environments, and aircraft airworthiness standards within the context of low-altitude economics.","order":78,"static_url":"/people/61/"},{"section":"Team","title":"Wangqiao Chen","url":"/people/41/","summary":"measurement acoustics; super-resolution acoustic imaging method; propeller noise;","meta":"Former Research Assistant Professor, HKUST","search_text":"wangqiao chen measurement acoustics; super-resolution acoustic imaging method; propeller noise; former research assistant professor, hkust dr. wangqiao chen received his bachelor and doctor's degree from the department of aeronautics and astronautics, at peking university (china) in 2016 and 2021. his research focuses on the understanding of aeroacoustics of fluids and engines. he has systematically examined different factors affecting the propeller trailing edge noise and proposed corresponding experimental methods which can significantly improve the interpretation of physical processes. he also investigates the super-resolution acoustic imaging method, which helps identify low-frequency sources through acoustic analogy-based tomography. in addition, the super-resolution imaging method is the first time to break through the resolution limitation of low-frequency noise source imaging and is expected to be applied to the actual industrial demand. the corresponding publication has been selected as the cover of the journal of fluid mechanics. measurement acoustics; super-resolution acoustic imaging method; propeller noise;","order":79,"static_url":"/people/41/"},{"section":"Team","title":"Haochen Chu","url":"/people/67/","summary":"","meta":"PhD Student","search_text":"haochen chu phd student","order":80,"static_url":"/people/67/"},{"section":"Team","title":"Yuzhe Dun","url":"/people/69/","summary":"","meta":"PhD Student","search_text":"yuzhe dun phd student","order":81,"static_url":"/people/69/"},{"section":"Team","title":"Yi Fang","url":"/people/5/","summary":"Experimental methods, analytical acoustics, meta-surface materials, and numerical simulations.","meta":"Former Research Fellow, AANTC","search_text":"yi fang experimental methods, analytical acoustics, meta-surface materials, and numerical simulations. former research fellow, aantc dr yi fang received her bachelor degree from nanjing university of aeronautics and astronautics (china) in 2013, major in aircraft design and engineering. in 2014, she received her msc degree from cranfield university (uk), with her major in aircraft design. she joined the advanced aircraft noise technology centre and started her phd programme at the hong kong university of science and technology in 2015. she graduated in 2018 and is now a research fellow in aantc. experimental methods, analytical acoustics, meta-surface materials, and numerical simulations.","order":82,"static_url":"/people/5/"},{"section":"Team","title":"Ryu Fattah","url":"/people/1/","summary":"Manage operations at the Aerodynamics and Acoustics Facility (formerly the Wind/Wave Tunnel Facility).","meta":"Former Wind Tunnel Engineer and Manager","search_text":"ryu fattah manage operations at the aerodynamics and acoustics facility (formerly the wind/wave tunnel facility). former wind tunnel engineer and manager dr ryu fattah is the engineer/manager of the aerodynamics and acoustics facility (aaf) at the hong kong university of science and technology (hkust). he received his meng degree in aeronautics and astronautics from the university of southampton with first-class honours in 2010. he joined the airbus noise technology centre (antc) at the university of southampton (uos) in 2010 and obtained his phd in 2016. his phd thesis focused on airframe noise, specifically by the landing gear system. he designed and conducted experiments in the uos wind tunnels, and developed the antc's high-order computational aeroacoustics code. in 2014 he became a member of a 2-year antc-airbus project that involved experiments in the airbus wind tunnel at bristol, uk. afterwards, he joined hkust in october 2016 and worked as a research fellow on high-order numerical modelling and establish the group's research into drone/uav aeroacoustics. manage operations at the aerodynamics and acoustics facility (formerly the wind/wave tunnel facility).","order":83,"static_url":"/people/1/"},{"section":"Team","title":"Jingwen Guo","url":"/people/12/","summary":"High-order numerical simulations, linearised Euler equations, duct acoustics, acoustic liners, experimental methods.","meta":"Professor, Institute of Acoustics, Chinese Academy of Sciences","search_text":"jingwen guo high-order numerical simulations, linearised euler equations, duct acoustics, acoustic liners, experimental methods. professor, institute of acoustics, chinese academy of sciences mr jingwen guo received his bachelor' degree from the department of energy power system and automation, at xi'an jiao tong university (china) in 2013. he went to tsinghua university (china) and obtained his master' degree from the department of thermal engineering in 2015. since september 2015, mr jingwen guo has been a phd student at the department of mechanical and aerospace engineering at the hong kong university of science and technology. he graduated as a phd in 2019 and is now working as a research fellow in aantc. high-order numerical simulations, linearised euler equations, duct acoustics, acoustic liners, experimental methods.","order":84,"static_url":"/people/12/"},{"section":"Team","title":"YU Haoyang","url":"/people/65/","summary":"","meta":"PhD Student","search_text":"yu haoyang phd student","order":85,"static_url":"/people/65/"},{"section":"Team","title":"Jiahua He","url":"/people/51/","summary":"Jiahua obtained his BEng degree at Northwestern poly-technical University with a major of Aircraft design and engineering in 2020. Then he received his ME degree at the same university in 2023, major in aeroacoustics and aerodynamics. He joined the AANTC as a full-time PhD at HK…","meta":"PhD Candidate","search_text":"jiahua he jiahua obtained his beng degree at northwestern poly-technical university with a major of aircraft design and engineering in 2020. then he received his me degree at the same university in 2023, major in aeroacoustics and aerodynamics. he joined the aantc as a full-time phd at hkust in sep. 2023. phd candidate jiahua obtained his beng degree at northwestern poly-technical university with a major of aircraft design and engineering in 2020. then he received his me degree at the same university in 2023, major in aeroacoustics and aerodynamics. he joined the aantc as a full-time phd at hkust in sep. 2023.","order":86,"static_url":"/people/51/"},{"section":"Team","title":"Jiafan Hou","url":"/people/38/","summary":"Windsurfing simulation.","meta":"PhD in Mechanical Engineering, HKUST (2025)","search_text":"jiafan hou windsurfing simulation. phd in mechanical engineering, hkust (2025) jiafan hou received her b.eng degree from the chinese university of hong kong, shenzhen (cuhksz) in 2020. before joining aantc, she worked as a research assistant in robotics & artificial intelligence lab in cuhksz. she started her phd study at hkust in sep. 2021 and focused on the research of windsurfing simulation. windsurfing simulation.","order":87,"static_url":"/people/38/"},{"section":"Team","title":"Zixiang Hu","url":"/people/50/","summary":"Mr. HU Zixiang obtained his bachelor's degree and master's degree from Beihang University in 2020 and 2023 respectively. His previous major was tracked robot, especially in design, modeling, control and attitude perception. He started his PhD study at HKUST in Sept. 2023.","meta":"PhD Candidate","search_text":"zixiang hu mr. hu zixiang obtained his bachelor's degree and master's degree from beihang university in 2020 and 2023 respectively. his previous major was tracked robot, especially in design, modeling, control and attitude perception. he started his phd study at hkust in sept. 2023. phd candidate mr. hu zixiang obtained his bachelor's degree and master's degree from beihang university in 2020 and 2023 respectively. his previous major was tracked robot, especially in design, modeling, control and attitude perception. he started his phd study at hkust in sept. 2023.","order":88,"static_url":"/people/50/"},{"section":"Team","title":"Hanbo Jiang","url":"/people/6/","summary":"Computational fluid dynamics; Computational aeroacoustics Boundary element method","meta":"Assistant Professor, Eastern Institute of Technology, Ningbo","search_text":"hanbo jiang computational fluid dynamics; computational aeroacoustics boundary element method assistant professor, eastern institute of technology, ningbo dr. hanbo jiang was born in nov. 1990 in the jilin province of china. he obtained his bachelor's degree of aeronautics and astronautics at peking university (china) in 2014. he continued his study at the same university and obtained his master's degree of mechanics(dynamics and control). he was admitted to the hong kong university of science and technology in sept. 2017 and got his phd degree in jan. 2021. currently his research focuses on developing and applying numerical methods to study aeroacoustic problems, e.g., multi-propeller powered urban aerial vehicle noise. computational fluid dynamics; computational aeroacoustics boundary element method","order":89,"static_url":"/people/6/"},{"section":"Team","title":"Stanley Leung","url":"/people/47/","summary":"","meta":"Teaching Associate","search_text":"stanley leung teaching associate","order":90,"static_url":"/people/47/"},{"section":"Team","title":"Xiangru Li","url":"/people/46/","summary":"Sports Engineering Experiment; Physiology;","meta":"PhD Candidate","search_text":"xiangru li sports engineering experiment; physiology; phd candidate mr. xiangru li obtained his bachelor's degree in mechanical engineering at the university of hong kong in jun 2020. in 2020-2021, he worked as a ra at southern university of science and technology in shenzhen and developed a bio-inspired robotic fish and won the gwr of the fastest 50m swim by a robotic fish. then he received the master's degree at hkust in jun 2022, and joined the aantc as a full-time phd student in sep 2022. mr. li will focus on the sports aerodynamics coupled with physiological status. sports engineering experiment; physiology;","order":91,"static_url":"/people/46/"},{"section":"Team","title":"Xiangtian Li","url":"/people/42/","summary":"","meta":"Post-doctoral Fellow","search_text":"xiangtian li post-doctoral fellow","order":92,"static_url":"/people/42/"},{"section":"Team","title":"Yuhong Li","url":"/people/34/","summary":"Aeroelasticity and aeroacoustics, CFD and CAA","meta":"PhD in Mechanical Engineering, HKUST (2024)","search_text":"yuhong li aeroelasticity and aeroacoustics, cfd and caa phd in mechanical engineering, hkust (2024) yuhong li was born in may. 1997 in chongqing, china. he studied aeronautics and astronautics in the aerospace school at tsinghua university, and obtained his bachelor's degree in 2018. after graduation he went to imperial college london and obtained his msc in advanced computational methods for aeronautics, flow management and fluid-structure interaction with distinction. he was admitted to the hong kong university of science and technology to pursue his phd degree on sept. 2020. currently his research interest lies in theoretical and computational aeroacoustic problems of flexible wings. aeroelasticity and aeroacoustics, cfd and caa","order":93,"static_url":"/people/34/"},{"section":"Team","title":"Guangsheng Liu","url":"/people/19/","summary":"Aero-sensors; Electronic Device/Sensor Design; Vapor Liquid Microthruster; Experimental Aerodynamics","meta":"Post-doctoral Fellow","search_text":"guangsheng liu aero-sensors; electronic device/sensor design; vapor liquid microthruster; experimental aerodynamics post-doctoral fellow mr liu guangsheng obtained his bsc degree in harbor channel and coastal engineering from ocean university of china. for the final year of research, he worked on a topic about 2d numerical simulations for oscillating hydrofoil. he also has experience in control and automation system design. his project multi-rotor skid linkage rescue drone won the first prize in national marine vehicle design and production competition, 2016. he received his msc degree in aeronautical engineering from the hong kong university of science and technology, and his master research mainly focused on experimental aerodynamics and professional sports engineering. he joined in aantc as a research assistant in august 2019. aero-sensors; electronic device/sensor design; vapor liquid microthruster; experimental aerodynamics","order":94,"static_url":"/people/19/"},{"section":"Team","title":"Qian Liu","url":"/people/23/","summary":"Trailing edge noise, Elastic materials, Experimental methods","meta":"PhD in Mechanical Engineering, HKUST (2023)","search_text":"qian liu trailing edge noise, elastic materials, experimental methods phd in mechanical engineering, hkust (2023) miss liu qian obtained her bsc and msc degree in flight vehicle design from the northwestern polytechnical university in 2016 and 2019 respectively. her undergraduate dissertation is about the difference schemes of computational acoustic propagation equation. during the master period, she mainly focused on time-domain impedance boundary condition. miss liu qian joined aantc as a phd student of the joint program of the hong kong university of science and technology and southern university of science and technology in the fall of 2019. trailing edge noise, elastic materials, experimental methods","order":95,"static_url":"/people/23/"},{"section":"Team","title":"Zhida Ma","url":"/people/35/","summary":"rotor aerodynamics and aeroacoustics, the design and noise mitigation method for UAVs and eVTOL aircrafts.","meta":"Post-doctoral Fellow","search_text":"zhida ma rotor aerodynamics and aeroacoustics, the design and noise mitigation method for uavs and evtol aircrafts. post-doctoral fellow mr. ma zhida received his b.eng degree in aircraft design and engineering from nanjing university of aeronautics and astronautics (china) in 2018. his final year project was the design and implementation of a small-scale uav with distributed electric propulsion. he obtained his m.sc degree in mechanical engineering from the hong kong university of science and technology in 2020. he started his phd study at hkust in sept. 2020. rotor aerodynamics and aeroacoustics, the design and noise mitigation method for uavs and evtol aircrafts.","order":96,"static_url":"/people/35/"},{"section":"Team","title":"Jiaqi Mao","url":"/people/43/","summary":"","meta":"Post-doctoral Fellow","search_text":"jiaqi mao post-doctoral fellow","order":97,"static_url":"/people/43/"},{"section":"Team","title":"Kwan Pui Mok","url":"/people/33/","summary":"","meta":"Post-doctoral Fellow","search_text":"kwan pui mok post-doctoral fellow","order":98,"static_url":"/people/33/"},{"section":"Team","title":"Zhenjun Peng","url":"/people/49/","summary":"Zhenjun received his BEng degree from Nanjing University of Aeronautics and Astronautics with a major in Aircraft design and engineering in 2021. He received his MSc degree from Cranfield University in 2022, major in Aerospace vehicle design. He joined AANTC as a PhD student in …","meta":"PhD Candidate","search_text":"zhenjun peng zhenjun received his beng degree from nanjing university of aeronautics and astronautics with a major in aircraft design and engineering in 2021. he received his msc degree from cranfield university in 2022, major in aerospace vehicle design. he joined aantc as a phd student in the spring of 2023. phd candidate zhenjun received his beng degree from nanjing university of aeronautics and astronautics with a major in aircraft design and engineering in 2021. he received his msc degree from cranfield university in 2022, major in aerospace vehicle design. he joined aantc as a phd student in the spring of 2023.","order":99,"static_url":"/people/49/"},{"section":"Team","title":"Renhao Qu","url":"/people/36/","summary":"aeroacoustics, metasurfaces, duct acoustics","meta":"PhD in Mechanical Engineering, HKUST (2024)","search_text":"renhao qu aeroacoustics, metasurfaces, duct acoustics phd in mechanical engineering, hkust (2024) mr qu renhao obtained his bsc degree from chongqing university in 2017 and the master’s degree of mechanical engineering in shanghai jiao tong university. he joined hkust in 2020 and his current research interest is to develop the metasurfaces in aeroacoustics. aeroacoustics, metasurfaces, duct acoustics","order":100,"static_url":"/people/36/"},{"section":"Team","title":"Étienne Spieser","url":"/people/52/","summary":"I am particularly interested in the fundamental mechanisms involved in the generation of sound by flow. I am currently working on the development of analytical and numerical tools for aeroacoustics.","meta":"Researcher, Électricité de France","search_text":"étienne spieser i am particularly interested in the fundamental mechanisms involved in the generation of sound by flow. i am currently working on the development of analytical and numerical tools for aeroacoustics. researcher, électricité de france after graduating from the french aeronautical engineering school isae-supaéro, i did my doctoral studies on the modelling of sound propagation in jets at the école centrale de lyon. i am a research associate in the department of mechanical and aerospace engineering at hkust since september 2022. i am particularly interested in the fundamental mechanisms involved in the generation of sound by flow. i am currently working on the development of analytical and numerical tools for aeroacoustics.","order":101,"static_url":"/people/52/"},{"section":"Team","title":"Shivam Sundeep","url":"/people/25/","summary":"Experimental aeroacoustics, Aerodynamics flow over metamaterials, Acoustic holography.","meta":"PhD in Mechanical Engineering, HKUST (2023)","search_text":"shivam sundeep experimental aeroacoustics, aerodynamics flow over metamaterials, acoustic holography. phd in mechanical engineering, hkust (2023) i received my bachelor's degree in mechanical engineering in 2015 from sardar vallabhbhai national institute of technology (nit) india. my final year project was on solar energy storage using phase change materials. i completed my masters in thermal engineering from indian institute of technology madras (iitm) india in 2017. my research topic in masters was nearfield acoustic holography of jets and hartman whistle. after that i have worked in belcan company for two years as thermo-fluid engineer. i worked on simulation of secondary air flow and oil heat management system of rolls royce jet engines. i have joined hkust as a phd student in 2019. experimental aeroacoustics, aerodynamics flow over metamaterials, acoustic holography.","order":102,"static_url":"/people/25/"},{"section":"Team","title":"Qichen Tan","url":"/people/31/","summary":"Noise perception, UAM planning, and Human-computer interaction","meta":"Associate Professor, Soochow University","search_text":"qichen tan noise perception, uam planning, and human-computer interaction associate professor, soochow university dr. qichen tan obtained his phd degree in intelligent transportation at hkust in 2024, and obtained the beng degree in software engineering at university of electronic science and technology of china in 2020. his study focuses on noise simulation of pilotless aerial vehicle, sustainable flight path planning, and artificial intelligence. noise perception, uam planning, and human-computer interaction","order":103,"static_url":"/people/31/"},{"section":"Team","title":"Lican Wang","url":"/people/53/","summary":"He's interested in the fundamental physics of aerodynamics and aeroacoustics, spanning from subsonic to supersonic regimes. He developed a stabilized numerical method and some theoretical correction schemes to help understand the recognized issue of sound propagation within non-…","meta":"Lecturer, Research Institute of Aerospace Technology, Central South University","search_text":"lican wang he's interested in the fundamental physics of aerodynamics and aeroacoustics, spanning from subsonic to supersonic regimes. he developed a stabilized numerical method and some theoretical correction schemes to help understand the recognized issue of sound propagation within non-uniform sheared flows, which drives the discovery of a total reflection mechanism at wide incident angles. assisted by advanced experimental techniques and machine learning algorithms, he experimentally explored the transition behavior of supersonic sheared flow over different rough metasurfaces for the first time. he has recently worked on engineering topics such as beamforming acceleration and the boundary element method, which facilitate the progression of acoustic imaging techniques in scattering environments and the fast multipole equivalent source method. lecturer, research institute of aerospace technology, central south university he received a bachelor's degree in 2016 and a doctoral degree in 2021 at xiamen university. then, he engaged in postdoctoral research at the national university of defense and technology. in 2023, he joined aantc as a research associate. he's interested in the fundamental physics of aerodynamics and aeroacoustics, spanning from subsonic to supersonic regimes. he developed a stabilized numerical method and some theoretical correction schemes to help understand the recognized issue of sound propagation within non-uniform sheared flows, which drives the discovery of a total reflection mechanism at wide incident angles. assisted by advanced experimental techniques and machine learning algorithms, he experimentally explored the transition behavior of supersonic sheared flow over different rough metasurfaces for the first time. he has recently worked on engineering topics such as beamforming acceleration and the boundary element method, which facilitate the progression of acoustic imaging techniques in scattering environments and the fast multipole equivalent source method.","order":104,"static_url":"/people/53/"},{"section":"Team","title":"Zilu Wang","url":"/people/54/","summary":"Mr. Wang Zilu received his Bachelor's degree in Engineering from Harbin Institute of Technology (China) in 2019, and then went to the Ecole Centrale de Nantes (France) to study computational mechanics and obtain his Master's degree. Mr. Wang worked as a research assistant at the…","meta":"PhD Candidate","search_text":"zilu wang mr. wang zilu received his bachelor's degree in engineering from harbin institute of technology (china) in 2019, and then went to the ecole centrale de nantes (france) to study computational mechanics and obtain his master's degree. mr. wang worked as a research assistant at the state key laboratory of aerodynamics and then at the hong kong university of science and technology. he joined aantc as a full-time doctoral student in september 2023. phd candidate mr. wang zilu received his bachelor's degree in engineering from harbin institute of technology (china) in 2019, and then went to the ecole centrale de nantes (france) to study computational mechanics and obtain his master's degree. mr. wang worked as a research assistant at the state key laboratory of aerodynamics and then at the hong kong university of science and technology. he joined aantc as a full-time doctoral student in september 2023.","order":105,"static_url":"/people/54/"},{"section":"Team","title":"Han Wu","url":"/people/8/","summary":"aeroacoustics, propeller noise, experimental method","meta":"Postdoctoral Fellow, The Hong Kong Polytechnic University","search_text":"han wu aeroacoustics, propeller noise, experimental method postdoctoral fellow, the hong kong polytechnic university mr. han wu obtained his bachelor’s degree of engineering in xi’an jiaotong university in 2017. then he went to hkust and received his msc degree. afterwards he joined aantc as a research assistant and conducted his phd study in 2020. he is currently working on the experimental investigation on the noise generated by the propellers of multi-rotor powered vehicles. aeroacoustics, propeller noise, experimental method","order":106,"static_url":"/people/8/"},{"section":"Team","title":"Yuqi Xiao","url":"/people/68/","summary":"","meta":"PhD Student","search_text":"yuqi xiao phd student","order":107,"static_url":"/people/68/"},{"section":"Team","title":"Wei Yi","url":"/people/24/","summary":"Experimental methods, computational fluid dynamics, and aeroacoustics.","meta":"Alumni","search_text":"wei yi experimental methods, computational fluid dynamics, and aeroacoustics. alumni he joined the hkust in 2018. he obtained his bachelor's degree of theoretical and applied mechanics from northwestern polytechnical university (china) in 2010. in the same year, he entered ari (aerodynamics research institute) of avic (china) and the main research area is propeller design and research, wind tunnel design and experiment. he served as the director of the wind tunnel system technology office and the director of system and aerodynamic technology office of ari. he was in charge and involved in a series of scientific research or engineering projects, including national research projects, the avic's innovation fund, national technical reform projects, etc. involving a total investment of hundreds of millions. he won the title of outstanding individual/outstanding contribution/advanced model five times in more than seven years of work, two of which are first prizes of institute -level scientific and technological achievements, and became the only one who was accelerable promoted to be an engineer in harbin branch institute in 2014. he is \"excellent youth expert in harbin\" and \"young professionals in central enterprises of china\". experimental methods, computational fluid dynamics, and aeroacoustics.","order":108,"static_url":"/people/24/"},{"section":"Team","title":"Wei Ying","url":"/people/40/","summary":"","meta":"PhD in Mechanical Engineering, HKUST (2021)","search_text":"wei ying phd in mechanical engineering, hkust (2021)","order":109,"static_url":"/people/40/"},{"section":"Team","title":"Xin Zhang","url":"/people/2/","summary":"Chair Professor","meta":"Swire Professor of Aerospace Engineering and Chair Professor","search_text":"xin zhang chair professor swire professor of aerospace engineering and chair professor prof. zhang conducts research and lectures in aerodynamics and aeroacoustics, in particular, aircraft aerodynamics and noise. he has conducted experimental and computational research in the area of unsteady aerodynamics, ground effect, aeroacoustics, and aircraft noise. he is an authority in the airframe and engine noise. he performed research in its understanding, developed novel and accurate numerical schemes for its prediction, devised methods for noise attenuation and developed predictive codes based on physics for noise prediction which are being used by industry. chair professor","order":110,"static_url":"/people/2/"},{"section":"Team","title":"Zhicheng Zhang","url":"/people/58/","summary":"","meta":"PhD Candidate","search_text":"zhicheng zhang phd candidate","order":111,"static_url":"/people/58/"},{"section":"Team","title":"Chuntai Zheng","url":"/people/22/","summary":"Experiment methods, Aerodynamics and Aeroacoustics.","meta":"Assistant Professor, Shenzhen Technology University","search_text":"chuntai zheng experiment methods, aerodynamics and aeroacoustics. assistant professor, shenzhen technology university mr. zheng chuntai has received his bachelor degree from harbin engineering university (china), school of power and energy engineering in 2014. in the same year, as a master student, he joined beihang university, school of energy and power engineering, and graduated in 2017. his master research mainly focused on turbomachinery, experimental fluid mechanics and optical measurement. in 2019, he joined the hong kong university of science and technology, the department of mechanical and aerospace engineering, as a ph.d. candidate. experiment methods, aerodynamics and aeroacoustics.","order":112,"static_url":"/people/22/"},{"section":"Team","title":"Siyang Zhong","url":"/people/3/","summary":"High-order simulations, analytical acoustics, and turbulence-aerofoil leading edge noise.","meta":"Assistant Professor, Department of Aeronautical and Aviation Engineering, The Hong Kong Polytechnic University","search_text":"siyang zhong high-order simulations, analytical acoustics, and turbulence-aerofoil leading edge noise. assistant professor, department of aeronautical and aviation engineering, the hong kong polytechnic university mr siyang zhong was born in oct. 1989 in the guizhou province of china. he obtained his bachelor's degree of theoretical and applied mechanics at peking university (china) in 2011. he continued his study at the same university and obtained his master's degree of control theory. he was admitted to the hong kong university of science and technology to pursue his phd degree on jan. 2015. he graduate as a phd in 2018. currently his research focuses on developing and applying high-order numerical methods to study aeroacoustic problems. high-order simulations, analytical acoustics, and turbulence-aerofoil leading edge noise.","order":113,"static_url":"/people/3/"},{"section":"Team","title":"Peng Zhou","url":"/people/7/","summary":"Experimental methods, MEMS and NEMS design, hydrophobic nanomaterials, and aeroacoustics.","meta":"Research Assistant Professor","search_text":"peng zhou experimental methods, mems and nems design, hydrophobic nanomaterials, and aeroacoustics. research assistant professor dr peng zhou joined aantc as a phd candidate in the fall of 2017. he received his bachelor's degree in mechanical engineering and minor in math from the hong kong university of science and technology in 2017. he has done undergraduate research about super-hydrophobic nanomaterials, and a joint research program about 2d materials at the mit eecs lab. his final year design project titled \"smart soft end effector\" won the president's cup in 2017, and was selected as one of the outstanding final year design projects. experimental methods, mems and nems design, hydrophobic nanomaterials, and aeroacoustics.","order":114,"static_url":"/people/7/"},{"section":"Team","title":"Teng Zhou","url":"/people/13/","summary":"","meta":"Lecturer in Acoustics, University of Southampton","search_text":"teng zhou lecturer in acoustics, university of southampton","order":115,"static_url":"/people/13/"},{"section":"Publications","title":"Stochastic wind-aware route planning in competitive sailing: A Markov-enhanced hybrid A* approach","url":"/publications/169/","summary":"Hou, Jiafan; Tan, Qichen; Mok, Kwan Pui; Zhou, Peng; Zhang, Xin. “Stochastic wind-aware route planning in competitive sailing: A Markov-enhanced hybrid A* approach.” Ocean Engineering, v. 364, (P2), article number 126948. (2026). DOI: 10.1016/j.oceaneng.2026.126948.","meta":"Journal article · 2026","search_text":"stochastic wind-aware route planning in competitive sailing: a markov-enhanced hybrid a* approach hou, jiafan; tan, qichen; mok, kwan pui; zhou, peng; zhang, xin. “stochastic wind-aware route planning in competitive sailing: a markov-enhanced hybrid a* approach.” ocean engineering, v. 364, (p2), article number 126948. (2026). doi: 10.1016/j.oceaneng.2026.126948. journal article · 2026 hou, jiafan; tan, qichen; mok, kwan pui; zhou, peng; zhang, xin 2026 10.1016/j.oceaneng.2026.126948 ocean engineering 364 (p2) article 126948","order":116,"static_url":"/publications/169/"},{"section":"Publications","title":"Optimizing Cycling Postures: Upper Limb Muscle Effort and Aerodynamic Performance","url":"/publications/168/","summary":"LI, Xiangru; ZHOU, Peng; ZHANG, Xin. “Optimizing Cycling Postures: Upper Limb Muscle Effort and Aerodynamic Performance.” International Journal of Sports Physiology and Performance, v. 21, (5), p. 656-665. (2026). DOI: 10.1123/ijspp.2025-0344.","meta":"Journal article · 2026","search_text":"optimizing cycling postures: upper limb muscle effort and aerodynamic performance li, xiangru; zhou, peng; zhang, xin. “optimizing cycling postures: upper limb muscle effort and aerodynamic performance.” international journal of sports physiology and performance, v. 21, (5), p. 656-665. (2026). doi: 10.1123/ijspp.2025-0344. journal article · 2026 li, xiangru; zhou, peng; zhang, xin 2026 10.1123/ijspp.2025-0344 international journal of sports physiology and performance 21 (5) 656-665","order":117,"static_url":"/publications/168/"},{"section":"Publications","title":"Influence of aerodynamic and kinematic parameters on the propulsive performance of wingsail pumping","url":"/publications/167/","summary":"Mok, Kwan Pui; Zhou, Peng; Zhang, Xin. “Influence of aerodynamic and kinematic parameters on the propulsive performance of wingsail pumping.” Ocean Engineering, v. 344, article number 123572. (2026). DOI: 10.1016/j.oceaneng.2025.123572.","meta":"Journal article · 2026","search_text":"influence of aerodynamic and kinematic parameters on the propulsive performance of wingsail pumping mok, kwan pui; zhou, peng; zhang, xin. “influence of aerodynamic and kinematic parameters on the propulsive performance of wingsail pumping.” ocean engineering, v. 344, article number 123572. (2026). doi: 10.1016/j.oceaneng.2025.123572. journal article · 2026 mok, kwan pui; zhou, peng; zhang, xin 2026 10.1016/j.oceaneng.2025.123572 ocean engineering 344 article 123572","order":118,"static_url":"/publications/167/"},{"section":"Publications","title":"Experimental Flow and Aeroacoustic Study of a Ducted Propeller in Axial Flow","url":"/publications/166/","summary":"Cantos, Sinforiano; Wu, Han; LI, Xiangtian; ZHOU, Peng; ZHANG, Xin. “Experimental Flow and Aeroacoustic Study of a Ducted Propeller in Axial Flow.” AIAA Journal. (2026). DOI: 10.2514/1.j066347.","meta":"Journal article · 2026","search_text":"experimental flow and aeroacoustic study of a ducted propeller in axial flow cantos, sinforiano; wu, han; li, xiangtian; zhou, peng; zhang, xin. “experimental flow and aeroacoustic study of a ducted propeller in axial flow.” aiaa journal. (2026). doi: 10.2514/1.j066347. journal article · 2026 cantos, sinforiano; wu, han; li, xiangtian; zhou, peng; zhang, xin 2026 10.2514/1.j066347 aiaa journal","order":119,"static_url":"/publications/166/"},{"section":"Publications","title":"Experimental evaluation of a frequency-domain acoustic model for drone rotor noise prediction in non-axial flows","url":"/publications/165/","summary":"Zhang, Zhicheng; Peng, Zhenjun; Chen, Bao; Zhou, Peng; Zhang, Xin. “Experimental evaluation of a frequency-domain acoustic model for drone rotor noise prediction in non-axial flows.” Aerospace Science and Technology, v. 176, (Part E), article number 112737. (2026). DOI: 10.1016/…","meta":"Journal article · 2026","search_text":"experimental evaluation of a frequency-domain acoustic model for drone rotor noise prediction in non-axial flows zhang, zhicheng; peng, zhenjun; chen, bao; zhou, peng; zhang, xin. “experimental evaluation of a frequency-domain acoustic model for drone rotor noise prediction in non-axial flows.” aerospace science and technology, v. 176, (part e), article number 112737. (2026). doi: 10.1016/j.ast.2026.112737. journal article · 2026 zhang, zhicheng; peng, zhenjun; chen, bao; zhou, peng; zhang, xin 2026 10.1016/j.ast.2026.112737 aerospace science and technology 176 (part e) article 112737","order":120,"static_url":"/publications/165/"},{"section":"Publications","title":"Effects of vortex dynamics on rotor aeroacoustics during blade-vortex interaction","url":"/publications/164/","summary":"Li, Xiangtian; Chen, Wangqiao; Peng, Zhenjun; Zhou, Peng; Zhang, Xin. “Effects of vortex dynamics on rotor aeroacoustics during blade-vortex interaction.” Journal of Fluid Mechanics, v. 1038, p. 1-35, article number A47. (2026). DOI: 10.1017/jfm.2026.11750.","meta":"Journal article · 2026","search_text":"effects of vortex dynamics on rotor aeroacoustics during blade-vortex interaction li, xiangtian; chen, wangqiao; peng, zhenjun; zhou, peng; zhang, xin. “effects of vortex dynamics on rotor aeroacoustics during blade-vortex interaction.” journal of fluid mechanics, v. 1038, p. 1-35, article number a47. (2026). doi: 10.1017/jfm.2026.11750. journal article · 2026 li, xiangtian; chen, wangqiao; peng, zhenjun; zhou, peng; zhang, xin 2026 10.1017/jfm.2026.11750 journal of fluid mechanics 1038 1-35; article a47","order":121,"static_url":"/publications/164/"},{"section":"Publications","title":"Aeroacoustics of a wing encountering large-scale vortex gusts","url":"/publications/163/","summary":"Li, Xiangtian; Chen, Wangqiao; Wang, Puyuan; Chen, Bao; Zhou, Peng; Zhang, Xin. “Aeroacoustics of a wing encountering large-scale vortex gusts.” Journal of the Acoustical Society of America, v. 160, (2), p. 1546-1559. (2026). DOI: 10.1121/10.0046094.","meta":"Journal article · 2026","search_text":"aeroacoustics of a wing encountering large-scale vortex gusts li, xiangtian; chen, wangqiao; wang, puyuan; chen, bao; zhou, peng; zhang, xin. “aeroacoustics of a wing encountering large-scale vortex gusts.” journal of the acoustical society of america, v. 160, (2), p. 1546-1559. (2026). doi: 10.1121/10.0046094. journal article · 2026 li, xiangtian; chen, wangqiao; wang, puyuan; chen, bao; zhou, peng; zhang, xin 2026 10.1121/10.0046094 journal of the acoustical society of america 160 (2) 1546-1559","order":122,"static_url":"/publications/163/"},{"section":"Publications","title":"On weak compressibility effects in low-Mach-number aeroacoustic simulations of small-scale rotors","url":"/publications/162/","summary":"ZHANG, Zhicheng; XIAO, Yuqi; PENG, Zhenjun; ZHOU, Peng; ZHANG, Xin. “On weak compressibility effects in low-Mach-number aeroacoustic simulations of small-scale rotors.” Physics of Fluids, v. 38, (7), article number 078119. (2026). DOI: 10.1063/5.0335315.","meta":"Journal article · 2026","search_text":"on weak compressibility effects in low-mach-number aeroacoustic simulations of small-scale rotors zhang, zhicheng; xiao, yuqi; peng, zhenjun; zhou, peng; zhang, xin. “on weak compressibility effects in low-mach-number aeroacoustic simulations of small-scale rotors.” physics of fluids, v. 38, (7), article number 078119. (2026). doi: 10.1063/5.0335315. journal article · 2026 zhang, zhicheng; xiao, yuqi; peng, zhenjun; zhou, peng; zhang, xin 2026 10.1063/5.0335315 physics of fluids 38 (7) article 078119","order":123,"static_url":"/publications/162/"},{"section":"Publications","title":"The Air Vehicle Flyover Noise Assessment in Urban Areas with Complex Urban Wind Conditions","url":"/publications/187/","summary":"BAO, Hongsen; TAN, Qichen; HE, Jiahua; ZHOU, Peng; CHEN, Wangqiao; ZHANG, Xin. “The Air Vehicle Flyover Noise Assessment in Urban Areas with Complex Urban Wind Conditions.” Paper presented at The 31st International Congress on Sound and Vibration (ICSV31), Incheon, Korea, Republ…","meta":"Conference paper · 2025","search_text":"the air vehicle flyover noise assessment in urban areas with complex urban wind conditions bao, hongsen; tan, qichen; he, jiahua; zhou, peng; chen, wangqiao; zhang, xin. “the air vehicle flyover noise assessment in urban areas with complex urban wind conditions.” paper presented at the 31st international congress on sound and vibration (icsv31), incheon, korea, republic of. (2025). conference paper · 2025 bao, hongsen; tan, qichen; he, jiahua; zhou, peng; chen, wangqiao; zhang, xin 2025 paper presented at the 31st international congress on sound and vibration (icsv31), incheon, korea, republic of","order":124,"static_url":"/publications/187/"},{"section":"Publications","title":"Outdoor and Indoor Acoustic Characterization of Low-Altitude Flying UAS","url":"/publications/186/","summary":"Ma, Zhida; Peng, Zhenjun; Cao, Runzhen; Shum, Nick; Liu, Guangsheng; He, Jiahua; Zhou, Peng; Chen, Wangqiao; Zhang, Xin. “Outdoor and Indoor Acoustic Characterization of Low-Altitude Flying UAS.” Proceedings of 2025 International Conference of Mechanical Engineering on Aerospace…","meta":"Conference paper · 2025","search_text":"outdoor and indoor acoustic characterization of low-altitude flying uas ma, zhida; peng, zhenjun; cao, runzhen; shum, nick; liu, guangsheng; he, jiahua; zhou, peng; chen, wangqiao; zhang, xin. “outdoor and indoor acoustic characterization of low-altitude flying uas.” proceedings of 2025 international conference of mechanical engineering on aerospace, comea 2025, institute of electrical and electronics engineers inc., 2025, article number 11241330. (2025). doi: 10.1109/comea66280.2025.11241330. conference paper · 2025 ma, zhida; peng, zhenjun; cao, runzhen; shum, nick; liu, guangsheng; he, jiahua; zhou, peng; chen, wangqiao; zhang, xin 2025 10.1109/comea66280.2025.11241330 proceedings of 2025 international conference of mechanical engineering on aerospace, comea 2025, institute of electrical and electronics engineers inc., 2025, article number 11241330 article 11241330","order":125,"static_url":"/publications/186/"},{"section":"Publications","title":"Experimental Study on Contra-Rotating Rotor Noise During Descending Process","url":"/publications/185/","summary":"Cao, Cheng; Ma, Zhida; Li, Xiangtian; Chen, Wangqiao; Zhou, Peng; Zhang, Xin; Wang, Puyuan; Chen, Bao. “Experimental Study on Contra-Rotating Rotor Noise During Descending Process.” Proceedings of the 31st International Congress on Sound and Vibration (ICSV31), Society of Acoust…","meta":"Conference paper · 2025","search_text":"experimental study on contra-rotating rotor noise during descending process cao, cheng; ma, zhida; li, xiangtian; chen, wangqiao; zhou, peng; zhang, xin; wang, puyuan; chen, bao. “experimental study on contra-rotating rotor noise during descending process.” proceedings of the 31st international congress on sound and vibration (icsv31), society of acoustics, 2025, p. 2645-2652. (2025). conference paper · 2025 cao, cheng; ma, zhida; li, xiangtian; chen, wangqiao; zhou, peng; zhang, xin; wang, puyuan; chen, bao 2025 proceedings of the 31st international congress on sound and vibration (icsv31), society of acoustics, 2025, p. 2645-2652 2645-2652","order":126,"static_url":"/publications/185/"},{"section":"Publications","title":"Acoustic response of wing interaction with large-scale vortex gusts","url":"/publications/184/","summary":"Li, Xiangtian; Chen, Wangqiao; Zhou, Peng; Zhang, Xin; Chen, Bao; Wang, Puyuan. “Acoustic response of wing interaction with large-scale vortex gusts.” Paper presented at 54th International Congress and Exposition on Noise Control Engineering, INTERNOISE 2025, Sao Paulo, Brazil, …","meta":"Conference paper · 2025","search_text":"acoustic response of wing interaction with large-scale vortex gusts li, xiangtian; chen, wangqiao; zhou, peng; zhang, xin; chen, bao; wang, puyuan. “acoustic response of wing interaction with large-scale vortex gusts.” paper presented at 54th international congress and exposition on noise control engineering, internoise 2025, sao paulo, brazil, p. 971-982. (2025). doi: 10.3397/in_2025_1074217. conference paper · 2025 li, xiangtian; chen, wangqiao; zhou, peng; zhang, xin; chen, bao; wang, puyuan 2025 10.3397/in_2025_1074217 paper presented at 54th international congress and exposition on noise control engineering, internoise 2025, sao paulo, brazil, p. 971-982 971-982","order":127,"static_url":"/publications/184/"},{"section":"Publications","title":"Balance of Upper Limb Muscle Activation and Aerodynamics for Cycling Posture Optimization","url":"/publications/183/","summary":"Li, Xiangru; Zhou, Peng; Zhang, Xin. “Balance of Upper Limb Muscle Activation and Aerodynamics for Cycling Posture Optimization.” Proceedings of the 13th International Conference on Sport Sciences Research and Technology Support, IcSPORTS 2025 / edited by Arellano Raul; Morouco …","meta":"Conference paper · 2025","search_text":"balance of upper limb muscle activation and aerodynamics for cycling posture optimization li, xiangru; zhou, peng; zhang, xin. “balance of upper limb muscle activation and aerodynamics for cycling posture optimization.” proceedings of the 13th international conference on sport sciences research and technology support, icsports 2025 / edited by arellano raul; morouco pedro; capelli carlo. science and technology publications, lda, 2025, p. 50-56. (2025). doi: 10.5220/0013677000003988. conference paper · 2025 li, xiangru; zhou, peng; zhang, xin 2025 10.5220/0013677000003988 proceedings of the 13th international conference on sport sciences research and technology support, icsports 2025 / edited by arellano raul; morouco pedro; capelli carlo. science and technology publications, lda, 2025, p. 50-56 50-56","order":128,"static_url":"/publications/183/"},{"section":"Publications","title":"Anechoic Noise Characterization Of Sub-7kg Multi-Rotor Drones: Configuration Effects And Spl Scaling Models","url":"/publications/182/","summary":"Cao, Runzhen; Zhang, Zhicheng; Peng, Zhenjun; Ma, Zhida; Chen, Wangqiao; Zhou, Peng; Zhang, Xin. “Anechoic Noise Characterization Of Sub-7kg Multi-Rotor Drones: Configuration Effects And Spl Scaling Models.” Proceedings of the 11th Convention of the European Acoustics Associatio…","meta":"Conference paper · 2025","search_text":"anechoic noise characterization of sub-7kg multi-rotor drones: configuration effects and spl scaling models cao, runzhen; zhang, zhicheng; peng, zhenjun; ma, zhida; chen, wangqiao; zhou, peng; zhang, xin. “anechoic noise characterization of sub-7kg multi-rotor drones: configuration effects and spl scaling models.” proceedings of the 11th convention of the european acoustics association forum acusticum / euronoise 2025, málaga, spain: european acoustics association, eaa, 2025, p. 1697-1704. (2025). doi: 10.61782/fa.2025.0137. conference paper · 2025 cao, runzhen; zhang, zhicheng; peng, zhenjun; ma, zhida; chen, wangqiao; zhou, peng; zhang, xin 2025 10.61782/fa.2025.0137 proceedings of the 11th convention of the european acoustics association forum acusticum / euronoise 2025, málaga, spain: european acoustics association, eaa, 2025, p. 1697-1704 1697-1704","order":129,"static_url":"/publications/182/"},{"section":"Publications","title":"Experimental aeroacoustics of rotors with aeroelastic effects under edgewise forward flight conditions","url":"/publications/181/","summary":"Peng, Zhenjun; Chen, Wangqiao; Chen, Bao; Wang, Puyuan; Zhou, Peng; Zhang, Xin. “Experimental aeroacoustics of rotors with aeroelastic effects under edgewise forward flight conditions.” Paper presented at 54th International Congress and Exposition on Noise Control Engineering, I…","meta":"Conference paper · 2025","search_text":"experimental aeroacoustics of rotors with aeroelastic effects under edgewise forward flight conditions peng, zhenjun; chen, wangqiao; chen, bao; wang, puyuan; zhou, peng; zhang, xin. “experimental aeroacoustics of rotors with aeroelastic effects under edgewise forward flight conditions.” paper presented at 54th international congress and exposition on noise control engineering, internoise 2025, sao paulo, brazil, p. 983-994. (2025). doi: 10.3397/in_2025_1074218. conference paper · 2025 peng, zhenjun; chen, wangqiao; chen, bao; wang, puyuan; zhou, peng; zhang, xin 2025 10.3397/in_2025_1074218 paper presented at 54th international congress and exposition on noise control engineering, internoise 2025, sao paulo, brazil, p. 983-994 983-994","order":130,"static_url":"/publications/181/"},{"section":"Publications","title":"Acoustic-Driven Artificial Potential Field for Low-Noise Multi-UAV Path Planning","url":"/publications/180/","summary":"Tan, Qichen; Dun, Yuzhe; He, Jiahua; Bao, Hongsen; Chen, Wangqiao; Zhou, Peng; Zhang, Xin. “Acoustic-Driven Artificial Potential Field for Low-Noise Multi-UAV Path Planning.” Proceedings of the 31st International Congress on Sound and Vibration (ICSV31), Society of Acoustics, 20…","meta":"Conference paper · 2025","search_text":"acoustic-driven artificial potential field for low-noise multi-uav path planning tan, qichen; dun, yuzhe; he, jiahua; bao, hongsen; chen, wangqiao; zhou, peng; zhang, xin. “acoustic-driven artificial potential field for low-noise multi-uav path planning.” proceedings of the 31st international congress on sound and vibration (icsv31), society of acoustics, 2025, p. 2715-2723. (2025). conference paper · 2025 tan, qichen; dun, yuzhe; he, jiahua; bao, hongsen; chen, wangqiao; zhou, peng; zhang, xin 2025 proceedings of the 31st international congress on sound and vibration (icsv31), society of acoustics, 2025, p. 2715-2723 2715-2723","order":131,"static_url":"/publications/180/"},{"section":"Publications","title":"A Computational Aeroacoustic Study of a Drone Rotor in Forward Flight with Flapping Motion","url":"/publications/179/","summary":"Zhang, Zhicheng; Peng, Zhenjun; Li, Xiangtian; Chen, Wangqiao; Zhou, Peng; Zhang, Xin. “A Computational Aeroacoustic Study of a Drone Rotor in Forward Flight with Flapping Motion.” Proceedings of the 31st International Congress on Sound and Vibration (ICSV31), Society of Acousti…","meta":"Conference paper · 2025","search_text":"a computational aeroacoustic study of a drone rotor in forward flight with flapping motion zhang, zhicheng; peng, zhenjun; li, xiangtian; chen, wangqiao; zhou, peng; zhang, xin. “a computational aeroacoustic study of a drone rotor in forward flight with flapping motion.” proceedings of the 31st international congress on sound and vibration (icsv31), society of acoustics, 2025, p. 1269-1276. (2025). conference paper · 2025 zhang, zhicheng; peng, zhenjun; li, xiangtian; chen, wangqiao; zhou, peng; zhang, xin 2025 proceedings of the 31st international congress on sound and vibration (icsv31), society of acoustics, 2025, p. 1269-1276 1269-1276","order":132,"static_url":"/publications/179/"},{"section":"Publications","title":"Transient Aeroacoustic Analysis of Pitching Wing at Low Reynolds Number","url":"/publications/178/","summary":"Chen, Wangqiao; Zhou, Peng; Zhong, Siyang; Zhang, Xin. “Transient Aeroacoustic Analysis of Pitching Wing at Low Reynolds Number.” Flinovia-Flow Induced Noise and Vibration Issues and Aspects-IV / Springer Nature, 2025, p. 87-102 (2025). DOI: 10.1007/978-3-031-73935-4_5.","meta":"Book chapter · 2025","search_text":"transient aeroacoustic analysis of pitching wing at low reynolds number chen, wangqiao; zhou, peng; zhong, siyang; zhang, xin. “transient aeroacoustic analysis of pitching wing at low reynolds number.” flinovia-flow induced noise and vibration issues and aspects-iv / springer nature, 2025, p. 87-102 (2025). doi: 10.1007/978-3-031-73935-4_5. book chapter · 2025 chen, wangqiao; zhou, peng; zhong, siyang; zhang, xin 2025 10.1007/978-3-031-73935-4_5 flinovia-flow induced noise and vibration issues and aspects-iv / springer nature, 2025, p. 87-102","order":133,"static_url":"/publications/178/"},{"section":"Publications","title":"On the Gaussian beam tracing method for long-distance sound wave propagation in non-uniform mean flows","url":"/publications/177/","summary":"BAO, Hongsen; Tan, Qichen; ZHOU, Peng; CHEN, Wangqiao; ZHANG, Xin; Zhong, Siyang. “On the Gaussian beam tracing method for long-distance sound wave propagation in non-uniform mean flows.” Proceedings of the Royal Society A: Mathematical, Physical and Engineering Sciences, v. 481…","meta":"Journal article · 2025","search_text":"on the gaussian beam tracing method for long-distance sound wave propagation in non-uniform mean flows bao, hongsen; tan, qichen; zhou, peng; chen, wangqiao; zhang, xin; zhong, siyang. “on the gaussian beam tracing method for long-distance sound wave propagation in non-uniform mean flows.” proceedings of the royal society a: mathematical, physical and engineering sciences, v. 481, (2307), article number 20240485. (2025). doi: 10.1098/rspa.2024.0485. journal article · 2025 bao, hongsen; tan, qichen; zhou, peng; chen, wangqiao; zhang, xin; zhong, siyang 2025 10.1098/rspa.2024.0485 proceedings of the royal society a: mathematical, physical and engineering sciences 481 (2307) article 20240485","order":134,"static_url":"/publications/177/"},{"section":"Publications","title":"Machine learning-based prediction of drone noise propagation in three-dimensional urban environments","url":"/publications/176/","summary":"He, Jiahua; Tan, Qichen; Bao, Hongsen; Li, Yuhong; Chen, Wangqiao; Zhou, Peng; Zhang, Xin. “Machine learning-based prediction of drone noise propagation in three-dimensional urban environments.” Journal of the Acoustical Society of America, v. 158, (2), p. 946-957. (2025). DOI: …","meta":"Journal article · 2025","search_text":"machine learning-based prediction of drone noise propagation in three-dimensional urban environments he, jiahua; tan, qichen; bao, hongsen; li, yuhong; chen, wangqiao; zhou, peng; zhang, xin. “machine learning-based prediction of drone noise propagation in three-dimensional urban environments.” journal of the acoustical society of america, v. 158, (2), p. 946-957. (2025). doi: 10.1121/10.0038749. journal article · 2025 he, jiahua; tan, qichen; bao, hongsen; li, yuhong; chen, wangqiao; zhou, peng; zhang, xin 2025 10.1121/10.0038749 journal of the acoustical society of america 158 (2) 946-957","order":135,"static_url":"/publications/176/"},{"section":"Publications","title":"Inshore sailing route optimization integrating terrain-influenced wind field","url":"/publications/175/","summary":"Hou, Jiafan; Tan, Qichen; Wang, Zilu; Pui Mok, Kwan; Zhou, Peng; Zhang, Xin. “Inshore sailing route optimization integrating terrain-influenced wind field.” Ocean Engineering, v. 326, article number 120848. (2025). DOI: 10.1016/j.oceaneng.2025.120848.","meta":"Journal article · 2025","search_text":"inshore sailing route optimization integrating terrain-influenced wind field hou, jiafan; tan, qichen; wang, zilu; pui mok, kwan; zhou, peng; zhang, xin. “inshore sailing route optimization integrating terrain-influenced wind field.” ocean engineering, v. 326, article number 120848. (2025). doi: 10.1016/j.oceaneng.2025.120848. journal article · 2025 hou, jiafan; tan, qichen; wang, zilu; pui mok, kwan; zhou, peng; zhang, xin 2025 10.1016/j.oceaneng.2025.120848 ocean engineering 326 article 120848","order":136,"static_url":"/publications/175/"},{"section":"Publications","title":"Experimental study of the multiple tones in trailing edge noise of an aerofoil at low-to-moderate Reynolds number","url":"/publications/174/","summary":"Li, Xiangtian; Chen, Wangqiao; Zhou, Peng; Huang, Xun; Zhang, Xin. “Experimental study of the multiple tones in trailing edge noise of an aerofoil at low-to-moderate Reynolds number.” Journal of Sound and Vibration, v. 596, article number 118802. (2025). DOI: 10.1016/j.jsv.2024.…","meta":"Journal article · 2025","search_text":"experimental study of the multiple tones in trailing edge noise of an aerofoil at low-to-moderate reynolds number li, xiangtian; chen, wangqiao; zhou, peng; huang, xun; zhang, xin. “experimental study of the multiple tones in trailing edge noise of an aerofoil at low-to-moderate reynolds number.” journal of sound and vibration, v. 596, article number 118802. (2025). doi: 10.1016/j.jsv.2024.118802. journal article · 2025 li, xiangtian; chen, wangqiao; zhou, peng; huang, xun; zhang, xin 2025 10.1016/j.jsv.2024.118802 journal of sound and vibration 596 article 118802","order":137,"static_url":"/publications/174/"},{"section":"Publications","title":"Effect of rotation speed fluctuation on rotor noise generation: A numerical and experimental study","url":"/publications/173/","summary":"Li, Yuhong; Ma, Zhida; Qu, Renhao; Tan, Qichen; Zhong, Siyang; Zhou, Peng; Zhang, Xin. “Effect of rotation speed fluctuation on rotor noise generation: A numerical and experimental study.” Journal of Sound and Vibration, v. 595, article number 118717. (2025). DOI: 10.1016/j.jsv.…","meta":"Journal article · 2025","search_text":"effect of rotation speed fluctuation on rotor noise generation: a numerical and experimental study li, yuhong; ma, zhida; qu, renhao; tan, qichen; zhong, siyang; zhou, peng; zhang, xin. “effect of rotation speed fluctuation on rotor noise generation: a numerical and experimental study.” journal of sound and vibration, v. 595, article number 118717. (2025). doi: 10.1016/j.jsv.2024.118717. journal article · 2025 li, yuhong; ma, zhida; qu, renhao; tan, qichen; zhong, siyang; zhou, peng; zhang, xin 2025 10.1016/j.jsv.2024.118717 journal of sound and vibration 595 article 118717","order":138,"static_url":"/publications/173/"},{"section":"Publications","title":"Design and performance of a high-fidelity grazing flow tube facility for the investigation of acoustic liners","url":"/publications/172/","summary":"YI, Wei; Guo, Jingwen; QU, Renhao; FANG, Yi; Zhong, Siyang; ZHOU, Peng; ZHANG, Xin. “Design and performance of a high-fidelity grazing flow tube facility for the investigation of acoustic liners.” Applied Acoustics, v. 231, article number 110501. (2025). DOI: 10.1016/j.apacoust.…","meta":"Journal article · 2025","search_text":"design and performance of a high-fidelity grazing flow tube facility for the investigation of acoustic liners yi, wei; guo, jingwen; qu, renhao; fang, yi; zhong, siyang; zhou, peng; zhang, xin. “design and performance of a high-fidelity grazing flow tube facility for the investigation of acoustic liners.” applied acoustics, v. 231, article number 110501. (2025). doi: 10.1016/j.apacoust.2024.110501. journal article · 2025 yi, wei; guo, jingwen; qu, renhao; fang, yi; zhong, siyang; zhou, peng; zhang, xin 2025 10.1016/j.apacoust.2024.110501 applied acoustics 231 article 110501","order":139,"static_url":"/publications/172/"},{"section":"Publications","title":"Broadband Noise of a Hovering Rotor: Measurement, Prediction, and Reduction","url":"/publications/171/","summary":"Wu, Han; Zhou, Peng; Zhang, Xin; Wang, Puyuan; Zhou, Guocheng; Chen, Bao; Zhong, Siyang. “Broadband Noise of a Hovering Rotor: Measurement, Prediction, and Reduction.” AIAA Journal, v. 63, (8), p. 3275-3287. (2025). DOI: 10.2514/1.j064974.","meta":"Journal article · 2025","search_text":"broadband noise of a hovering rotor: measurement, prediction, and reduction wu, han; zhou, peng; zhang, xin; wang, puyuan; zhou, guocheng; chen, bao; zhong, siyang. “broadband noise of a hovering rotor: measurement, prediction, and reduction.” aiaa journal, v. 63, (8), p. 3275-3287. (2025). doi: 10.2514/1.j064974. journal article · 2025 wu, han; zhou, peng; zhang, xin; wang, puyuan; zhou, guocheng; chen, bao; zhong, siyang 2025 10.2514/1.j064974 aiaa journal 63 (8) 3275-3287","order":140,"static_url":"/publications/171/"},{"section":"Publications","title":"Aerodynamic characterisation of isolated cycling wheels","url":"/publications/170/","summary":"MAO, Jiaqi; ZHOU, Peng; YI, Wei; ZHANG, Xin. “Aerodynamic characterisation of isolated cycling wheels.” Experimental Thermal and Fluid Science, v. 164, (111423), article number 111423. (2025). DOI: 10.1016/j.expthermflusci.2025.111423.","meta":"Journal article · 2025","search_text":"aerodynamic characterisation of isolated cycling wheels mao, jiaqi; zhou, peng; yi, wei; zhang, xin. “aerodynamic characterisation of isolated cycling wheels.” experimental thermal and fluid science, v. 164, (111423), article number 111423. (2025). doi: 10.1016/j.expthermflusci.2025.111423. journal article · 2025 mao, jiaqi; zhou, peng; yi, wei; zhang, xin 2025 10.1016/j.expthermflusci.2025.111423 experimental thermal and fluid science 164 (111423) article 111423","order":141,"static_url":"/publications/170/"},{"section":"Publications","title":"A hybrid multilevel fast multipole and equivalent source method for aeroacoustic scattering prediction","url":"/publications/161/","summary":"Wang, Lican; Zhong, Siyang; Chen, Bao; ZHOU, Peng; Chen, Wangqiao; ZHANG, Xin. “A hybrid multilevel fast multipole and equivalent source method for aeroacoustic scattering prediction.” Journal of Sound and Vibration, v. 607, article number 119033. (2025). DOI: 10.1016/j.jsv.2025…","meta":"Journal article · 2025","search_text":"a hybrid multilevel fast multipole and equivalent source method for aeroacoustic scattering prediction wang, lican; zhong, siyang; chen, bao; zhou, peng; chen, wangqiao; zhang, xin. “a hybrid multilevel fast multipole and equivalent source method for aeroacoustic scattering prediction.” journal of sound and vibration, v. 607, article number 119033. (2025). doi: 10.1016/j.jsv.2025.119033. journal article · 2025 wang, lican; zhong, siyang; chen, bao; zhou, peng; chen, wangqiao; zhang, xin 2025 10.1016/j.jsv.2025.119033 journal of sound and vibration 607 article 119033","order":142,"static_url":"/publications/161/"},{"section":"Publications","title":"Numerical and Experimental Investigation of the Effect of Rotation Speed Fluctuations on the Rotor Noise for Unmanned Aircraft Systems","url":"/publications/449/","summary":"Yuhong Li; Zhida Ma; Renhao Qu; Peng Zhou; Siyang Zhong; Xin Zhang. “Numerical and Experimental Investigation of the Effect of Rotation Speed Fluctuations on the Rotor Noise for Unmanned Aircraft Systems.” (2024). DOI: 10.2514/6.2024-3216.","meta":"Conference paper · 2024","search_text":"numerical and experimental investigation of the effect of rotation speed fluctuations on the rotor noise for unmanned aircraft systems yuhong li; zhida ma; renhao qu; peng zhou; siyang zhong; xin zhang. “numerical and experimental investigation of the effect of rotation speed fluctuations on the rotor noise for unmanned aircraft systems.” (2024). doi: 10.2514/6.2024-3216. conference paper · 2024 yuhong li; zhida ma; renhao qu; peng zhou; siyang zhong; xin zhang 2024 10.2514/6.2024-3216","order":143,"static_url":"/publications/449/"},{"section":"Publications","title":"Low-noise multi-agent intelligent navigation for unmanned aircraft systems","url":"/publications/448/","summary":"Qichen Tan; Yuhong Li; Hongsen Bao; Jiahua He; Peng Zhou; Xin Zhang; Hong Kam Lo; Siyang Zhong. “Low-noise multi-agent intelligent navigation for unmanned aircraft systems.” (2024). DOI: 10.2514/6.2024-3234.","meta":"Conference paper · 2024","search_text":"low-noise multi-agent intelligent navigation for unmanned aircraft systems qichen tan; yuhong li; hongsen bao; jiahua he; peng zhou; xin zhang; hong kam lo; siyang zhong. “low-noise multi-agent intelligent navigation for unmanned aircraft systems.” (2024). doi: 10.2514/6.2024-3234. conference paper · 2024 qichen tan; yuhong li; hongsen bao; jiahua he; peng zhou; xin zhang; hong kam lo; siyang zhong 2024 10.2514/6.2024-3234","order":144,"static_url":"/publications/448/"},{"section":"Publications","title":"Experimental study on the reflection of sound waves at different incident angles by acoustic metasurface in a grazing flow","url":"/publications/447/","summary":"Renhao Qu; Jingwen Guo; Yi Fang; Wei Yi; Peng Zhou; Wangqiao Chen; Xin Zhang. “Experimental study on the reflection of sound waves at different incident angles by acoustic metasurface in a grazing flow.” (2024). DOI: 10.2514/6.2024-3352.","meta":"Conference paper · 2024","search_text":"experimental study on the reflection of sound waves at different incident angles by acoustic metasurface in a grazing flow renhao qu; jingwen guo; yi fang; wei yi; peng zhou; wangqiao chen; xin zhang. “experimental study on the reflection of sound waves at different incident angles by acoustic metasurface in a grazing flow.” (2024). doi: 10.2514/6.2024-3352. conference paper · 2024 renhao qu; jingwen guo; yi fang; wei yi; peng zhou; wangqiao chen; xin zhang 2024 10.2514/6.2024-3352","order":145,"static_url":"/publications/447/"},{"section":"Publications","title":"Experimental investigation of the flow and acoustic characteristics of a ducted propeller with incoming flow","url":"/publications/446/","summary":"Sinforiano Cantos; Han Wu; Xiangtian Li; Wangqiao Chen; Peng Zhou; Xin Zhang; Xun Huang; Siyang Zhong. “Experimental investigation of the flow and acoustic characteristics of a ducted propeller with incoming flow.” (2024).","meta":"Conference paper · 2024","search_text":"experimental investigation of the flow and acoustic characteristics of a ducted propeller with incoming flow sinforiano cantos; han wu; xiangtian li; wangqiao chen; peng zhou; xin zhang; xun huang; siyang zhong. “experimental investigation of the flow and acoustic characteristics of a ducted propeller with incoming flow.” (2024). conference paper · 2024 sinforiano cantos; han wu; xiangtian li; wangqiao chen; peng zhou; xin zhang; xun huang; siyang zhong 2024","order":146,"static_url":"/publications/446/"},{"section":"Publications","title":"Experimental and Modelling Characterization of the Broadband Noise of a Rotor in Hover","url":"/publications/445/","summary":"Han Wu; Zhicheng Zhang; Zhenjun Peng; Wangqiao Chen; Peng Zhou; Xin Zhang; Siyang Zhong; Bao Chen; Guocheng Zhou. “Experimental and Modelling Characterization of the Broadband Noise of a Rotor in Hover.” (2024).","meta":"Conference paper · 2024","search_text":"experimental and modelling characterization of the broadband noise of a rotor in hover han wu; zhicheng zhang; zhenjun peng; wangqiao chen; peng zhou; xin zhang; siyang zhong; bao chen; guocheng zhou. “experimental and modelling characterization of the broadband noise of a rotor in hover.” (2024). conference paper · 2024 han wu; zhicheng zhang; zhenjun peng; wangqiao chen; peng zhou; xin zhang; siyang zhong; bao chen; guocheng zhou 2024","order":147,"static_url":"/publications/445/"},{"section":"Publications","title":"Experimental analysis of the transient aeroacoustic interaction of coaxial contra-rotating rotors","url":"/publications/444/","summary":"Zhida Ma; Wangqiao Chen; Guangsheng Liu; Han Wu; Peng Zhou; Xin Zhang; Siyang Zhong. “Experimental analysis of the transient aeroacoustic interaction of coaxial contra-rotating rotors.” (2024).","meta":"Conference paper · 2024","search_text":"experimental analysis of the transient aeroacoustic interaction of coaxial contra-rotating rotors zhida ma; wangqiao chen; guangsheng liu; han wu; peng zhou; xin zhang; siyang zhong. “experimental analysis of the transient aeroacoustic interaction of coaxial contra-rotating rotors.” (2024). conference paper · 2024 zhida ma; wangqiao chen; guangsheng liu; han wu; peng zhou; xin zhang; siyang zhong 2024","order":148,"static_url":"/publications/444/"},{"section":"Publications","title":"Enhancing broadband noise prediction of a hovering rotor with an empirical wall-pressure spectrum model","url":"/publications/443/","summary":"Zhicheng Zhang; Jiahua He; Xiangtian Li; Yuhong Li; Peng Zhou; Xin Zhang; Xun Huang. “Enhancing broadband noise prediction of a hovering rotor with an empirical wall-pressure spectrum model.” (2024).","meta":"Conference paper · 2024","search_text":"enhancing broadband noise prediction of a hovering rotor with an empirical wall-pressure spectrum model zhicheng zhang; jiahua he; xiangtian li; yuhong li; peng zhou; xin zhang; xun huang. “enhancing broadband noise prediction of a hovering rotor with an empirical wall-pressure spectrum model.” (2024). conference paper · 2024 zhicheng zhang; jiahua he; xiangtian li; yuhong li; peng zhou; xin zhang; xun huang 2024","order":149,"static_url":"/publications/443/"},{"section":"Publications","title":"Exploring the influence of winds in urban region on sound propagation and low-noise path planning of urban air mobility","url":"/publications/205/","summary":"Tan, Qichen; Bao, Hongsen; Wang, Zilu; Li, Yuhong; Zhou, Peng; Luo, Hongyu; Zhong, siyang; Zhang, Xin. “Exploring the influence of winds in urban region on sound propagation and low-noise path planning of urban air mobility.” Paper presented at Quiet Drones 2024. (2024).","meta":"Conference paper · 2024","search_text":"exploring the influence of winds in urban region on sound propagation and low-noise path planning of urban air mobility tan, qichen; bao, hongsen; wang, zilu; li, yuhong; zhou, peng; luo, hongyu; zhong, siyang; zhang, xin. “exploring the influence of winds in urban region on sound propagation and low-noise path planning of urban air mobility.” paper presented at quiet drones 2024. (2024). conference paper · 2024 tan, qichen; bao, hongsen; wang, zilu; li, yuhong; zhou, peng; luo, hongyu; zhong, siyang; zhang, xin 2024 paper presented at quiet drones 2024","order":150,"static_url":"/publications/205/"},{"section":"Publications","title":"Experimental study of aeroacoustics and boundary layer transition of a lifting rotor during forward flight","url":"/publications/204/","summary":"Li, Xiangtian; Wu, Han; Zhou, Peng; Chen, Wangqiao; Zhang, Xin; Chen, Bao; Wang, Puyuan; Huang, Xun; Zhong, Siyang. “Experimental study of aeroacoustics and boundary layer transition of a lifting rotor during forward flight.” Paper presented at Proceedings of the 30th Internatio…","meta":"Conference paper · 2024","search_text":"experimental study of aeroacoustics and boundary layer transition of a lifting rotor during forward flight li, xiangtian; wu, han; zhou, peng; chen, wangqiao; zhang, xin; chen, bao; wang, puyuan; huang, xun; zhong, siyang. “experimental study of aeroacoustics and boundary layer transition of a lifting rotor during forward flight.” paper presented at proceedings of the 30th international congress on sound and vibration. (2024). conference paper · 2024 li, xiangtian; wu, han; zhou, peng; chen, wangqiao; zhang, xin; chen, bao; wang, puyuan; huang, xun; zhong, siyang 2024 paper presented at proceedings of the 30th international congress on sound and vibration","order":151,"static_url":"/publications/204/"},{"section":"Publications","title":"Effect of Sail Rig-back Angle in Windsurfing Sailing","url":"/publications/203/","summary":"Chan, King Yin; So, Chi-Hung; Song, Wenbin; Hou, Jiafan; Mok, Kwan Pui; Zhang, Xin; Zhou, Peng. “Effect of Sail Rig-back Angle in Windsurfing Sailing.” Paper presented at 8th High Performance Yacht Design Conference (HPYD 8). (2024).","meta":"Conference paper · 2024","search_text":"effect of sail rig-back angle in windsurfing sailing chan, king yin; so, chi-hung; song, wenbin; hou, jiafan; mok, kwan pui; zhang, xin; zhou, peng. “effect of sail rig-back angle in windsurfing sailing.” paper presented at 8th high performance yacht design conference (hpyd 8). (2024). conference paper · 2024 chan, king yin; so, chi-hung; song, wenbin; hou, jiafan; mok, kwan pui; zhang, xin; zhou, peng 2024 paper presented at 8th high performance yacht design conference (hpyd 8)","order":152,"static_url":"/publications/203/"},{"section":"Publications","title":"An Improved Gaussian Beam Tracing Method for the Long-distance Sound Wave Propagation in Non-uniform Mean Flows","url":"/publications/202/","summary":"Siyang, Zhong; Bao, Hongsen; Chen, Wangqiao; Xin, Zhang; Zhou, Peng. “An Improved Gaussian Beam Tracing Method for the Long-distance Sound Wave Propagation in Non-uniform Mean Flows.” Paper presented at The 30th International Congress on Sound and Vibration (ICSV30). (2024).","meta":"Conference paper · 2024","search_text":"an improved gaussian beam tracing method for the long-distance sound wave propagation in non-uniform mean flows siyang, zhong; bao, hongsen; chen, wangqiao; xin, zhang; zhou, peng. “an improved gaussian beam tracing method for the long-distance sound wave propagation in non-uniform mean flows.” paper presented at the 30th international congress on sound and vibration (icsv30). (2024). conference paper · 2024 siyang, zhong; bao, hongsen; chen, wangqiao; xin, zhang; zhou, peng 2024 paper presented at the 30th international congress on sound and vibration (icsv30)","order":153,"static_url":"/publications/202/"},{"section":"Publications","title":"Aerodynamic characterisation of isolated cycling wheels using load and flow field measurements","url":"/publications/201/","summary":"Mao, Jiaqi; Zhou, Peng; Yi, Wei; Zhang, Xin. “Aerodynamic characterisation of isolated cycling wheels using load and flow field measurements.” Paper presented at 1st European Fluid Dynamics Conference (EFDC1). (2024).","meta":"Conference paper · 2024","search_text":"aerodynamic characterisation of isolated cycling wheels using load and flow field measurements mao, jiaqi; zhou, peng; yi, wei; zhang, xin. “aerodynamic characterisation of isolated cycling wheels using load and flow field measurements.” paper presented at 1st european fluid dynamics conference (efdc1). (2024). conference paper · 2024 mao, jiaqi; zhou, peng; yi, wei; zhang, xin 2024 paper presented at 1st european fluid dynamics conference (efdc1)","order":154,"static_url":"/publications/201/"},{"section":"Publications","title":"Aerodynamic and acoustic evaluation of a cylinder covered by stretched grooved fabric near critical Reynolds numbers","url":"/publications/200/","summary":"Li, Xiangru; Mao, Jiaqi; Chen, Wangqiao; Zhang, Xin; Zhou, Peng. “Aerodynamic and acoustic evaluation of a cylinder covered by stretched grooved fabric near critical Reynolds numbers.” 53rd International Congress and Exposition on Noise Control Engineering, Internoise 2024, Soci…","meta":"Conference paper · 2024","search_text":"aerodynamic and acoustic evaluation of a cylinder covered by stretched grooved fabric near critical reynolds numbers li, xiangru; mao, jiaqi; chen, wangqiao; zhang, xin; zhou, peng. “aerodynamic and acoustic evaluation of a cylinder covered by stretched grooved fabric near critical reynolds numbers.” 53rd international congress and exposition on noise control engineering, internoise 2024, societe francaise d'acoustique, 2024, p. 5724-5733. (2024). doi: 10.3397/in_2024_3638. conference paper · 2024 li, xiangru; mao, jiaqi; chen, wangqiao; zhang, xin; zhou, peng 2024 10.3397/in_2024_3638 53rd international congress and exposition on noise control engineering, internoise 2024, societe francaise d'acoustique, 2024, p. 5724-5733 5724-5733","order":155,"static_url":"/publications/200/"},{"section":"Publications","title":"A Hierarchical Approach for Windsurfing Performance Analysis and Velocity Prediction","url":"/publications/199/","summary":"Chan, King Yin; So, Chi-Hung; Song, Wenbin; Tan, Qichen; Hou, Jiafan; Mok, Kwan Pui; Zhang, Xin; Zhou, Peng. “A Hierarchical Approach for Windsurfing Performance Analysis and Velocity Prediction.” Paper presented at 8th High Performance Yacht Design Conference (HPYD 8). (2024).","meta":"Conference paper · 2024","search_text":"a hierarchical approach for windsurfing performance analysis and velocity prediction chan, king yin; so, chi-hung; song, wenbin; tan, qichen; hou, jiafan; mok, kwan pui; zhang, xin; zhou, peng. “a hierarchical approach for windsurfing performance analysis and velocity prediction.” paper presented at 8th high performance yacht design conference (hpyd 8). (2024). conference paper · 2024 chan, king yin; so, chi-hung; song, wenbin; tan, qichen; hou, jiafan; mok, kwan pui; zhang, xin; zhou, peng 2024 paper presented at 8th high performance yacht design conference (hpyd 8)","order":156,"static_url":"/publications/199/"},{"section":"Publications","title":"Velocity prediction program for windsurfing: A hierarchical approach integrating biomechanical insights","url":"/publications/198/","summary":"Hou, Jiafan; Liu, Guangsheng; Tan, Qichen; Mok, Kwan Pui; Song, Wenbin; Chan, King Yin; So, Raymond Chi Hung; Zhou, Peng; Zhang, Xin. “Velocity prediction program for windsurfing: A hierarchical approach integrating biomechanical insights.” Ocean Engineering, v. 312, article num…","meta":"Journal article · 2024","search_text":"velocity prediction program for windsurfing: a hierarchical approach integrating biomechanical insights hou, jiafan; liu, guangsheng; tan, qichen; mok, kwan pui; song, wenbin; chan, king yin; so, raymond chi hung; zhou, peng; zhang, xin. “velocity prediction program for windsurfing: a hierarchical approach integrating biomechanical insights.” ocean engineering, v. 312, article number 119070. (2024). doi: 10.1016/j.oceaneng.2024.119070. journal article · 2024 hou, jiafan; liu, guangsheng; tan, qichen; mok, kwan pui; song, wenbin; chan, king yin; so, raymond chi hung; zhou, peng; zhang, xin 2024 10.1016/j.oceaneng.2024.119070 ocean engineering 312 article 119070","order":157,"static_url":"/publications/198/"},{"section":"Publications","title":"The influence of crosswinds and leg positions on cycling aerodynamics","url":"/publications/197/","summary":"Mao, Jiaqi; Zhou, Peng; Liu, Guangsheng; Zhong, Siyang; Huang, Xun; Zhang, Xin. “The influence of crosswinds and leg positions on cycling aerodynamics.” Experiments in Fluids, v. 65, (6), article number 85. (2024). DOI: 10.1007/s00348-024-03823-y.","meta":"Journal article · 2024","search_text":"the influence of crosswinds and leg positions on cycling aerodynamics mao, jiaqi; zhou, peng; liu, guangsheng; zhong, siyang; huang, xun; zhang, xin. “the influence of crosswinds and leg positions on cycling aerodynamics.” experiments in fluids, v. 65, (6), article number 85. (2024). doi: 10.1007/s00348-024-03823-y. journal article · 2024 mao, jiaqi; zhou, peng; liu, guangsheng; zhong, siyang; huang, xun; zhang, xin 2024 10.1007/s00348-024-03823-y experiments in fluids 65 (6) article 85","order":158,"static_url":"/publications/197/"},{"section":"Publications","title":"On the evolution of flow structures around a track cyclist","url":"/publications/196/","summary":"Zheng, Chuntai; Zhou, Peng; Mao, Xiaochen; Cantos, Sinforiano; Liu, Guangsheng; Zhang, Xin. “On the evolution of flow structures around a track cyclist.” Physics of Fluids, v. 36, (1), article number 015160. (2024). DOI: 10.1063/5.0188946.","meta":"Journal article · 2024","search_text":"on the evolution of flow structures around a track cyclist zheng, chuntai; zhou, peng; mao, xiaochen; cantos, sinforiano; liu, guangsheng; zhang, xin. “on the evolution of flow structures around a track cyclist.” physics of fluids, v. 36, (1), article number 015160. (2024). doi: 10.1063/5.0188946. journal article · 2024 zheng, chuntai; zhou, peng; mao, xiaochen; cantos, sinforiano; liu, guangsheng; zhang, xin 2024 10.1063/5.0188946 physics of fluids 36 (1) article 015160","order":159,"static_url":"/publications/196/"},{"section":"Publications","title":"Numerical simulation of windsurfing sail aerodynamics: Insights into forces and flow characteristics","url":"/publications/195/","summary":"Hou, Jiafan; Mok, Kwan Pui; Cantos, Sinforiano; Bertin, Celia; Chan, King Yin; Zhou, Peng; Zhong, Siyang; Zhang, Xin. “Numerical simulation of windsurfing sail aerodynamics: Insights into forces and flow characteristics.” Ocean Engineering, v. 300, article number 117477. (2024).…","meta":"Journal article · 2024","search_text":"numerical simulation of windsurfing sail aerodynamics: insights into forces and flow characteristics hou, jiafan; mok, kwan pui; cantos, sinforiano; bertin, celia; chan, king yin; zhou, peng; zhong, siyang; zhang, xin. “numerical simulation of windsurfing sail aerodynamics: insights into forces and flow characteristics.” ocean engineering, v. 300, article number 117477. (2024). doi: 10.1016/j.oceaneng.2024.117477. journal article · 2024 hou, jiafan; mok, kwan pui; cantos, sinforiano; bertin, celia; chan, king yin; zhou, peng; zhong, siyang; zhang, xin 2024 10.1016/j.oceaneng.2024.117477 ocean engineering 300 article 117477","order":160,"static_url":"/publications/195/"},{"section":"Publications","title":"Low-noise flight path planning of drones based on a virtual flight noise simulator: a vehicle routing problem","url":"/publications/194/","summary":"TAN, Qichen; Zhong, Siyang; QU, Renhao; LI, Yuhong; Zhou, Peng; Lo, Hong Kam; Zhang, Xin. “Low-noise flight path planning of drones based on a virtual flight noise simulator: a vehicle routing problem.” IEEE Intelligent Transportation Systems Magazine, v. 16, (6), p. 56-71, arti…","meta":"Journal article · 2024","search_text":"low-noise flight path planning of drones based on a virtual flight noise simulator: a vehicle routing problem tan, qichen; zhong, siyang; qu, renhao; li, yuhong; zhou, peng; lo, hong kam; zhang, xin. “low-noise flight path planning of drones based on a virtual flight noise simulator: a vehicle routing problem.” ieee intelligent transportation systems magazine, v. 16, (6), p. 56-71, article number 10540653. (2024). doi: 10.1109/mits.2024.3396430. journal article · 2024 tan, qichen; zhong, siyang; qu, renhao; li, yuhong; zhou, peng; lo, hong kam; zhang, xin 2024 10.1109/mits.2024.3396430 ieee intelligent transportation systems magazine 16 (6) 56-71; article 10540653","order":161,"static_url":"/publications/194/"},{"section":"Publications","title":"Exploring noise reduction strategies: Optimizing drone station placement for last-mile delivery","url":"/publications/193/","summary":"Tan, Qichen; Hou, Jiafan; Li, Yuhong; Qu, Renhao; Zhou, Peng; Zhong, Siyang; Lo, Hong Kam; Zhang, Xin. “Exploring noise reduction strategies: Optimizing drone station placement for last-mile delivery.” Transportation Research Part D: Transport and Environment, v. 133, article nu…","meta":"Journal article · 2024","search_text":"exploring noise reduction strategies: optimizing drone station placement for last-mile delivery tan, qichen; hou, jiafan; li, yuhong; qu, renhao; zhou, peng; zhong, siyang; lo, hong kam; zhang, xin. “exploring noise reduction strategies: optimizing drone station placement for last-mile delivery.” transportation research part d: transport and environment, v. 133, article number 104306. (2024). doi: 10.1016/j.trd.2024.104306. journal article · 2024 tan, qichen; hou, jiafan; li, yuhong; qu, renhao; zhou, peng; zhong, siyang; lo, hong kam; zhang, xin 2024 10.1016/j.trd.2024.104306 transportation research part d: transport and environment 133 article 104306","order":162,"static_url":"/publications/193/"},{"section":"Publications","title":"Experimental study of the turbulence ingestion noise of rotor blades","url":"/publications/192/","summary":"Wu, Han; Li, Yuhong; Zhang, Xin; Zhong, Siyang; Huang, Xun. “Experimental study of the turbulence ingestion noise of rotor blades.” Physical Review Fluids, v. 9, (4), article number 044801. (2024). DOI: 10.1103/physrevfluids.9.044801.","meta":"Journal article · 2024","search_text":"experimental study of the turbulence ingestion noise of rotor blades wu, han; li, yuhong; zhang, xin; zhong, siyang; huang, xun. “experimental study of the turbulence ingestion noise of rotor blades.” physical review fluids, v. 9, (4), article number 044801. (2024). doi: 10.1103/physrevfluids.9.044801. journal article · 2024 wu, han; li, yuhong; zhang, xin; zhong, siyang; huang, xun 2024 10.1103/physrevfluids.9.044801 physical review fluids 9 (4) article 044801","order":163,"static_url":"/publications/192/"},{"section":"Publications","title":"Experimental investigations on the effects of longitudinal groove fabric for drag reductions on a track cyclist","url":"/publications/191/","summary":"Zheng, Chuntai; Zhou, Peng; Mao, Jiaqi; Zhang, Xin. “Experimental investigations on the effects of longitudinal groove fabric for drag reductions on a track cyclist.” Experimental Thermal and Fluid Science, v. 156, article number 111223. (2024). DOI: 10.1016/j.expthermflusci.202…","meta":"Journal article · 2024","search_text":"experimental investigations on the effects of longitudinal groove fabric for drag reductions on a track cyclist zheng, chuntai; zhou, peng; mao, jiaqi; zhang, xin. “experimental investigations on the effects of longitudinal groove fabric for drag reductions on a track cyclist.” experimental thermal and fluid science, v. 156, article number 111223. (2024). doi: 10.1016/j.expthermflusci.2024.111223. journal article · 2024 zheng, chuntai; zhou, peng; mao, jiaqi; zhang, xin 2024 10.1016/j.expthermflusci.2024.111223 experimental thermal and fluid science 156 article 111223","order":164,"static_url":"/publications/191/"},{"section":"Publications","title":"Experimental investigation on the aerodynamics of a windsurfing sail under steady sailing conditions","url":"/publications/190/","summary":"Mok, Kwan Pui; Zhou, Peng; Liu, Guangsheng; Hou, Jiafan; Zhang, Xin; Chan, King Yin; Song, Wenbin. “Experimental investigation on the aerodynamics of a windsurfing sail under steady sailing conditions.” Ocean Engineering, v. 310, article number 118617. (2024). DOI: 10.1016/j.oce…","meta":"Journal article · 2024","search_text":"experimental investigation on the aerodynamics of a windsurfing sail under steady sailing conditions mok, kwan pui; zhou, peng; liu, guangsheng; hou, jiafan; zhang, xin; chan, king yin; song, wenbin. “experimental investigation on the aerodynamics of a windsurfing sail under steady sailing conditions.” ocean engineering, v. 310, article number 118617. (2024). doi: 10.1016/j.oceaneng.2024.118617. journal article · 2024 mok, kwan pui; zhou, peng; liu, guangsheng; hou, jiafan; zhang, xin; chan, king yin; song, wenbin 2024 10.1016/j.oceaneng.2024.118617 ocean engineering 310 article 118617","order":165,"static_url":"/publications/190/"},{"section":"Publications","title":"Experimental Assessment of the Flow Recirculation Effect on the Noise Measurement of a Free-Flying Multi-rotor UAS in a Closed Anechoic Chamber","url":"/publications/189/","summary":"Ma, Zhida; Zhou, Peng; Zhang, Xin; Zhong, Siyang. “Experimental Assessment of the Flow Recirculation Effect on the Noise Measurement of a Free-Flying Multi-rotor UAS in a Closed Anechoic Chamber.” Acoustics Australia, v. 52, (3), p. 313-322, article number 116330. (2024). DOI: 1…","meta":"Journal article · 2024","search_text":"experimental assessment of the flow recirculation effect on the noise measurement of a free-flying multi-rotor uas in a closed anechoic chamber ma, zhida; zhou, peng; zhang, xin; zhong, siyang. “experimental assessment of the flow recirculation effect on the noise measurement of a free-flying multi-rotor uas in a closed anechoic chamber.” acoustics australia, v. 52, (3), p. 313-322, article number 116330. (2024). doi: 10.1007/s40857-024-00327-x. journal article · 2024 ma, zhida; zhou, peng; zhang, xin; zhong, siyang 2024 10.1007/s40857-024-00327-x acoustics australia 52 (3) 313-322; article 116330","order":166,"static_url":"/publications/189/"},{"section":"Publications","title":"A Numerical Study of Cyclist-Cyclist Aerodynamic Interaction towards Efficient Overtaking Strategy","url":"/publications/188/","summary":"Cantos, Sinforiano; Mok, Kwan Pui; Zhou, Peng; Jiang, Hanbo; Mao, Xiaochen; Zhong, Siyang; Zhang, Xin. “A Numerical Study of Cyclist-Cyclist Aerodynamic Interaction towards Efficient Overtaking Strategy.” Journal of Fluids Engineering, Transactions of the ASME, v. 146, (2), arti…","meta":"Journal article · 2024","search_text":"a numerical study of cyclist-cyclist aerodynamic interaction towards efficient overtaking strategy cantos, sinforiano; mok, kwan pui; zhou, peng; jiang, hanbo; mao, xiaochen; zhong, siyang; zhang, xin. “a numerical study of cyclist-cyclist aerodynamic interaction towards efficient overtaking strategy.” journal of fluids engineering, transactions of the asme, v. 146, (2), article number 021202. (2024). doi: 10.1115/1.4063935. journal article · 2024 cantos, sinforiano; mok, kwan pui; zhou, peng; jiang, hanbo; mao, xiaochen; zhong, siyang; zhang, xin 2024 10.1115/1.4063935 journal of fluids engineering, transactions of the asme 146 (2) article 021202","order":167,"static_url":"/publications/188/"},{"section":"Publications","title":"Acoustic imaging of geometrically shielded sound sources using tailored Green's functions","url":"/publications/160/","summary":"Lican Wang, Zhenjun Peng, Bao Chen, Zhida Ma, Wangqiao Chen, Peng Zhou, Guocheng Zhou, Siyang Zhong; Acoustic imaging of geometrically shielded sound sources using tailored Green's functions. J. Acoust. Soc. Am. 1 November 2024; 156 (5): 3102–3111.","meta":"Journal article · 2024","search_text":"acoustic imaging of geometrically shielded sound sources using tailored green's functions lican wang, zhenjun peng, bao chen, zhida ma, wangqiao chen, peng zhou, guocheng zhou, siyang zhong; acoustic imaging of geometrically shielded sound sources using tailored green's functions. j. acoust. soc. am. 1 november 2024; 156 (5): 3102–3111. journal article · 2024 lican wang; zhenjun peng; bao chen; zhida ma; wangqiao chen; peng zhou; guocheng zhou; siyang zhong 2024 10.1121/10.0034353 the journal of the acoustical society of america 156 (5) 3102-3111","order":168,"static_url":"/publications/160/"},{"section":"Publications","title":"Experimental Study of the Effect of Boundary-Layer Transition on Rotor Aeroacoustics","url":"/publications/148/","summary":"Li, Xiangtian; Wu, Han; Li, Yuhong; Zhou, Peng; Zhong, Siyang; Zhang, Xin; Ma, Zhaokai. “Experimental Study of the Effect of Boundary-Layer Transition on Rotor Aeroacoustics.” AIAA Journal, v. 62, (5), p. 1974-1981. (2024). DOI: 10.2514/1.j063785.","meta":"Journal article · 2024","search_text":"experimental study of the effect of boundary-layer transition on rotor aeroacoustics li, xiangtian; wu, han; li, yuhong; zhou, peng; zhong, siyang; zhang, xin; ma, zhaokai. “experimental study of the effect of boundary-layer transition on rotor aeroacoustics.” aiaa journal, v. 62, (5), p. 1974-1981. (2024). doi: 10.2514/1.j063785. journal article · 2024 li, xiangtian; wu, han; li, yuhong; zhou, peng; zhong, siyang; zhang, xin; ma, zhaokai 2024 10.2514/1.j063785 aiaa journal 62 (5) 1974-1981","order":169,"static_url":"/publications/148/"},{"section":"Publications","title":"Enhancing sustainable urban air transportation: Low-noise UAS flight planning using noise assessment simulator","url":"/publications/147/","summary":"Tan, Qichen; Li, Yuhong; Wu, Han; Zhou, Peng; Lo, Hong Kam; Zhong, Siyang; Zhang, Xin. “Enhancing sustainable urban air transportation: Low-noise UAS flight planning using noise assessment simulator.” Aerospace Science and Technology, v. 147, article number 109071. (2024). DOI: …","meta":"Journal article · 2024","search_text":"enhancing sustainable urban air transportation: low-noise uas flight planning using noise assessment simulator tan, qichen; li, yuhong; wu, han; zhou, peng; lo, hong kam; zhong, siyang; zhang, xin. “enhancing sustainable urban air transportation: low-noise uas flight planning using noise assessment simulator.” aerospace science and technology, v. 147, article number 109071. (2024). doi: 10.1016/j.ast.2024.109071. journal article · 2024 tan, qichen; li, yuhong; wu, han; zhou, peng; lo, hong kam; zhong, siyang; zhang, xin 2024 10.1016/j.ast.2024.109071 aerospace science and technology 147 article 109071","order":170,"static_url":"/publications/147/"},{"section":"Publications","title":"Aerodynamics and aeroacoustics of ducted propellers: A study on the design and geometry effects","url":"/publications/146/","summary":"Cantos, Sinforiano; Zhou, Peng; Wu, Han; Ma, Zhida; Chen, Wangqiao; Zhong, Siyang; Zhang, Xin. “Aerodynamics and aeroacoustics of ducted propellers: A study on the design and geometry effects.” Physics of Fluids, v. 36, (3), article number 035116. (2024). DOI: 10.1063/5.0191323.","meta":"Journal article · 2024","search_text":"aerodynamics and aeroacoustics of ducted propellers: a study on the design and geometry effects cantos, sinforiano; zhou, peng; wu, han; ma, zhida; chen, wangqiao; zhong, siyang; zhang, xin. “aerodynamics and aeroacoustics of ducted propellers: a study on the design and geometry effects.” physics of fluids, v. 36, (3), article number 035116. (2024). doi: 10.1063/5.0191323. journal article · 2024 cantos, sinforiano; zhou, peng; wu, han; ma, zhida; chen, wangqiao; zhong, siyang; zhang, xin 2024 10.1063/5.0191323 physics of fluids 36 (3) article 035116","order":171,"static_url":"/publications/146/"},{"section":"Publications","title":"A numerical investigation of the aerodynamic and aeroacoustic interactions between components of a multi-rotor vehicle for urban air mobility","url":"/publications/145/","summary":"Li, Yuhong; Ma, Zhida; Zhou, Peng; Zhong, Siyang; Zhang, Xin. “A numerical investigation of the aerodynamic and aeroacoustic interactions between components of a multi-rotor vehicle for urban air mobility.” Journal of Sound and Vibration, v. 571, article number 118002. (2024). D…","meta":"Journal article · 2024","search_text":"a numerical investigation of the aerodynamic and aeroacoustic interactions between components of a multi-rotor vehicle for urban air mobility li, yuhong; ma, zhida; zhou, peng; zhong, siyang; zhang, xin. “a numerical investigation of the aerodynamic and aeroacoustic interactions between components of a multi-rotor vehicle for urban air mobility.” journal of sound and vibration, v. 571, article number 118002. (2024). doi: 10.1016/j.jsv.2023.118002. journal article · 2024 li, yuhong; ma, zhida; zhou, peng; zhong, siyang; zhang, xin 2024 10.1016/j.jsv.2023.118002 journal of sound and vibration 571 article 118002","order":172,"static_url":"/publications/145/"},{"section":"Publications","title":"Sound propagation in the presence of non-isothermal sheared flow refraction and metasurface impedance reflection","url":"/publications/144/","summary":"Wang, Lican; Qu, Renhao; Zhou, Peng; Zhang, Xin. “Sound propagation in the presence of non-isothermal sheared flow refraction and metasurface impedance reflection.” Journal of Sound and Vibration, v. 590, article number 118591. (2024). DOI: 10.1016/j.jsv.2024.118591.","meta":"Journal article · 2024","search_text":"sound propagation in the presence of non-isothermal sheared flow refraction and metasurface impedance reflection wang, lican; qu, renhao; zhou, peng; zhang, xin. “sound propagation in the presence of non-isothermal sheared flow refraction and metasurface impedance reflection.” journal of sound and vibration, v. 590, article number 118591. (2024). doi: 10.1016/j.jsv.2024.118591. journal article · 2024 wang, lican; qu, renhao; zhou, peng; zhang, xin 2024 10.1016/j.jsv.2024.118591 journal of sound and vibration 590 article 118591","order":173,"static_url":"/publications/144/"},{"section":"Publications","title":"Transient aeroacoustic analysis of a pitching airfoil at low Reynolds number","url":"/publications/224/","summary":"Zhong, Siyang; Chen, Wangqiao; Zhang, Xin; Zhou, Peng. “Transient aeroacoustic analysis of a pitching airfoil at low Reynolds number.” Paper presented at Flinovia IV Symposium. (2023).","meta":"Conference paper · 2023","search_text":"transient aeroacoustic analysis of a pitching airfoil at low reynolds number zhong, siyang; chen, wangqiao; zhang, xin; zhou, peng. “transient aeroacoustic analysis of a pitching airfoil at low reynolds number.” paper presented at flinovia iv symposium. (2023). conference paper · 2023 zhong, siyang; chen, wangqiao; zhang, xin; zhou, peng 2023 paper presented at flinovia iv symposium","order":174,"static_url":"/publications/224/"},{"section":"Publications","title":"Reflected wave manipulation by aeroacoustic metasurfaces in sheared grazing flows","url":"/publications/223/","summary":"Fang, Yi; Guo, Jingwen; Qu, Renhao; Yi, Wei; Zhang, Xin. “Reflected wave manipulation by aeroacoustic metasurfaces in sheared grazing flows.” Paper presented at 52nd International Congress and Exposition on Noise Control Engineering (INTER-NOISE 2023). (2023). DOI: 10.3397/in_20…","meta":"Conference paper · 2023","search_text":"reflected wave manipulation by aeroacoustic metasurfaces in sheared grazing flows fang, yi; guo, jingwen; qu, renhao; yi, wei; zhang, xin. “reflected wave manipulation by aeroacoustic metasurfaces in sheared grazing flows.” paper presented at 52nd international congress and exposition on noise control engineering (inter-noise 2023). (2023). doi: 10.3397/in_2023_0506. conference paper · 2023 fang, yi; guo, jingwen; qu, renhao; yi, wei; zhang, xin 2023 10.3397/in_2023_0506 paper presented at 52nd international congress and exposition on noise control engineering (inter-noise 2023)","order":175,"static_url":"/publications/223/"},{"section":"Publications","title":"On the multiple tones in trailing edge noise of an aerofoil at low-to-moderate Reynolds number flows","url":"/publications/222/","summary":"Huang, Xun; Zhong, Siyang; Chen, Wangqiao; Li, Xiangtian; Zhang, Xin. “On the multiple tones in trailing edge noise of an aerofoil at low-to-moderate Reynolds number flows.” Paper presented at 52nd International Congress and Exposition on Noise Control Engineering (INTER-NOISE 2…","meta":"Conference paper · 2023","search_text":"on the multiple tones in trailing edge noise of an aerofoil at low-to-moderate reynolds number flows huang, xun; zhong, siyang; chen, wangqiao; li, xiangtian; zhang, xin. “on the multiple tones in trailing edge noise of an aerofoil at low-to-moderate reynolds number flows.” paper presented at 52nd international congress and exposition on noise control engineering (inter-noise 2023). (2023). doi: 10.3397/in_2023_0591. conference paper · 2023 huang, xun; zhong, siyang; chen, wangqiao; li, xiangtian; zhang, xin 2023 10.3397/in_2023_0591 paper presented at 52nd international congress and exposition on noise control engineering (inter-noise 2023)","order":176,"static_url":"/publications/222/"},{"section":"Publications","title":"NONLINEAR SOUND ABSORPTION OF HELMHOLTZ RESONATORS WITH EXTENDED NECKS AT HIGH SOUND PRESSURE LEVELS","url":"/publications/221/","summary":"Qu, Renhao; Guo, Jingwen; Yi, Wei; Fang, Yi; Zhang, Xin; Zhong, Siyang. “NONLINEAR SOUND ABSORPTION OF HELMHOLTZ RESONATORS WITH EXTENDED NECKS AT HIGH SOUND PRESSURE LEVELS.” Proceedings of the 29th International Congress on Sound and Vibration, ICSV 2023 / edited by Carletti E…","meta":"Conference paper · 2023","search_text":"nonlinear sound absorption of helmholtz resonators with extended necks at high sound pressure levels qu, renhao; guo, jingwen; yi, wei; fang, yi; zhang, xin; zhong, siyang. “nonlinear sound absorption of helmholtz resonators with extended necks at high sound pressure levels.” proceedings of the 29th international congress on sound and vibration, icsv 2023 / edited by carletti eleonora. society of acoustics, 2023. (2023). conference paper · 2023 qu, renhao; guo, jingwen; yi, wei; fang, yi; zhang, xin; zhong, siyang 2023 proceedings of the 29th international congress on sound and vibration, icsv 2023 / edited by carletti eleonora. society of acoustics, 2023","order":177,"static_url":"/publications/221/"},{"section":"Publications","title":"Noise-aware UAS flight path planning based on virtual flight simulation","url":"/publications/220/","summary":"Zhong, Siyang; Bao, Hongsen; Lo, Hong Kam; Tan, Qichen; Zhang, Xin; Zhou, Peng. “Noise-aware UAS flight path planning based on virtual flight simulation.” Paper presented at 52nd International Congress and Exposition on Noise Control Engineering (INTER-NOISE 2023). (2023). DOI: …","meta":"Conference paper · 2023","search_text":"noise-aware uas flight path planning based on virtual flight simulation zhong, siyang; bao, hongsen; lo, hong kam; tan, qichen; zhang, xin; zhou, peng. “noise-aware uas flight path planning based on virtual flight simulation.” paper presented at 52nd international congress and exposition on noise control engineering (inter-noise 2023). (2023). doi: 10.3397/in_2023_0507. conference paper · 2023 zhong, siyang; bao, hongsen; lo, hong kam; tan, qichen; zhang, xin; zhou, peng 2023 10.3397/in_2023_0507 paper presented at 52nd international congress and exposition on noise control engineering (inter-noise 2023)","order":178,"static_url":"/publications/220/"},{"section":"Publications","title":"Noise assessment and low-noise flight path planning platform for urban air mobility","url":"/publications/219/","summary":"Bao, Hongsen; Li, Yuhong; Ma, Zhida; Tan, Qichen; Wu, Han; Zhang, Xin; Zhou, Peng. “Noise assessment and low-noise flight path planning platform for urban air mobility.” Paper presented at Acoustical Society of America Sydney Conference Acoustics 2023. (2023). DOI: 10.1121/10.00…","meta":"Conference paper · 2023","search_text":"noise assessment and low-noise flight path planning platform for urban air mobility bao, hongsen; li, yuhong; ma, zhida; tan, qichen; wu, han; zhang, xin; zhou, peng. “noise assessment and low-noise flight path planning platform for urban air mobility.” paper presented at acoustical society of america sydney conference acoustics 2023. (2023). doi: 10.1121/10.0023570. conference paper · 2023 bao, hongsen; li, yuhong; ma, zhida; tan, qichen; wu, han; zhang, xin; zhou, peng 2023 10.1121/10.0023570 paper presented at acoustical society of america sydney conference acoustics 2023","order":179,"static_url":"/publications/219/"},{"section":"Publications","title":"LOW-NOISE FLIGHT ROUTING PLANNING OF DRONES BASED ON A VIRTUAL FLIGHT NOISE SIMULATOR","url":"/publications/218/","summary":"Tan, Qichen; Zhou, Peng; Lo, Hong Kam; Zhang, Xin; Zhong, Siyang. “LOW-NOISE FLIGHT ROUTING PLANNING OF DRONES BASED ON A VIRTUAL FLIGHT NOISE SIMULATOR.” Proceedings of the 29th International Congress on Sound and Vibration, ICSV 2023 / edited by Carletti Eleonora. Society of A…","meta":"Conference paper · 2023","search_text":"low-noise flight routing planning of drones based on a virtual flight noise simulator tan, qichen; zhou, peng; lo, hong kam; zhang, xin; zhong, siyang. “low-noise flight routing planning of drones based on a virtual flight noise simulator.” proceedings of the 29th international congress on sound and vibration, icsv 2023 / edited by carletti eleonora. society of acoustics, 2023. (2023). conference paper · 2023 tan, qichen; zhou, peng; lo, hong kam; zhang, xin; zhong, siyang 2023 proceedings of the 29th international congress on sound and vibration, icsv 2023 / edited by carletti eleonora. society of acoustics, 2023","order":180,"static_url":"/publications/218/"},{"section":"Publications","title":"Low Mach number aeroacoustic computations of airfoils in application with Pierce's wave equation","url":"/publications/217/","summary":"Spieser, Etienne; Zhang, Xin. “Low Mach number aeroacoustic computations of airfoils in application with Pierce's wave equation.” Paper presented at 52nd International Congress and Exposition on Noise Control Engineering (INTER-NOISE 2023). (2023). DOI: 10.3397/in_2023_0234.","meta":"Conference paper · 2023","search_text":"low mach number aeroacoustic computations of airfoils in application with pierce's wave equation spieser, etienne; zhang, xin. “low mach number aeroacoustic computations of airfoils in application with pierce's wave equation.” paper presented at 52nd international congress and exposition on noise control engineering (inter-noise 2023). (2023). doi: 10.3397/in_2023_0234. conference paper · 2023 spieser, etienne; zhang, xin 2023 10.3397/in_2023_0234 paper presented at 52nd international congress and exposition on noise control engineering (inter-noise 2023)","order":181,"static_url":"/publications/217/"},{"section":"Publications","title":"Experimental investigation on the aeroacoustics of coaxial rotors","url":"/publications/216/","summary":"Chen, Bao; Wang, Puyuan; Zhou, Guocheng; Zhong, Siyang; Ma, Zhida; Liu, Guangsheng; Wu, Han; Zhang, Xin; Zhou, Peng. “Experimental investigation on the aeroacoustics of coaxial rotors.” Paper presented at 52nd International Congress and Exposition on Noise Control Engineering (I…","meta":"Conference paper · 2023","search_text":"experimental investigation on the aeroacoustics of coaxial rotors chen, bao; wang, puyuan; zhou, guocheng; zhong, siyang; ma, zhida; liu, guangsheng; wu, han; zhang, xin; zhou, peng. “experimental investigation on the aeroacoustics of coaxial rotors.” paper presented at 52nd international congress and exposition on noise control engineering (inter-noise 2023). (2023). doi: 10.3397/in_2023_0471. conference paper · 2023 chen, bao; wang, puyuan; zhou, guocheng; zhong, siyang; ma, zhida; liu, guangsheng; wu, han; zhang, xin; zhou, peng 2023 10.3397/in_2023_0471 paper presented at 52nd international congress and exposition on noise control engineering (inter-noise 2023)","order":182,"static_url":"/publications/216/"},{"section":"Publications","title":"COMPUTATIONAL INVESTIGATION OF THE EXPANSION EFFECT ON THE AERODYNAMICS AND AEROACOUSTICS OF DUCTED PROPELLERS","url":"/publications/215/","summary":"Cantos, Sinforiano; Zhou, Peng; Zhang, Xin; Zhong, Siyang. “COMPUTATIONAL INVESTIGATION OF THE EXPANSION EFFECT ON THE AERODYNAMICS AND AEROACOUSTICS OF DUCTED PROPELLERS.” Proceedings of the 29th International Congress on Sound and Vibration, ICSV 2023 / edited by Carletti Eleo…","meta":"Conference paper · 2023","search_text":"computational investigation of the expansion effect on the aerodynamics and aeroacoustics of ducted propellers cantos, sinforiano; zhou, peng; zhang, xin; zhong, siyang. “computational investigation of the expansion effect on the aerodynamics and aeroacoustics of ducted propellers.” proceedings of the 29th international congress on sound and vibration, icsv 2023 / edited by carletti eleonora. society of acoustics, 2023. (2023). conference paper · 2023 cantos, sinforiano; zhou, peng; zhang, xin; zhong, siyang 2023 proceedings of the 29th international congress on sound and vibration, icsv 2023 / edited by carletti eleonora. society of acoustics, 2023","order":183,"static_url":"/publications/215/"},{"section":"Publications","title":"An investigation of the noise characteristics of a small-scale rotor in axial descent","url":"/publications/214/","summary":"Huang, Xun; Li, Yuhong; Zhang, Xin; Zhou, Peng. “An investigation of the noise characteristics of a small-scale rotor in axial descent.” Paper presented at 52nd International Congress and Exposition on Noise Control Engineering (INTER-NOISE 2023). (2023). DOI: 10.3397/in_2023_04…","meta":"Conference paper · 2023","search_text":"an investigation of the noise characteristics of a small-scale rotor in axial descent huang, xun; li, yuhong; zhang, xin; zhou, peng. “an investigation of the noise characteristics of a small-scale rotor in axial descent.” paper presented at 52nd international congress and exposition on noise control engineering (inter-noise 2023). (2023). doi: 10.3397/in_2023_0418. conference paper · 2023 huang, xun; li, yuhong; zhang, xin; zhou, peng 2023 10.3397/in_2023_0418 paper presented at 52nd international congress and exposition on noise control engineering (inter-noise 2023)","order":184,"static_url":"/publications/214/"},{"section":"Publications","title":"An improved artificial compressibility method for aeroacoustics at low Mach numbers","url":"/publications/213/","summary":"Li, Yuhong; Spieser, Etienne; Zhang, Xin. “An improved artificial compressibility method for aeroacoustics at low Mach numbers.” Paper presented at 52nd International Congress and Exposition on Noise Control Engineering (INTER-NOISE 2023). (2023). DOI: 10.3397/in_2023_0437.","meta":"Conference paper · 2023","search_text":"an improved artificial compressibility method for aeroacoustics at low mach numbers li, yuhong; spieser, etienne; zhang, xin. “an improved artificial compressibility method for aeroacoustics at low mach numbers.” paper presented at 52nd international congress and exposition on noise control engineering (inter-noise 2023). (2023). doi: 10.3397/in_2023_0437. conference paper · 2023 li, yuhong; spieser, etienne; zhang, xin 2023 10.3397/in_2023_0437 paper presented at 52nd international congress and exposition on noise control engineering (inter-noise 2023)","order":185,"static_url":"/publications/213/"},{"section":"Publications","title":"AEROACOUSTIC INVESTIGATION OF GRID TURBULENCE INTERACTING WITH ROTORS","url":"/publications/212/","summary":"Wu, Han; Chen, Wangqiao; Zhang, Xin; Zhong, Siyang; Huang, Xun. “AEROACOUSTIC INVESTIGATION OF GRID TURBULENCE INTERACTING WITH ROTORS.” Proceedings of the 29th International Congress on Sound and Vibration, ICSV 2023 / edited by Carletti Eleonora. Society of Acoustics, 2023. (2…","meta":"Conference paper · 2023","search_text":"aeroacoustic investigation of grid turbulence interacting with rotors wu, han; chen, wangqiao; zhang, xin; zhong, siyang; huang, xun. “aeroacoustic investigation of grid turbulence interacting with rotors.” proceedings of the 29th international congress on sound and vibration, icsv 2023 / edited by carletti eleonora. society of acoustics, 2023. (2023). conference paper · 2023 wu, han; chen, wangqiao; zhang, xin; zhong, siyang; huang, xun 2023 proceedings of the 29th international congress on sound and vibration, icsv 2023 / edited by carletti eleonora. society of acoustics, 2023","order":186,"static_url":"/publications/212/"},{"section":"Publications","title":"A numerical study of the duct geometry effects on the aerodynamics and aeroacoustics of ducted propellers","url":"/publications/211/","summary":"Zhong, Siyang; Ma, Zhida; Cantos Trigo, Sinforiano Sebastian; Wu, Han; Zhang, Xin; Zhou, Peng. “A numerical study of the duct geometry effects on the aerodynamics and aeroacoustics of ducted propellers.” Paper presented at INTER-NOISE and NOISE-CON Congress and Conference Procee…","meta":"Conference paper · 2023","search_text":"a numerical study of the duct geometry effects on the aerodynamics and aeroacoustics of ducted propellers zhong, siyang; ma, zhida; cantos trigo, sinforiano sebastian; wu, han; zhang, xin; zhou, peng. “a numerical study of the duct geometry effects on the aerodynamics and aeroacoustics of ducted propellers.” paper presented at inter-noise and noise-con congress and conference proceedings, internoise23, p. 4717-4725. (2023). doi: 10.3397/in_2023_0670. conference paper · 2023 zhong, siyang; ma, zhida; cantos trigo, sinforiano sebastian; wu, han; zhang, xin; zhou, peng 2023 10.3397/in_2023_0670 paper presented at inter-noise and noise-con congress and conference proceedings, internoise23, p. 4717-4725 4717-4725","order":187,"static_url":"/publications/211/"},{"section":"Publications","title":"Performance of a windsurfing sail under steady condition","url":"/publications/210/","summary":"Mok, Kwan Pui; Zhou, Peng; Hou, Jiafan; Zhong, Siyang; Zhang, Xin; So, Raymond Chi Hung; Chan, King Yin. “Performance of a windsurfing sail under steady condition.” Ocean Engineering, v. 289, article number 116295. (2023). DOI: 10.1016/j.oceaneng.2023.116295.","meta":"Journal article · 2023","search_text":"performance of a windsurfing sail under steady condition mok, kwan pui; zhou, peng; hou, jiafan; zhong, siyang; zhang, xin; so, raymond chi hung; chan, king yin. “performance of a windsurfing sail under steady condition.” ocean engineering, v. 289, article number 116295. (2023). doi: 10.1016/j.oceaneng.2023.116295. journal article · 2023 mok, kwan pui; zhou, peng; hou, jiafan; zhong, siyang; zhang, xin; so, raymond chi hung; chan, king yin 2023 10.1016/j.oceaneng.2023.116295 ocean engineering 289 article 116295","order":188,"static_url":"/publications/210/"},{"section":"Publications","title":"On the cylinder noise and drag reductions in different Reynolds number ranges using surface pattern fabrics","url":"/publications/209/","summary":"Zheng, Chuntai; Zhou, Peng; Zhong, Siyang; Zhang, Xin. “On the cylinder noise and drag reductions in different Reynolds number ranges using surface pattern fabrics.” Physics of Fluids, v. 35, (3), article number 035111. (2023). DOI: 10.1063/5.0138074.","meta":"Journal article · 2023","search_text":"on the cylinder noise and drag reductions in different reynolds number ranges using surface pattern fabrics zheng, chuntai; zhou, peng; zhong, siyang; zhang, xin. “on the cylinder noise and drag reductions in different reynolds number ranges using surface pattern fabrics.” physics of fluids, v. 35, (3), article number 035111. (2023). doi: 10.1063/5.0138074. journal article · 2023 zheng, chuntai; zhou, peng; zhong, siyang; zhang, xin 2023 10.1063/5.0138074 physics of fluids 35 (3) article 035111","order":189,"static_url":"/publications/209/"},{"section":"Publications","title":"Frequency-Multiplexed Transmitted-Wave Manipulation with Multifunctional Acoustic Metasurfaces","url":"/publications/208/","summary":"Cheng, Haoyi; Guo, Jingwen; Zhang, Xin; Ye, Wenjing. “Frequency-Multiplexed Transmitted-Wave Manipulation with Multifunctional Acoustic Metasurfaces.” Physical Review Applied, v. 20, (3), article number 034009. (2023). DOI: 10.1103/physrevapplied.20.034009.","meta":"Journal article · 2023","search_text":"frequency-multiplexed transmitted-wave manipulation with multifunctional acoustic metasurfaces cheng, haoyi; guo, jingwen; zhang, xin; ye, wenjing. “frequency-multiplexed transmitted-wave manipulation with multifunctional acoustic metasurfaces.” physical review applied, v. 20, (3), article number 034009. (2023). doi: 10.1103/physrevapplied.20.034009. journal article · 2023 cheng, haoyi; guo, jingwen; zhang, xin; ye, wenjing 2023 10.1103/physrevapplied.20.034009 physical review applied 20 (3) article 034009","order":190,"static_url":"/publications/208/"},{"section":"Publications","title":"Experimental investigation on cylinder noise and its reductions by identifying aerodynamic sound sources in flow fields","url":"/publications/207/","summary":"Zheng, Chuntai; Zhou, Peng; Zhong, Siyang; Zhang, Xin. “Experimental investigation on cylinder noise and its reductions by identifying aerodynamic sound sources in flow fields.” Physics of Fluids, v. 35, (3), article number 035103. (2023). DOI: 10.1063/5.0138080.","meta":"Journal article · 2023","search_text":"experimental investigation on cylinder noise and its reductions by identifying aerodynamic sound sources in flow fields zheng, chuntai; zhou, peng; zhong, siyang; zhang, xin. “experimental investigation on cylinder noise and its reductions by identifying aerodynamic sound sources in flow fields.” physics of fluids, v. 35, (3), article number 035103. (2023). doi: 10.1063/5.0138080. journal article · 2023 zheng, chuntai; zhou, peng; zhong, siyang; zhang, xin 2023 10.1063/5.0138080 physics of fluids 35 (3) article 035103","order":191,"static_url":"/publications/207/"},{"section":"Publications","title":"Development of a Low-Noise and High-Efficiency Propeller Using Divergent Riblet Surface Pattern","url":"/publications/206/","summary":"Zheng, Chuntai; Chen, Wangqiao; Wu, Han; Zhou, Peng; Zhong, Siyang; Zhang, Xin. “Development of a Low-Noise and High-Efficiency Propeller Using Divergent Riblet Surface Pattern.” AIAA Journal, v. 61, (4), p. 1876-1880. (2023). DOI: 10.2514/1.j062602.","meta":"Journal article · 2023","search_text":"development of a low-noise and high-efficiency propeller using divergent riblet surface pattern zheng, chuntai; chen, wangqiao; wu, han; zhou, peng; zhong, siyang; zhang, xin. “development of a low-noise and high-efficiency propeller using divergent riblet surface pattern.” aiaa journal, v. 61, (4), p. 1876-1880. (2023). doi: 10.2514/1.j062602. journal article · 2023 zheng, chuntai; chen, wangqiao; wu, han; zhou, peng; zhong, siyang; zhang, xin 2023 10.2514/1.j062602 aiaa journal 61 (4) 1876-1880","order":192,"static_url":"/publications/206/"},{"section":"Publications","title":"Virtual flight simulation of delivery drone noise in the urban residential community","url":"/publications/159/","summary":"Tan, Qichen; Bian, Haoyu; Guo, Jingwen; Zhou, Peng; Lo, Hong Kam; Zhong, Siyang; Zhang, Xin. “Virtual flight simulation of delivery drone noise in the urban residential community.” Transportation Research Part D: Transport and Environment, v. 118, article number 103686. (2023). …","meta":"Journal article · 2023","search_text":"virtual flight simulation of delivery drone noise in the urban residential community tan, qichen; bian, haoyu; guo, jingwen; zhou, peng; lo, hong kam; zhong, siyang; zhang, xin. “virtual flight simulation of delivery drone noise in the urban residential community.” transportation research part d: transport and environment, v. 118, article number 103686. (2023). doi: 10.1016/j.trd.2023.103686. journal article · 2023 tan, qichen; bian, haoyu; guo, jingwen; zhou, peng; lo, hong kam; zhong, siyang; zhang, xin 2023 10.1016/j.trd.2023.103686 transportation research part d: transport and environment 118 article 103686","order":193,"static_url":"/publications/159/"},{"section":"Publications","title":"Sound reflection by periodic acoustic metasurface in sheared grazing flows","url":"/publications/158/","summary":"Qu, Renhao; Guo, Jingwen; Fang, Yi; Yi, Wei; Zhong, Siyang; Zhang, Xin. “Sound reflection by periodic acoustic metasurface in sheared grazing flows.” International Journal of Mechanical Sciences, v. 239, article number 107895. (2023). DOI: 10.1016/j.ijmecsci.2022.107895.","meta":"Journal article · 2023","search_text":"sound reflection by periodic acoustic metasurface in sheared grazing flows qu, renhao; guo, jingwen; fang, yi; yi, wei; zhong, siyang; zhang, xin. “sound reflection by periodic acoustic metasurface in sheared grazing flows.” international journal of mechanical sciences, v. 239, article number 107895. (2023). doi: 10.1016/j.ijmecsci.2022.107895. journal article · 2023 qu, renhao; guo, jingwen; fang, yi; yi, wei; zhong, siyang; zhang, xin 2023 10.1016/j.ijmecsci.2022.107895 international journal of mechanical sciences 239 article 107895","order":194,"static_url":"/publications/158/"},{"section":"Publications","title":"Predicting the aerodynamic noise of counter-rotating coaxial rotors","url":"/publications/157/","summary":"Zhong, Siyang; Ma, Zhida; Zhou, Peng; Wu, Han; Zhang, Xin. “Predicting the aerodynamic noise of counter-rotating coaxial rotors.” Journal of Sound and Vibration, v. 547, article number 117487. (2023). DOI: 10.1016/j.jsv.2022.117487.","meta":"Journal article · 2023","search_text":"predicting the aerodynamic noise of counter-rotating coaxial rotors zhong, siyang; ma, zhida; zhou, peng; wu, han; zhang, xin. “predicting the aerodynamic noise of counter-rotating coaxial rotors.” journal of sound and vibration, v. 547, article number 117487. (2023). doi: 10.1016/j.jsv.2022.117487. journal article · 2023 zhong, siyang; ma, zhida; zhou, peng; wu, han; zhang, xin 2023 10.1016/j.jsv.2022.117487 journal of sound and vibration 547 article 117487","order":195,"static_url":"/publications/157/"},{"section":"Publications","title":"Experimental investigation of the effect of sectional airfoil profile deviation on propeller noise","url":"/publications/156/","summary":"Wu, Han; Chen, Wangqiao; Jiang, Hanbo; Zhong, Siyang; Zhang, Xin. “Experimental investigation of the effect of sectional airfoil profile deviation on propeller noise.” Physics of Fluids, v. 35, (2), article number 027104. (2023). DOI: 10.1063/5.0135555.","meta":"Journal article · 2023","search_text":"experimental investigation of the effect of sectional airfoil profile deviation on propeller noise wu, han; chen, wangqiao; jiang, hanbo; zhong, siyang; zhang, xin. “experimental investigation of the effect of sectional airfoil profile deviation on propeller noise.” physics of fluids, v. 35, (2), article number 027104. (2023). doi: 10.1063/5.0135555. journal article · 2023 wu, han; chen, wangqiao; jiang, hanbo; zhong, siyang; zhang, xin 2023 10.1063/5.0135555 physics of fluids 35 (2) article 027104","order":196,"static_url":"/publications/156/"},{"section":"Publications","title":"Experimental and numerical investigations on rotor noise in axial descending flight","url":"/publications/155/","summary":"Li, Yuhong; Li, Xiangtian; Wu, Han; Zhou, Peng; Zhang, Xin; Zhong, Siyang. “Experimental and numerical investigations on rotor noise in axial descending flight.” Physical Review Fluids, v. 8, (9), article number 094803. (2023). DOI: 10.1103/physrevfluids.8.094803.","meta":"Journal article · 2023","search_text":"experimental and numerical investigations on rotor noise in axial descending flight li, yuhong; li, xiangtian; wu, han; zhou, peng; zhang, xin; zhong, siyang. “experimental and numerical investigations on rotor noise in axial descending flight.” physical review fluids, v. 8, (9), article number 094803. (2023). doi: 10.1103/physrevfluids.8.094803. journal article · 2023 li, yuhong; li, xiangtian; wu, han; zhou, peng; zhang, xin; zhong, siyang 2023 10.1103/physrevfluids.8.094803 physical review fluids 8 (9) article 094803","order":197,"static_url":"/publications/155/"},{"section":"Publications","title":"Development and progress in acoustic phase-gradient metamaterials for wavefront modulation","url":"/publications/154/","summary":"Guo, Jingwen; Fang, Yi; Qu, Renhao; Zhang, Xin. “Development and progress in acoustic phase-gradient metamaterials for wavefront modulation.” Materials Today, v. 66, p. 321-338. (2023). DOI: 10.1016/j.mattod.2023.04.004.","meta":"Journal article · 2023","search_text":"development and progress in acoustic phase-gradient metamaterials for wavefront modulation guo, jingwen; fang, yi; qu, renhao; zhang, xin. “development and progress in acoustic phase-gradient metamaterials for wavefront modulation.” materials today, v. 66, p. 321-338. (2023). doi: 10.1016/j.mattod.2023.04.004. journal article · 2023 guo, jingwen; fang, yi; qu, renhao; zhang, xin 2023 10.1016/j.mattod.2023.04.004 materials today 66 321-338","order":198,"static_url":"/publications/154/"},{"section":"Publications","title":"Computational aeroacoustics study of propellers with vibrational motion","url":"/publications/153/","summary":"Li, Yuhong; Wu, Han; Jiang, Hanbo; Zhong, Siyang; Zhang, Xin. “Computational aeroacoustics study of propellers with vibrational motion.” AIAA Journal, v. 61, (7), p. 3091-3107. (2023). DOI: 10.2514/1.j062370.","meta":"Journal article · 2023","search_text":"computational aeroacoustics study of propellers with vibrational motion li, yuhong; wu, han; jiang, hanbo; zhong, siyang; zhang, xin. “computational aeroacoustics study of propellers with vibrational motion.” aiaa journal, v. 61, (7), p. 3091-3107. (2023). doi: 10.2514/1.j062370. journal article · 2023 li, yuhong; wu, han; jiang, hanbo; zhong, siyang; zhang, xin 2023 10.2514/1.j062370 aiaa journal 61 (7) 3091-3107","order":199,"static_url":"/publications/153/"},{"section":"Publications","title":"Broadband quasi-perfect sound absorption by a metasurface with coupled resonators at both low- and high-amplitude excitations","url":"/publications/152/","summary":"Qu, Renhao; Guo, Jingwen; Fang, Yi; Zhong, Siyang; Zhang, Xin. “Broadband quasi-perfect sound absorption by a metasurface with coupled resonators at both low- and high-amplitude excitations.” Mechanical Systems and Signal Processing, v. 204, article number 110782. (2023). DOI: 1…","meta":"Journal article · 2023","search_text":"broadband quasi-perfect sound absorption by a metasurface with coupled resonators at both low- and high-amplitude excitations qu, renhao; guo, jingwen; fang, yi; zhong, siyang; zhang, xin. “broadband quasi-perfect sound absorption by a metasurface with coupled resonators at both low- and high-amplitude excitations.” mechanical systems and signal processing, v. 204, article number 110782. (2023). doi: 10.1016/j.ymssp.2023.110782. journal article · 2023 qu, renhao; guo, jingwen; fang, yi; zhong, siyang; zhang, xin 2023 10.1016/j.ymssp.2023.110782 mechanical systems and signal processing 204 article 110782","order":200,"static_url":"/publications/152/"},{"section":"Publications","title":"An investigation of rotor aeroacoustics with unsteady motions and uncertainty factors","url":"/publications/151/","summary":"Zhong, Siyang; Zhou, Peng; Chen, Wangqiao; Jiang, Hanbo; Wu, Han; Zhang, Xin. “An investigation of rotor aeroacoustics with unsteady motions and uncertainty factors.” Journal of Fluid Mechanics, v. 956, article number A16. (2023). DOI: 10.1017/jfm.2022.1097.","meta":"Journal article · 2023","search_text":"an investigation of rotor aeroacoustics with unsteady motions and uncertainty factors zhong, siyang; zhou, peng; chen, wangqiao; jiang, hanbo; wu, han; zhang, xin. “an investigation of rotor aeroacoustics with unsteady motions and uncertainty factors.” journal of fluid mechanics, v. 956, article number a16. (2023). doi: 10.1017/jfm.2022.1097. journal article · 2023 zhong, siyang; zhou, peng; chen, wangqiao; jiang, hanbo; wu, han; zhang, xin 2023 10.1017/jfm.2022.1097 journal of fluid mechanics 956 article a16","order":201,"static_url":"/publications/151/"},{"section":"Publications","title":"Acoustic imaging of the broadband noise arising in contra-rotating co-axial propellers","url":"/publications/150/","summary":"Chen, Wangqiao; Ma, Zhida; Spieser, Etienne; Guo, Jingwen; Zhou, Peng; Zhong, Siyang; Zhang, Xin; Huang, Xun. “Acoustic imaging of the broadband noise arising in contra-rotating co-axial propellers.” Aerospace Science and Technology, v. 141, article number 108531. (2023). DOI: 1…","meta":"Journal article · 2023","search_text":"acoustic imaging of the broadband noise arising in contra-rotating co-axial propellers chen, wangqiao; ma, zhida; spieser, etienne; guo, jingwen; zhou, peng; zhong, siyang; zhang, xin; huang, xun. “acoustic imaging of the broadband noise arising in contra-rotating co-axial propellers.” aerospace science and technology, v. 141, article number 108531. (2023). doi: 10.1016/j.ast.2023.108531. journal article · 2023 chen, wangqiao; ma, zhida; spieser, etienne; guo, jingwen; zhou, peng; zhong, siyang; zhang, xin; huang, xun 2023 10.1016/j.ast.2023.108531 aerospace science and technology 141 article 108531","order":202,"static_url":"/publications/150/"},{"section":"Publications","title":"A phase-gradient acoustic metasurface for broadband duct noise attenuation in the presence of flow","url":"/publications/149/","summary":"Guo, Jingwen; Qu, Renhao; Fang, Yi; Yi, Wei; Zhang, Xin. “A phase-gradient acoustic metasurface for broadband duct noise attenuation in the presence of flow.” International Journal of Mechanical Sciences, v. 237, article number 107822. (2023). DOI: 10.1016/j.ijmecsci.2022.107822.","meta":"Journal article · 2023","search_text":"a phase-gradient acoustic metasurface for broadband duct noise attenuation in the presence of flow guo, jingwen; qu, renhao; fang, yi; yi, wei; zhang, xin. “a phase-gradient acoustic metasurface for broadband duct noise attenuation in the presence of flow.” international journal of mechanical sciences, v. 237, article number 107822. (2023). doi: 10.1016/j.ijmecsci.2022.107822. journal article · 2023 guo, jingwen; qu, renhao; fang, yi; yi, wei; zhang, xin 2023 10.1016/j.ijmecsci.2022.107822 international journal of mechanical sciences 237 article 107822","order":203,"static_url":"/publications/149/"},{"section":"Publications","title":"UNCERTAINTY FACTORS IN PROPELLER AEROACOUSTIC MEASUREMENTS","url":"/publications/250/","summary":"Wu, Han; Jiang, Hanbo; Zhou, Peng; Zhong, Siyang; Zhang, Xin. “UNCERTAINTY FACTORS IN PROPELLER AEROACOUSTIC MEASUREMENTS.” Proceedings of the 28th International Congress on Sound and Vibration, ICSV 2022, Society of Acoustics, 2022. (2022).","meta":"Conference paper · 2022","search_text":"uncertainty factors in propeller aeroacoustic measurements wu, han; jiang, hanbo; zhou, peng; zhong, siyang; zhang, xin. “uncertainty factors in propeller aeroacoustic measurements.” proceedings of the 28th international congress on sound and vibration, icsv 2022, society of acoustics, 2022. (2022). conference paper · 2022 wu, han; jiang, hanbo; zhou, peng; zhong, siyang; zhang, xin 2022 proceedings of the 28th international congress on sound and vibration, icsv 2022, society of acoustics, 2022","order":204,"static_url":"/publications/250/"},{"section":"Publications","title":"Trailing edge noise reduction using velvety serrations","url":"/publications/249/","summary":"Zhou, Peng; Li, Xiangtian; Li, Yuhong; Jiang, Hanbo; Guo, Jingwen; Zhong, Siyang; Zhang, Xin; Angland, David. “Trailing edge noise reduction using velvety serrations.” 28th AIAA/CEAS Aeroacoustics Conference, 2022, American Institute of Aeronautics and Astronautics Inc, AIAA, 20…","meta":"Conference paper · 2022","search_text":"trailing edge noise reduction using velvety serrations zhou, peng; li, xiangtian; li, yuhong; jiang, hanbo; guo, jingwen; zhong, siyang; zhang, xin; angland, david. “trailing edge noise reduction using velvety serrations.” 28th aiaa/ceas aeroacoustics conference, 2022, american institute of aeronautics and astronautics inc, aiaa, 2022, article number aiaa 2022-2893. (2022). doi: 10.2514/6.2022-2893. conference paper · 2022 zhou, peng; li, xiangtian; li, yuhong; jiang, hanbo; guo, jingwen; zhong, siyang; zhang, xin; angland, david 2022 10.2514/6.2022-2893 28th aiaa/ceas aeroacoustics conference, 2022, american institute of aeronautics and astronautics inc, aiaa, 2022, article number aiaa 2022-2893 article aiaa 2022-2893","order":205,"static_url":"/publications/249/"},{"section":"Publications","title":"Reflected wave manipulation by acoustic metasurface in shear flows","url":"/publications/248/","summary":"Qu, Renhao; Guo, Jingwen; Fang, Yi; Yi, Wei; Zhong, Siyang; Angland, David; Zhang, Xin. “Reflected wave manipulation by acoustic metasurface in shear flows.” 28th AIAA/CEAS Aeroacoustics Conference, 2022, American Institute of Aeronautics and Astronautics Inc, AIAA, 2022, articl…","meta":"Conference paper · 2022","search_text":"reflected wave manipulation by acoustic metasurface in shear flows qu, renhao; guo, jingwen; fang, yi; yi, wei; zhong, siyang; angland, david; zhang, xin. “reflected wave manipulation by acoustic metasurface in shear flows.” 28th aiaa/ceas aeroacoustics conference, 2022, american institute of aeronautics and astronautics inc, aiaa, 2022, article number aiaa 2022-2905. (2022). doi: 10.2514/6.2022-2905. conference paper · 2022 qu, renhao; guo, jingwen; fang, yi; yi, wei; zhong, siyang; angland, david; zhang, xin 2022 10.2514/6.2022-2905 28th aiaa/ceas aeroacoustics conference, 2022, american institute of aeronautics and astronautics inc, aiaa, 2022, article number aiaa 2022-2905 article aiaa 2022-2905","order":206,"static_url":"/publications/248/"},{"section":"Publications","title":"On the effect of unsteady motions on the rotor aerodynamic noise","url":"/publications/247/","summary":"Zhong, Siyang; Zhou, Peng; Jiang, Hanbo; Wu, Han; Guo, Jingwen; Zhang, Xin. “On the effect of unsteady motions on the rotor aerodynamic noise.” 28th AIAA/CEAS Aeroacoustics Conference, 2022, American Institute of Aeronautics and Astronautics Inc, AIAA, 2022, article number AIAA …","meta":"Conference paper · 2022","search_text":"on the effect of unsteady motions on the rotor aerodynamic noise zhong, siyang; zhou, peng; jiang, hanbo; wu, han; guo, jingwen; zhang, xin. “on the effect of unsteady motions on the rotor aerodynamic noise.” 28th aiaa/ceas aeroacoustics conference, 2022, american institute of aeronautics and astronautics inc, aiaa, 2022, article number aiaa 2022-3074. (2022). doi: 10.2514/6.2022-3074. conference paper · 2022 zhong, siyang; zhou, peng; jiang, hanbo; wu, han; guo, jingwen; zhang, xin 2022 10.2514/6.2022-3074 28th aiaa/ceas aeroacoustics conference, 2022, american institute of aeronautics and astronautics inc, aiaa, 2022, article number aiaa 2022-3074 article aiaa 2022-3074","order":207,"static_url":"/publications/247/"},{"section":"Publications","title":"Numerical study of the aeroacoustics of shrouded propellers for Urban Air Mobility vehicles","url":"/publications/246/","summary":"Cantos trigo, Sinforiano Sebastian; Jiang, Hanbo; Zhang, Xin; Zhong, Siyang. “Numerical study of the aeroacoustics of shrouded propellers for Urban Air Mobility vehicles.” Paper presented at Quiet Drones-Second International Symposium on Noise from UAVs UASs and eVTOLs. (2022).","meta":"Conference paper · 2022","search_text":"numerical study of the aeroacoustics of shrouded propellers for urban air mobility vehicles cantos trigo, sinforiano sebastian; jiang, hanbo; zhang, xin; zhong, siyang. “numerical study of the aeroacoustics of shrouded propellers for urban air mobility vehicles.” paper presented at quiet drones-second international symposium on noise from uavs uass and evtols. (2022). conference paper · 2022 cantos trigo, sinforiano sebastian; jiang, hanbo; zhang, xin; zhong, siyang 2022 paper presented at quiet drones-second international symposium on noise from uavs uass and evtols","order":208,"static_url":"/publications/246/"},{"section":"Publications","title":"Identification of deterministic components of propeller noise","url":"/publications/245/","summary":"Jiang, Hanbo; Wu, Han; Zhang, Xin; Zhong, Siyang; Zhou, Peng. “Identification of deterministic components of propeller noise.” Paper presented at Quiet Drones 2022-Second International Symposium on Noise from UAVs UASs and eVTOLs. (2022).","meta":"Conference paper · 2022","search_text":"identification of deterministic components of propeller noise jiang, hanbo; wu, han; zhang, xin; zhong, siyang; zhou, peng. “identification of deterministic components of propeller noise.” paper presented at quiet drones 2022-second international symposium on noise from uavs uass and evtols. (2022). conference paper · 2022 jiang, hanbo; wu, han; zhang, xin; zhong, siyang; zhou, peng 2022 paper presented at quiet drones 2022-second international symposium on noise from uavs uass and evtols","order":209,"static_url":"/publications/245/"},{"section":"Publications","title":"Enhancing the noise reduction capability of serrations using low-profile vortex generators","url":"/publications/244/","summary":"Sundeep, Shivam; Zhou, Peng; Zheng, Chuntai; Jiang, Hanbo; Zhong, Siyang; Zhang, Xin. “Enhancing the noise reduction capability of serrations using low-profile vortex generators.” Internoise 2022 - 51st International Congress and Exposition on Noise Control Engineering, The Inst…","meta":"Conference paper · 2022","search_text":"enhancing the noise reduction capability of serrations using low-profile vortex generators sundeep, shivam; zhou, peng; zheng, chuntai; jiang, hanbo; zhong, siyang; zhang, xin. “enhancing the noise reduction capability of serrations using low-profile vortex generators.” internoise 2022 - 51st international congress and exposition on noise control engineering, the institute of noise control engineering of the usa, inc., 2022. (2022). doi: 10.3397/in_2022_0571. conference paper · 2022 sundeep, shivam; zhou, peng; zheng, chuntai; jiang, hanbo; zhong, siyang; zhang, xin 2022 10.3397/in_2022_0571 internoise 2022 - 51st international congress and exposition on noise control engineering, the institute of noise control engineering of the usa, inc., 2022","order":210,"static_url":"/publications/244/"},{"section":"Publications","title":"Computational aeroacoustics of an urban air mobility vehicle using the acoustic preserved artificial compressibility method","url":"/publications/243/","summary":"Ma, Zhida; Jiang, Hanbo; Li, Yuhong; Zhang, Xin; Zhong, Siyang. “Computational aeroacoustics of an urban air mobility vehicle using the acoustic preserved artificial compressibility method.” Paper presented at Quiet Drones-Second International Symposium on Noise from UAVs UASs a…","meta":"Conference paper · 2022","search_text":"computational aeroacoustics of an urban air mobility vehicle using the acoustic preserved artificial compressibility method ma, zhida; jiang, hanbo; li, yuhong; zhang, xin; zhong, siyang. “computational aeroacoustics of an urban air mobility vehicle using the acoustic preserved artificial compressibility method.” paper presented at quiet drones-second international symposium on noise from uavs uass and evtols. (2022). conference paper · 2022 ma, zhida; jiang, hanbo; li, yuhong; zhang, xin; zhong, siyang 2022 paper presented at quiet drones-second international symposium on noise from uavs uass and evtols","order":211,"static_url":"/publications/243/"},{"section":"Publications","title":"Acoustic measurement of multi-rotor drones in anechoic and hemi-anechoic chambers","url":"/publications/242/","summary":"Ma, Zhida; Jiang, Hanbo; Wu, Han; Zhang, Xin; Zhong, Siyang. “Acoustic measurement of multi-rotor drones in anechoic and hemi-anechoic chambers.” Paper presented at Quiet Drones-2022-Second International Symposium on Noise from UAVs UASs and eVTOLs. (2022).","meta":"Conference paper · 2022","search_text":"acoustic measurement of multi-rotor drones in anechoic and hemi-anechoic chambers ma, zhida; jiang, hanbo; wu, han; zhang, xin; zhong, siyang. “acoustic measurement of multi-rotor drones in anechoic and hemi-anechoic chambers.” paper presented at quiet drones-2022-second international symposium on noise from uavs uass and evtols. (2022). conference paper · 2022 ma, zhida; jiang, hanbo; wu, han; zhang, xin; zhong, siyang 2022 paper presented at quiet drones-2022-second international symposium on noise from uavs uass and evtols","order":212,"static_url":"/publications/242/"},{"section":"Publications","title":"ACOUSTIC IMPEDANCE MEASUREMENTS USING AN ADVANCED GRAZING FLOW TUBE FACILITY","url":"/publications/241/","summary":"Yi, Wei; Guo, Jingwen; Fang, Yi; Qu, Renhao; Zhong, Siyang; Jiang, Hanbo; Zhou, Peng; Zhang, Xin. “ACOUSTIC IMPEDANCE MEASUREMENTS USING AN ADVANCED GRAZING FLOW TUBE FACILITY.” Proceedings of the 28th International Congress on Sound and Vibration, ICSV 2022, Society of Acoustic…","meta":"Conference paper · 2022","search_text":"acoustic impedance measurements using an advanced grazing flow tube facility yi, wei; guo, jingwen; fang, yi; qu, renhao; zhong, siyang; jiang, hanbo; zhou, peng; zhang, xin. “acoustic impedance measurements using an advanced grazing flow tube facility.” proceedings of the 28th international congress on sound and vibration, icsv 2022, society of acoustics, 2022. (2022). conference paper · 2022 yi, wei; guo, jingwen; fang, yi; qu, renhao; zhong, siyang; jiang, hanbo; zhou, peng; zhang, xin 2022 proceedings of the 28th international congress on sound and vibration, icsv 2022, society of acoustics, 2022","order":213,"static_url":"/publications/241/"},{"section":"Publications","title":"Toward high-efficiency low-noise propellers: A numerical and experimental study","url":"/publications/240/","summary":"Jiang, Hanbo; Wu, Han; Chen, Wangqiao; Zhou, Peng; Zhong, Siyang; Zhang, Xin; Zhou, Guocheng; Chen, Bao. “Toward high-efficiency low-noise propellers: A numerical and experimental study.” Physics of Fluids, v. 34, (7), article number 076116. (2022). DOI: 10.1063/5.0098891.","meta":"Journal article · 2022","search_text":"toward high-efficiency low-noise propellers: a numerical and experimental study jiang, hanbo; wu, han; chen, wangqiao; zhou, peng; zhong, siyang; zhang, xin; zhou, guocheng; chen, bao. “toward high-efficiency low-noise propellers: a numerical and experimental study.” physics of fluids, v. 34, (7), article number 076116. (2022). doi: 10.1063/5.0098891. journal article · 2022 jiang, hanbo; wu, han; chen, wangqiao; zhou, peng; zhong, siyang; zhang, xin; zhou, guocheng; chen, bao 2022 10.1063/5.0098891 physics of fluids 34 (7) article 076116","order":214,"static_url":"/publications/240/"},{"section":"Publications","title":"Topology optimization design and experimental validation of an acoustic metasurface for reflected wavefront modulation","url":"/publications/239/","summary":"Guo, Jingwen; Zhang, Xin; Fang, Yi. “Topology optimization design and experimental validation of an acoustic metasurface for reflected wavefront modulation.” Journal of Sound and Vibration, v. 520, article number 116631. (2022). DOI: 10.1016/j.jsv.2021.116631.","meta":"Journal article · 2022","search_text":"topology optimization design and experimental validation of an acoustic metasurface for reflected wavefront modulation guo, jingwen; zhang, xin; fang, yi. “topology optimization design and experimental validation of an acoustic metasurface for reflected wavefront modulation.” journal of sound and vibration, v. 520, article number 116631. (2022). doi: 10.1016/j.jsv.2021.116631. journal article · 2022 guo, jingwen; zhang, xin; fang, yi 2022 10.1016/j.jsv.2021.116631 journal of sound and vibration 520 article 116631","order":215,"static_url":"/publications/239/"},{"section":"Publications","title":"Reprint of: Assessment of UAM and drone noise impact on the environment based on virtual flights","url":"/publications/238/","summary":"Bian, Haoyu; Tan, Qichen; Zhong, Siyang; Zhang, Xin. “Reprint of: Assessment of UAM and drone noise impact on the environment based on virtual flights.” Aerospace Science and Technology, v. 125, article number 107547. (2022). DOI: 10.1016/j.ast.2022.107547.","meta":"Journal article · 2022","search_text":"reprint of: assessment of uam and drone noise impact on the environment based on virtual flights bian, haoyu; tan, qichen; zhong, siyang; zhang, xin. “reprint of: assessment of uam and drone noise impact on the environment based on virtual flights.” aerospace science and technology, v. 125, article number 107547. (2022). doi: 10.1016/j.ast.2022.107547. journal article · 2022 bian, haoyu; tan, qichen; zhong, siyang; zhang, xin 2022 10.1016/j.ast.2022.107547 aerospace science and technology 125 article 107547","order":216,"static_url":"/publications/238/"},{"section":"Publications","title":"Recognizing the aeroacoustic information of noise radiated by an unflanged duct based on convolutional neural networks","url":"/publications/237/","summary":"Guo, Jingwen; Li, Xiangtian; Ren, Chenyu; Zhang, Xin. “Recognizing the aeroacoustic information of noise radiated by an unflanged duct based on convolutional neural networks.” Journal of the Acoustical Society of America, v. 152, (5), p. 2531-2542. (2022). DOI: 10.1121/10.001500…","meta":"Journal article · 2022","search_text":"recognizing the aeroacoustic information of noise radiated by an unflanged duct based on convolutional neural networks guo, jingwen; li, xiangtian; ren, chenyu; zhang, xin. “recognizing the aeroacoustic information of noise radiated by an unflanged duct based on convolutional neural networks.” journal of the acoustical society of america, v. 152, (5), p. 2531-2542. (2022). doi: 10.1121/10.0015003. journal article · 2022 guo, jingwen; li, xiangtian; ren, chenyu; zhang, xin 2022 10.1121/10.0015003 journal of the acoustical society of america 152 (5) 2531-2542","order":217,"static_url":"/publications/237/"},{"section":"Publications","title":"Radiation Modes of Propeller Tonal Noise","url":"/publications/236/","summary":"Jiang, Hanbo; Zhong, Siyang; Wu, Han; Zhang, Xin; Huang, Xun; Zhou, Guocheng; Chen, Bao. “Radiation Modes of Propeller Tonal Noise.” Journal of Vibration and Acoustics, v. 144, (2), article number 021009. (2022). DOI: 10.1115/1.4051864.","meta":"Journal article · 2022","search_text":"radiation modes of propeller tonal noise jiang, hanbo; zhong, siyang; wu, han; zhang, xin; huang, xun; zhou, guocheng; chen, bao. “radiation modes of propeller tonal noise.” journal of vibration and acoustics, v. 144, (2), article number 021009. (2022). doi: 10.1115/1.4051864. journal article · 2022 jiang, hanbo; zhong, siyang; wu, han; zhang, xin; huang, xun; zhou, guocheng; chen, bao 2022 10.1115/1.4051864 journal of vibration and acoustics 144 (2) article 021009","order":218,"static_url":"/publications/236/"},{"section":"Publications","title":"On identifying the deterministic components of propeller noise","url":"/publications/235/","summary":"Wu, Han; Jiang, Hanbo; Zhou, Peng; Zhong, Siyang; Zhang, Xin; Zhou, Guocheng; Chen, Bao. “On identifying the deterministic components of propeller noise.” Aerospace Science and Technology, v. 130, article number 107948. (2022). DOI: 10.1016/j.ast.2022.107948.","meta":"Journal article · 2022","search_text":"on identifying the deterministic components of propeller noise wu, han; jiang, hanbo; zhou, peng; zhong, siyang; zhang, xin; zhou, guocheng; chen, bao. “on identifying the deterministic components of propeller noise.” aerospace science and technology, v. 130, article number 107948. (2022). doi: 10.1016/j.ast.2022.107948. journal article · 2022 wu, han; jiang, hanbo; zhou, peng; zhong, siyang; zhang, xin; zhou, guocheng; chen, bao 2022 10.1016/j.ast.2022.107948 aerospace science and technology 130 article 107948","order":219,"static_url":"/publications/235/"},{"section":"Publications","title":"Forbidden Transmission of Broadband Duct Noise Realized by Compactly Placed Detuned Resonators","url":"/publications/234/","summary":"Guo, Jingwen; Fang, Yi; Zhang, Xin. “Forbidden Transmission of Broadband Duct Noise Realized by Compactly Placed Detuned Resonators.” Acoustics Australia, v. 50, (1), p. 79-90. (2022). DOI: 10.1007/s40857-021-00258-x.","meta":"Journal article · 2022","search_text":"forbidden transmission of broadband duct noise realized by compactly placed detuned resonators guo, jingwen; fang, yi; zhang, xin. “forbidden transmission of broadband duct noise realized by compactly placed detuned resonators.” acoustics australia, v. 50, (1), p. 79-90. (2022). doi: 10.1007/s40857-021-00258-x. journal article · 2022 guo, jingwen; fang, yi; zhang, xin 2022 10.1007/s40857-021-00258-x acoustics australia 50 (1) 79-90","order":220,"static_url":"/publications/234/"},{"section":"Publications","title":"Efficient computation of broadband noise propagation using Gaussian beam tracing method","url":"/publications/233/","summary":"Bian, Haoyu; Tan, Qichen; Zhong, Siyang; Zhang, Xin. “Efficient computation of broadband noise propagation using Gaussian beam tracing method.” Journal of the Acoustical Society of America, v. 151, (5), p. 3387-3397. (2022). DOI: 10.1121/10.0011399.","meta":"Journal article · 2022","search_text":"efficient computation of broadband noise propagation using gaussian beam tracing method bian, haoyu; tan, qichen; zhong, siyang; zhang, xin. “efficient computation of broadband noise propagation using gaussian beam tracing method.” journal of the acoustical society of america, v. 151, (5), p. 3387-3397. (2022). doi: 10.1121/10.0011399. journal article · 2022 bian, haoyu; tan, qichen; zhong, siyang; zhang, xin 2022 10.1121/10.0011399 journal of the acoustical society of america 151 (5) 3387-3397","order":221,"static_url":"/publications/233/"},{"section":"Publications","title":"Broadband trailing edge noise reduction through porous velvet-coated serrations","url":"/publications/232/","summary":"Zhou, Peng; Zhong, Siyang; Li, Xiangtian; Li, Yuhong; Chen, Wangqiao; Jiang, Hanbo; Zhang, Xin. “Broadband trailing edge noise reduction through porous velvet-coated serrations.” Physics of Fluids, v. 34, (5), article number 057112. (2022). DOI: 10.1063/5.0089257.","meta":"Journal article · 2022","search_text":"broadband trailing edge noise reduction through porous velvet-coated serrations zhou, peng; zhong, siyang; li, xiangtian; li, yuhong; chen, wangqiao; jiang, hanbo; zhang, xin. “broadband trailing edge noise reduction through porous velvet-coated serrations.” physics of fluids, v. 34, (5), article number 057112. (2022). doi: 10.1063/5.0089257. journal article · 2022 zhou, peng; zhong, siyang; li, xiangtian; li, yuhong; chen, wangqiao; jiang, hanbo; zhang, xin 2022 10.1063/5.0089257 physics of fluids 34 (5) article 057112","order":222,"static_url":"/publications/232/"},{"section":"Publications","title":"Broadband acoustic meta-porous layer for reflected wave manipulation and absorption","url":"/publications/231/","summary":"Qu, Renhao; Guo, Jingwen; Fang, Yi; Zhong, Siyang; Zhang, Xin. “Broadband acoustic meta-porous layer for reflected wave manipulation and absorption.” International Journal of Mechanical Sciences, v. 227, article number 107426. (2022). DOI: 10.1016/j.ijmecsci.2022.107426.","meta":"Journal article · 2022","search_text":"broadband acoustic meta-porous layer for reflected wave manipulation and absorption qu, renhao; guo, jingwen; fang, yi; zhong, siyang; zhang, xin. “broadband acoustic meta-porous layer for reflected wave manipulation and absorption.” international journal of mechanical sciences, v. 227, article number 107426. (2022). doi: 10.1016/j.ijmecsci.2022.107426. journal article · 2022 qu, renhao; guo, jingwen; fang, yi; zhong, siyang; zhang, xin 2022 10.1016/j.ijmecsci.2022.107426 international journal of mechanical sciences 227 article 107426","order":223,"static_url":"/publications/231/"},{"section":"Publications","title":"Boundary element analysis on the fuselage scattering of drone noise","url":"/publications/230/","summary":"Jiang, Hanbo; Zhong, Siyang; Zhang, Xin; Huang, Xun. “Boundary element analysis on the fuselage scattering of drone noise.” International Journal of Aeroacoustics, v. 21, (1-2), p. 43-56. (2022). DOI: 10.1177/1475472x221079549.","meta":"Journal article · 2022","search_text":"boundary element analysis on the fuselage scattering of drone noise jiang, hanbo; zhong, siyang; zhang, xin; huang, xun. “boundary element analysis on the fuselage scattering of drone noise.” international journal of aeroacoustics, v. 21, (1-2), p. 43-56. (2022). doi: 10.1177/1475472x221079549. journal article · 2022 jiang, hanbo; zhong, siyang; zhang, xin; huang, xun 2022 10.1177/1475472x221079549 international journal of aeroacoustics 21 (1-2) 43-56","order":224,"static_url":"/publications/230/"},{"section":"Publications","title":"An extremely-thin acoustic metasurface for low-frequency sound attenuation with a tunable absorption bandwidth","url":"/publications/229/","summary":"Guo, Jingwen; Zhang, Xin; Fang, Yi; Qu, Renhao. “An extremely-thin acoustic metasurface for low-frequency sound attenuation with a tunable absorption bandwidth.” International Journal of Mechanical Sciences, v. 213, article number 106872. (2022). DOI: 10.1016/j.ijmecsci.2021.106…","meta":"Journal article · 2022","search_text":"an extremely-thin acoustic metasurface for low-frequency sound attenuation with a tunable absorption bandwidth guo, jingwen; zhang, xin; fang, yi; qu, renhao. “an extremely-thin acoustic metasurface for low-frequency sound attenuation with a tunable absorption bandwidth.” international journal of mechanical sciences, v. 213, article number 106872. (2022). doi: 10.1016/j.ijmecsci.2021.106872. journal article · 2022 guo, jingwen; zhang, xin; fang, yi; qu, renhao 2022 10.1016/j.ijmecsci.2021.106872 international journal of mechanical sciences 213 article 106872","order":225,"static_url":"/publications/229/"},{"section":"Publications","title":"An experimental study of aerodynamic noise from large obstructions in turbulent boundary layer flows","url":"/publications/228/","summary":"Sundeep, Shivam; Bu, Huanxian; Zhou, Peng; Zhong, Siyang; Zhang, Xin. “An experimental study of aerodynamic noise from large obstructions in turbulent boundary layer flows.” Physics of Fluids, v. 34, (2), article number 025121. (2022). DOI: 10.1063/5.0080426.","meta":"Journal article · 2022","search_text":"an experimental study of aerodynamic noise from large obstructions in turbulent boundary layer flows sundeep, shivam; bu, huanxian; zhou, peng; zhong, siyang; zhang, xin. “an experimental study of aerodynamic noise from large obstructions in turbulent boundary layer flows.” physics of fluids, v. 34, (2), article number 025121. (2022). doi: 10.1063/5.0080426. journal article · 2022 sundeep, shivam; bu, huanxian; zhou, peng; zhong, siyang; zhang, xin 2022 10.1063/5.0080426 physics of fluids 34 (2) article 025121","order":226,"static_url":"/publications/228/"},{"section":"Publications","title":"An efficient and high-order sliding mesh method for computational aeroacoustics","url":"/publications/227/","summary":"Ying, Wei; Fattah, Ryu; Zhong, Siyang; Guo, Jingwen; Zhang, Xin. “An efficient and high-order sliding mesh method for computational aeroacoustics.” Journal of Supercomputing, v. 78, (7), p. 9492-9520. (2022). DOI: 10.1007/s11227-021-04180-x.","meta":"Journal article · 2022","search_text":"an efficient and high-order sliding mesh method for computational aeroacoustics ying, wei; fattah, ryu; zhong, siyang; guo, jingwen; zhang, xin. “an efficient and high-order sliding mesh method for computational aeroacoustics.” journal of supercomputing, v. 78, (7), p. 9492-9520. (2022). doi: 10.1007/s11227-021-04180-x. journal article · 2022 ying, wei; fattah, ryu; zhong, siyang; guo, jingwen; zhang, xin 2022 10.1007/s11227-021-04180-x journal of supercomputing 78 (7) 9492-9520","order":227,"static_url":"/publications/227/"},{"section":"Publications","title":"An acoustic-wave preserved artificial compressibility method for low-Mach-number aeroacoustic simulations","url":"/publications/226/","summary":"Jiang, Hanbo; Zhang, Xin. “An acoustic-wave preserved artificial compressibility method for low-Mach-number aeroacoustic simulations.” Journal of Sound and Vibration, v. 516, article number 116505. (2022). DOI: 10.1016/j.jsv.2021.116505.","meta":"Journal article · 2022","search_text":"an acoustic-wave preserved artificial compressibility method for low-mach-number aeroacoustic simulations jiang, hanbo; zhang, xin. “an acoustic-wave preserved artificial compressibility method for low-mach-number aeroacoustic simulations.” journal of sound and vibration, v. 516, article number 116505. (2022). doi: 10.1016/j.jsv.2021.116505. journal article · 2022 jiang, hanbo; zhang, xin 2022 10.1016/j.jsv.2021.116505 journal of sound and vibration 516 article 116505","order":228,"static_url":"/publications/226/"},{"section":"Publications","title":"Aerodynamics of isolated cycling wheels using wind tunnel tests and computational fluid dynamics","url":"/publications/225/","summary":"Yi, Wei; Bertin, Celia; Zhou, Peng; Mao, Jiaqi; Zhong, Siyang; Zhang, Xin. “Aerodynamics of isolated cycling wheels using wind tunnel tests and computational fluid dynamics.” Journal of Wind Engineering and Industrial Aerodynamics, v. 228, article number 105085. (2022). DOI: 10.…","meta":"Journal article · 2022","search_text":"aerodynamics of isolated cycling wheels using wind tunnel tests and computational fluid dynamics yi, wei; bertin, celia; zhou, peng; mao, jiaqi; zhong, siyang; zhang, xin. “aerodynamics of isolated cycling wheels using wind tunnel tests and computational fluid dynamics.” journal of wind engineering and industrial aerodynamics, v. 228, article number 105085. (2022). doi: 10.1016/j.jweia.2022.105085. journal article · 2022 yi, wei; bertin, celia; zhou, peng; mao, jiaqi; zhong, siyang; zhang, xin 2022 10.1016/j.jweia.2022.105085 journal of wind engineering and industrial aerodynamics 228 article 105085","order":229,"static_url":"/publications/225/"},{"section":"Publications","title":"Ultra-light Metamaterial for Sound Absorption Based on Miura-ori Sandwich Structure","url":"/publications/284/","summary":"Fang, Yi; Guo, Jingwen; Wang, Yixin; Yu, Hongyu; Zhang, Xin. “Ultra-light Metamaterial for Sound Absorption Based on Miura-ori Sandwich Structure.” Paper presented at The 16th IEEE International Conference on Nano/Micro Engineered & Molecular Systems (IEEE-NEMS 2021). (2021).","meta":"Conference paper · 2021","search_text":"ultra-light metamaterial for sound absorption based on miura-ori sandwich structure fang, yi; guo, jingwen; wang, yixin; yu, hongyu; zhang, xin. “ultra-light metamaterial for sound absorption based on miura-ori sandwich structure.” paper presented at the 16th ieee international conference on nano/micro engineered & molecular systems (ieee-nems 2021). (2021). conference paper · 2021 fang, yi; guo, jingwen; wang, yixin; yu, hongyu; zhang, xin 2021 paper presented at the 16th ieee international conference on nano/micro engineered & molecular systems (ieee-nems 2021)","order":230,"static_url":"/publications/284/"},{"section":"Publications","title":"Trailing edge noise reduction through flexible serrations","url":"/publications/283/","summary":"Zhou, Peng; Liu, Qian; Zhong, Siyang; Zhang, Xin. “Trailing edge noise reduction through flexible serrations.” \"Advances in Acoustics, Noise and Vibration - 2021\" Proceedings of the 27th International Congress on Sound and Vibration, ICSV 2021 / edited by Carletti Eleonora; Croc…","meta":"Conference paper · 2021","search_text":"trailing edge noise reduction through flexible serrations zhou, peng; liu, qian; zhong, siyang; zhang, xin. “trailing edge noise reduction through flexible serrations.” \"advances in acoustics, noise and vibration - 2021\" proceedings of the 27th international congress on sound and vibration, icsv 2021 / edited by carletti eleonora; crocker malcolm; pawelczyk marek; tuma jiri. silesian university press, 2021. (2021). conference paper · 2021 zhou, peng; liu, qian; zhong, siyang; zhang, xin 2021 \"advances in acoustics, noise and vibration - 2021\" proceedings of the 27th international congress on sound and vibration, icsv 2021 / edited by carletti eleonora; crocker malcolm; pawelczyk marek; tuma jiri. silesian university press, 2021","order":231,"static_url":"/publications/283/"},{"section":"Publications","title":"The multi-functional rotor aerodynamic and aeroacoustic test platform at HKUST","url":"/publications/282/","summary":"Wu, Han; Zheng, Chuntai; Zhou, Peng; Fattah, Ryu; Zhong, Siyang; Zhang, Xin. “The multi-functional rotor aerodynamic and aeroacoustic test platform at HKUST.” Proceedings of INTER-NOISE 2021 - 2021 International Congress and Exposition of Noise Control Engineering / edited by Da…","meta":"Conference paper · 2021","search_text":"the multi-functional rotor aerodynamic and aeroacoustic test platform at hkust wu, han; zheng, chuntai; zhou, peng; fattah, ryu; zhong, siyang; zhang, xin. “the multi-functional rotor aerodynamic and aeroacoustic test platform at hkust.” proceedings of inter-noise 2021 - 2021 international congress and exposition of noise control engineering / edited by dare tyler; bolton stuart; davies patricia; xue yutong; ebbitt gordon. the institute of noise control engineering of the usa, inc., 2021. (2021). doi: 10.3397/in-2021-2695. conference paper · 2021 wu, han; zheng, chuntai; zhou, peng; fattah, ryu; zhong, siyang; zhang, xin 2021 10.3397/in-2021-2695 proceedings of inter-noise 2021 - 2021 international congress and exposition of noise control engineering / edited by dare tyler; bolton stuart; davies patricia; xue yutong; ebbitt gordon. the institute of noise control engineering of the usa, inc., 2021","order":232,"static_url":"/publications/282/"},{"section":"Publications","title":"The experimental study on sound reduction of a circular cylinder with surface pattern","url":"/publications/281/","summary":"Zheng, Chuntai; Zhou, Peng; Zhang, Xin. “The experimental study on sound reduction of a circular cylinder with surface pattern.” \"Advances in Acoustics, Noise and Vibration - 2021\" Proceedings of the 27th International Congress on Sound and Vibration, ICSV 2021 / edited by Carle…","meta":"Conference paper · 2021","search_text":"the experimental study on sound reduction of a circular cylinder with surface pattern zheng, chuntai; zhou, peng; zhang, xin. “the experimental study on sound reduction of a circular cylinder with surface pattern.” \"advances in acoustics, noise and vibration - 2021\" proceedings of the 27th international congress on sound and vibration, icsv 2021 / edited by carletti eleonora; crocker malcolm; pawelczyk marek; tuma jiri. silesian university press, 2021. (2021). conference paper · 2021 zheng, chuntai; zhou, peng; zhang, xin 2021 \"advances in acoustics, noise and vibration - 2021\" proceedings of the 27th international congress on sound and vibration, icsv 2021 / edited by carletti eleonora; crocker malcolm; pawelczyk marek; tuma jiri. silesian university press, 2021","order":233,"static_url":"/publications/281/"},{"section":"Publications","title":"Supercomputer Simulation of Turbulent Flow Around Isolated UAV Rotor and Associated Acoustic Fields","url":"/publications/280/","summary":"Bobkov, Vladimir; Gorobets, Andrey; Kozubskaya, Tatiana; Zhang, Xin; Zhong, Siyang. “Supercomputer Simulation of Turbulent Flow Around Isolated UAV Rotor and Associated Acoustic Fields.” Supercomputing - 7th Russian Supercomputing Days, RuSCDays 2021, Revised Selected Papers / e…","meta":"Conference paper · 2021","search_text":"supercomputer simulation of turbulent flow around isolated uav rotor and associated acoustic fields bobkov, vladimir; gorobets, andrey; kozubskaya, tatiana; zhang, xin; zhong, siyang. “supercomputer simulation of turbulent flow around isolated uav rotor and associated acoustic fields.” supercomputing - 7th russian supercomputing days, ruscdays 2021, revised selected papers / edited by voevodin vladimir; sobolev sergey. springer science and business media deutschland gmbh, 2021, p. 256-269. (2021). doi: 10.1007/978-3-030-92864-3_20. conference paper · 2021 bobkov, vladimir; gorobets, andrey; kozubskaya, tatiana; zhang, xin; zhong, siyang 2021 10.1007/978-3-030-92864-3_20 supercomputing - 7th russian supercomputing days, ruscdays 2021, revised selected papers / edited by voevodin vladimir; sobolev sergey. springer science and business media deutschland gmbh, 2021, p. 256-269 256-269","order":234,"static_url":"/publications/280/"},{"section":"Publications","title":"Sound reflection of acoustic porous metasurfaces under uniform mean flow","url":"/publications/279/","summary":"Qu, Renhao; Guo, Jingwen; Fang, Yi; Yi, Wei; Zhong, Siyang; Zhang, Xin. “Sound reflection of acoustic porous metasurfaces under uniform mean flow.” Proceedings of INTER-NOISE 2021 - 2021 International Congress and Exposition of Noise Control Engineering / edited by Dare Tyler; B…","meta":"Conference paper · 2021","search_text":"sound reflection of acoustic porous metasurfaces under uniform mean flow qu, renhao; guo, jingwen; fang, yi; yi, wei; zhong, siyang; zhang, xin. “sound reflection of acoustic porous metasurfaces under uniform mean flow.” proceedings of inter-noise 2021 - 2021 international congress and exposition of noise control engineering / edited by dare tyler; bolton stuart; davies patricia; xue yutong; ebbitt gordon. the institute of noise control engineering of the usa, inc., 2021. (2021). doi: 10.3397/in-2021-2182. conference paper · 2021 qu, renhao; guo, jingwen; fang, yi; yi, wei; zhong, siyang; zhang, xin 2021 10.3397/in-2021-2182 proceedings of inter-noise 2021 - 2021 international congress and exposition of noise control engineering / edited by dare tyler; bolton stuart; davies patricia; xue yutong; ebbitt gordon. the institute of noise control engineering of the usa, inc., 2021","order":235,"static_url":"/publications/279/"},{"section":"Publications","title":"Simulation of multi-rotor powered urban aerial mobility noise for environmental assessment","url":"/publications/278/","summary":"Tan, Qichen; Bian, Haoyu; Zhong, Siyang; Zhang, Xin. “Simulation of multi-rotor powered urban aerial mobility noise for environmental assessment.” Proceedings of INTER-NOISE 2021 - 2021 International Congress and Exposition of Noise Control Engineering / edited by Dare Tyler; Bo…","meta":"Conference paper · 2021","search_text":"simulation of multi-rotor powered urban aerial mobility noise for environmental assessment tan, qichen; bian, haoyu; zhong, siyang; zhang, xin. “simulation of multi-rotor powered urban aerial mobility noise for environmental assessment.” proceedings of inter-noise 2021 - 2021 international congress and exposition of noise control engineering / edited by dare tyler; bolton stuart; davies patricia; xue yutong; ebbitt gordon. the institute of noise control engineering of the usa, inc., 2021. (2021). doi: 10.3397/in-2021-2541. conference paper · 2021 tan, qichen; bian, haoyu; zhong, siyang; zhang, xin 2021 10.3397/in-2021-2541 proceedings of inter-noise 2021 - 2021 international congress and exposition of noise control engineering / edited by dare tyler; bolton stuart; davies patricia; xue yutong; ebbitt gordon. the institute of noise control engineering of the usa, inc., 2021","order":236,"static_url":"/publications/278/"},{"section":"Publications","title":"Simulation of Helmholtz resonator using immersed boundary method","url":"/publications/277/","summary":"Ying, Wei; Zhang, Xin; Zhong, Siyang. “Simulation of Helmholtz resonator using immersed boundary method.” Paper presented at 14th WCCM & ECCOMAS Congress 2020. (2021).","meta":"Conference paper · 2021","search_text":"simulation of helmholtz resonator using immersed boundary method ying, wei; zhang, xin; zhong, siyang. “simulation of helmholtz resonator using immersed boundary method.” paper presented at 14th wccm & eccomas congress 2020. (2021). conference paper · 2021 ying, wei; zhang, xin; zhong, siyang 2021 paper presented at 14th wccm & eccomas congress 2020","order":237,"static_url":"/publications/277/"},{"section":"Publications","title":"Rotor blockage effect simulation using high order sliding grid method","url":"/publications/276/","summary":"Ying, Wei; Fattah, Ryu; Zhong, Siyang; Zhang, Xin; Gea-Aguilera, Fernando. “Rotor blockage effect simulation using high order sliding grid method.” \"Advances in Acoustics, Noise and Vibration - 2021\" Proceedings of the 27th International Congress on Sound and Vibration, ICSV 202…","meta":"Conference paper · 2021","search_text":"rotor blockage effect simulation using high order sliding grid method ying, wei; fattah, ryu; zhong, siyang; zhang, xin; gea-aguilera, fernando. “rotor blockage effect simulation using high order sliding grid method.” \"advances in acoustics, noise and vibration - 2021\" proceedings of the 27th international congress on sound and vibration, icsv 2021 / edited by carletti eleonora; crocker malcolm; pawelczyk marek; tuma jiri. silesian university press, 2021. (2021). conference paper · 2021 ying, wei; fattah, ryu; zhong, siyang; zhang, xin; gea-aguilera, fernando 2021 \"advances in acoustics, noise and vibration - 2021\" proceedings of the 27th international congress on sound and vibration, icsv 2021 / edited by carletti eleonora; crocker malcolm; pawelczyk marek; tuma jiri. silesian university press, 2021","order":238,"static_url":"/publications/276/"},{"section":"Publications","title":"Numerical simulations of small-scale shrouded propellers","url":"/publications/275/","summary":"Cantos Trigo, Sinforiano Sebastian; Jiang, Hanbo; Wu, Han; Zhang, Xin; Zhong, Siyang. “Numerical simulations of small-scale shrouded propellers.” Paper presented at 50th International Congress and Exposition on Noise Control Engineering (InterNoise 2021). (2021).","meta":"Conference paper · 2021","search_text":"numerical simulations of small-scale shrouded propellers cantos trigo, sinforiano sebastian; jiang, hanbo; wu, han; zhang, xin; zhong, siyang. “numerical simulations of small-scale shrouded propellers.” paper presented at 50th international congress and exposition on noise control engineering (internoise 2021). (2021). conference paper · 2021 cantos trigo, sinforiano sebastian; jiang, hanbo; wu, han; zhang, xin; zhong, siyang 2021 paper presented at 50th international congress and exposition on noise control engineering (internoise 2021)","order":239,"static_url":"/publications/275/"},{"section":"Publications","title":"Experimental assessment of the noise characteristics of propellers for commercial drones","url":"/publications/274/","summary":"Wu, Han; Zhou, Peng; Zhong, Siyang; Zhang, Xin; Li, Qiang; Luo, Kunyu. “Experimental assessment of the noise characteristics of propellers for commercial drones.” Proceedings of INTER-NOISE 2021 - 2021 International Congress and Exposition of Noise Control Engineering / edited b…","meta":"Conference paper · 2021","search_text":"experimental assessment of the noise characteristics of propellers for commercial drones wu, han; zhou, peng; zhong, siyang; zhang, xin; li, qiang; luo, kunyu. “experimental assessment of the noise characteristics of propellers for commercial drones.” proceedings of inter-noise 2021 - 2021 international congress and exposition of noise control engineering / edited by dare tyler; bolton stuart; davies patricia; xue yutong; ebbitt gordon. the institute of noise control engineering of the usa, inc., 2021. (2021). doi: 10.3397/in-2021-2697. conference paper · 2021 wu, han; zhou, peng; zhong, siyang; zhang, xin; li, qiang; luo, kunyu 2021 10.3397/in-2021-2697 proceedings of inter-noise 2021 - 2021 international congress and exposition of noise control engineering / edited by dare tyler; bolton stuart; davies patricia; xue yutong; ebbitt gordon. the institute of noise control engineering of the usa, inc., 2021","order":240,"static_url":"/publications/274/"},{"section":"Publications","title":"Assessment of UAM noise impact on the environment based on virtual flights with realistic sources","url":"/publications/273/","summary":"Bian, Haoyu; Zhang, Xin; Zhong, Siyang. “Assessment of UAM noise impact on the environment based on virtual flights with realistic sources.” Paper presented at Delft International Conference on Urban Air-Mobility (DICUAM 2021). (2021).","meta":"Conference paper · 2021","search_text":"assessment of uam noise impact on the environment based on virtual flights with realistic sources bian, haoyu; zhang, xin; zhong, siyang. “assessment of uam noise impact on the environment based on virtual flights with realistic sources.” paper presented at delft international conference on urban air-mobility (dicuam 2021). (2021). conference paper · 2021 bian, haoyu; zhang, xin; zhong, siyang 2021 paper presented at delft international conference on urban air-mobility (dicuam 2021)","order":241,"static_url":"/publications/273/"},{"section":"Publications","title":"An experimental investigation of turbulent flow over a two-dimensional obstacle on a flat plate","url":"/publications/272/","summary":"Sundeep, Shivam; Bu, Huanxian; Zhou, Peng; Zhong, Siyang; Zhang, Xin. “An experimental investigation of turbulent flow over a two-dimensional obstacle on a flat plate.” Proceedings of INTER-NOISE 2021 - 2021 International Congress and Exposition of Noise Control Engineering / ed…","meta":"Conference paper · 2021","search_text":"an experimental investigation of turbulent flow over a two-dimensional obstacle on a flat plate sundeep, shivam; bu, huanxian; zhou, peng; zhong, siyang; zhang, xin. “an experimental investigation of turbulent flow over a two-dimensional obstacle on a flat plate.” proceedings of inter-noise 2021 - 2021 international congress and exposition of noise control engineering / edited by dare tyler; bolton stuart; davies patricia; xue yutong; ebbitt gordon. the institute of noise control engineering of the usa, inc., 2021. (2021). doi: 10.3397/in-2021-2711. conference paper · 2021 sundeep, shivam; bu, huanxian; zhou, peng; zhong, siyang; zhang, xin 2021 10.3397/in-2021-2711 proceedings of inter-noise 2021 - 2021 international congress and exposition of noise control engineering / edited by dare tyler; bolton stuart; davies patricia; xue yutong; ebbitt gordon. the institute of noise control engineering of the usa, inc., 2021","order":242,"static_url":"/publications/272/"},{"section":"Publications","title":"Aeroacoustic measurements of dual-rotor interactions","url":"/publications/271/","summary":"Bu, Huanxian; Wu, Han; Ryu, Fattah; Zhong, Siyang; Huang, Xun; Zhang, Xin. “Aeroacoustic measurements of dual-rotor interactions.” \"Advances in Acoustics, Noise and Vibration - 2021\" Proceedings of the 27th International Congress on Sound and Vibration, ICSV 2021 / edited by Car…","meta":"Conference paper · 2021","search_text":"aeroacoustic measurements of dual-rotor interactions bu, huanxian; wu, han; ryu, fattah; zhong, siyang; huang, xun; zhang, xin. “aeroacoustic measurements of dual-rotor interactions.” \"advances in acoustics, noise and vibration - 2021\" proceedings of the 27th international congress on sound and vibration, icsv 2021 / edited by carletti eleonora; crocker malcolm; pawelczyk marek; tuma jiri. silesian university press, 2021. (2021). conference paper · 2021 bu, huanxian; wu, han; ryu, fattah; zhong, siyang; huang, xun; zhang, xin 2021 \"advances in acoustics, noise and vibration - 2021\" proceedings of the 27th international congress on sound and vibration, icsv 2021 / edited by carletti eleonora; crocker malcolm; pawelczyk marek; tuma jiri. silesian university press, 2021","order":243,"static_url":"/publications/271/"},{"section":"Publications","title":"Acoustic scattering in the noise prediction of urban air mobility","url":"/publications/270/","summary":"Jiang, Hanbo; Zhang, Xin; Zhong, Siyang. “Acoustic scattering in the noise prediction of urban air mobility.” Paper presented at Delft International Conference on Urban Air-Mobility, DICUM 2021. (2021).","meta":"Conference paper · 2021","search_text":"acoustic scattering in the noise prediction of urban air mobility jiang, hanbo; zhang, xin; zhong, siyang. “acoustic scattering in the noise prediction of urban air mobility.” paper presented at delft international conference on urban air-mobility, dicum 2021. (2021). conference paper · 2021 jiang, hanbo; zhang, xin; zhong, siyang 2021 paper presented at delft international conference on urban air-mobility, dicum 2021","order":244,"static_url":"/publications/270/"},{"section":"Publications","title":"Acoustic scattering in the noise prediction of urban aerial vehicles","url":"/publications/269/","summary":"Jiang, Hanbo; Zhang, Xin; Zheng, Chuntai; Zhong, Siyang. “Acoustic scattering in the noise prediction of urban aerial vehicles.” Paper presented at Delft International Conference on Urban Air-Mobility (DICUAM 2021). (2021).","meta":"Conference paper · 2021","search_text":"acoustic scattering in the noise prediction of urban aerial vehicles jiang, hanbo; zhang, xin; zheng, chuntai; zhong, siyang. “acoustic scattering in the noise prediction of urban aerial vehicles.” paper presented at delft international conference on urban air-mobility (dicuam 2021). (2021). conference paper · 2021 jiang, hanbo; zhang, xin; zheng, chuntai; zhong, siyang 2021 paper presented at delft international conference on urban air-mobility (dicuam 2021)","order":245,"static_url":"/publications/269/"},{"section":"Publications","title":"A hybrid and efficient low-noise assessment platform for urban aerial mobility (HELPU)","url":"/publications/268/","summary":"Zhang, Xin; Zhong, Siyang; Fang, Yi; Zhou, Peng; Jiang, Hanbo; Bian, Haoyu; Wu, Han; Zheng, Chuntai; Tan, Qichen; Cantos, Sinforiano; Bu, Huanxian; Ma, Zhida. “A hybrid and efficient low-noise assessment platform for urban aerial mobility (HELPU).” Proceedings of INTER-NOISE 202…","meta":"Conference paper · 2021","search_text":"a hybrid and efficient low-noise assessment platform for urban aerial mobility (helpu) zhang, xin; zhong, siyang; fang, yi; zhou, peng; jiang, hanbo; bian, haoyu; wu, han; zheng, chuntai; tan, qichen; cantos, sinforiano; bu, huanxian; ma, zhida. “a hybrid and efficient low-noise assessment platform for urban aerial mobility (helpu).” proceedings of inter-noise 2021 - 2021 international congress and exposition of noise control engineering / edited by dare tyler; bolton stuart; davies patricia; xue yutong; ebbitt gordon. the institute of noise control engineering of the usa, inc., 2021. (2021). doi: 10.3397/in-2021-2509. conference paper · 2021 zhang, xin; zhong, siyang; fang, yi; zhou, peng; jiang, hanbo; bian, haoyu; wu, han; zheng, chuntai; tan, qichen; cantos, sinforiano; bu, huanxian; ma, zhida 2021 10.3397/in-2021-2509 proceedings of inter-noise 2021 - 2021 international congress and exposition of noise control engineering / edited by dare tyler; bolton stuart; davies patricia; xue yutong; ebbitt gordon. the institute of noise control engineering of the usa, inc., 2021","order":246,"static_url":"/publications/268/"},{"section":"Publications","title":"A high-fidelity diagnostic facility for characterization of liners performance under grazing flow","url":"/publications/267/","summary":"Fang, Yi; Guo, Jingwen; Qu, Renhao; Yi, Wei; Zhang, Xin; Zhong, Siyang. “A high-fidelity diagnostic facility for characterization of liners performance under grazing flow.” Paper presented at 50th International Congress and Exposition on Noise Control Engineering (InterNoise 202…","meta":"Conference paper · 2021","search_text":"a high-fidelity diagnostic facility for characterization of liners performance under grazing flow fang, yi; guo, jingwen; qu, renhao; yi, wei; zhang, xin; zhong, siyang. “a high-fidelity diagnostic facility for characterization of liners performance under grazing flow.” paper presented at 50th international congress and exposition on noise control engineering (internoise 2021). (2021). conference paper · 2021 fang, yi; guo, jingwen; qu, renhao; yi, wei; zhang, xin; zhong, siyang 2021 paper presented at 50th international congress and exposition on noise control engineering (internoise 2021)","order":247,"static_url":"/publications/267/"},{"section":"Publications","title":"A flow and acoustic facility for characterization of liner and meta-acoustic surfaces under grazing flow condition","url":"/publications/266/","summary":"Yi, Wei; Guo, Jingwen; Fang, Yi; Qu, Renhao; Zhong, Siyang; Zhang, Xin. “A flow and acoustic facility for characterization of liner and meta-acoustic surfaces under grazing flow condition.” Proceedings of INTER-NOISE 2021 - 2021 International Congress and Exposition of Noise Con…","meta":"Conference paper · 2021","search_text":"a flow and acoustic facility for characterization of liner and meta-acoustic surfaces under grazing flow condition yi, wei; guo, jingwen; fang, yi; qu, renhao; zhong, siyang; zhang, xin. “a flow and acoustic facility for characterization of liner and meta-acoustic surfaces under grazing flow condition.” proceedings of inter-noise 2021 - 2021 international congress and exposition of noise control engineering / edited by dare tyler; bolton stuart; davies patricia; xue yutong; ebbitt gordon. the institute of noise control engineering of the usa, inc., 2021. (2021). doi: 10.3397/in-2021-2324. conference paper · 2021 yi, wei; guo, jingwen; fang, yi; qu, renhao; zhong, siyang; zhang, xin 2021 10.3397/in-2021-2324 proceedings of inter-noise 2021 - 2021 international congress and exposition of noise control engineering / edited by dare tyler; bolton stuart; davies patricia; xue yutong; ebbitt gordon. the institute of noise control engineering of the usa, inc., 2021","order":248,"static_url":"/publications/266/"},{"section":"Publications","title":"Broadband Aerodynamic Noise Simulation Using Synthetic Turbulence Methods","url":"/publications/265/","summary":"Zhang, Xin; Zhong, Siyang. “Broadband Aerodynamic Noise Simulation Using Synthetic Turbulence Methods.” Flinovia-Flow Induced Noise and Vibration Issues and Aspects-III / Springer International Publishing, 2021, p. 377-398 (2021). DOI: 10.1007/978-3-030-64807-7_18.","meta":"Book chapter · 2021","search_text":"broadband aerodynamic noise simulation using synthetic turbulence methods zhang, xin; zhong, siyang. “broadband aerodynamic noise simulation using synthetic turbulence methods.” flinovia-flow induced noise and vibration issues and aspects-iii / springer international publishing, 2021, p. 377-398 (2021). doi: 10.1007/978-3-030-64807-7_18. book chapter · 2021 zhang, xin; zhong, siyang 2021 10.1007/978-3-030-64807-7_18 flinovia-flow induced noise and vibration issues and aspects-iii / springer international publishing, 2021, p. 377-398","order":249,"static_url":"/publications/265/"},{"section":"Publications","title":"Wideband low-frequency sound absorption by inhomogeneous multi-layer resonators with extended necks","url":"/publications/264/","summary":"Guo, Jingwen; Zhang, Xin; Fang, Yi; Jiang, Ziyan. “Wideband low-frequency sound absorption by inhomogeneous multi-layer resonators with extended necks.” Composite Structures, v. 260, article number 113538. (2021). DOI: 10.1016/j.compstruct.2020.113538.","meta":"Journal article · 2021","search_text":"wideband low-frequency sound absorption by inhomogeneous multi-layer resonators with extended necks guo, jingwen; zhang, xin; fang, yi; jiang, ziyan. “wideband low-frequency sound absorption by inhomogeneous multi-layer resonators with extended necks.” composite structures, v. 260, article number 113538. (2021). doi: 10.1016/j.compstruct.2020.113538. journal article · 2021 guo, jingwen; zhang, xin; fang, yi; jiang, ziyan 2021 10.1016/j.compstruct.2020.113538 composite structures 260 article 113538","order":250,"static_url":"/publications/264/"},{"section":"Publications","title":"Ultralight Metamaterial for Sound Absorption Based on Miura-Ori Tessellation Structures","url":"/publications/263/","summary":"Wang, Yixin; Guo, Jingwen; Fang, Yi; Zhang, Xin; Yu, Hongyu. “Ultralight Metamaterial for Sound Absorption Based on Miura-Ori Tessellation Structures.” Advanced Engineering Materials, v. 23, (12), article number 2100563. (2021). DOI: 10.1002/adem.202100563.","meta":"Journal article · 2021","search_text":"ultralight metamaterial for sound absorption based on miura-ori tessellation structures wang, yixin; guo, jingwen; fang, yi; zhang, xin; yu, hongyu. “ultralight metamaterial for sound absorption based on miura-ori tessellation structures.” advanced engineering materials, v. 23, (12), article number 2100563. (2021). doi: 10.1002/adem.202100563. journal article · 2021 wang, yixin; guo, jingwen; fang, yi; zhang, xin; yu, hongyu 2021 10.1002/adem.202100563 advanced engineering materials 23 (12) article 2100563","order":251,"static_url":"/publications/263/"},{"section":"Publications","title":"Propulsive efficiency and efficacy of a pumping sail","url":"/publications/262/","summary":"Zhou, Peng; Zhong, Siyang; Jiang, Hanbo; Zhang, Xin; So, Raymond Chi Hung. “Propulsive efficiency and efficacy of a pumping sail.” Physics of Fluids, v. 33, (10), article number 107105. (2021). DOI: 10.1063/5.0065561.","meta":"Journal article · 2021","search_text":"propulsive efficiency and efficacy of a pumping sail zhou, peng; zhong, siyang; jiang, hanbo; zhang, xin; so, raymond chi hung. “propulsive efficiency and efficacy of a pumping sail.” physics of fluids, v. 33, (10), article number 107105. (2021). doi: 10.1063/5.0065561. journal article · 2021 zhou, peng; zhong, siyang; jiang, hanbo; zhang, xin; so, raymond chi hung 2021 10.1063/5.0065561 physics of fluids 33 (10) article 107105","order":252,"static_url":"/publications/262/"},{"section":"Publications","title":"On the efficient modeling of generic source directivity in Gaussian beam tracing","url":"/publications/261/","summary":"Bian, Haoyu; Fattah, Ryu; Zhong, Siyang; Zhang, Xin. “On the efficient modeling of generic source directivity in Gaussian beam tracing.” Journal of the Acoustical Society of America, v. 149, (4), p. 2743-2751. (2021). DOI: 10.1121/10.0004318.","meta":"Journal article · 2021","search_text":"on the efficient modeling of generic source directivity in gaussian beam tracing bian, haoyu; fattah, ryu; zhong, siyang; zhang, xin. “on the efficient modeling of generic source directivity in gaussian beam tracing.” journal of the acoustical society of america, v. 149, (4), p. 2743-2751. (2021). doi: 10.1121/10.0004318. journal article · 2021 bian, haoyu; fattah, ryu; zhong, siyang; zhang, xin 2021 10.1121/10.0004318 journal of the acoustical society of america 149 (4) 2743-2751","order":253,"static_url":"/publications/261/"},{"section":"Publications","title":"On the effects of anisotropic turbulence on leading edge noise","url":"/publications/260/","summary":"Gea-Aguilera, Fernando; Karve, Ravish; Gill, James; Zhang, Xin; Angland, David. “On the effects of anisotropic turbulence on leading edge noise.” Journal of Sound and Vibration, v. 495, article number 115895 (2021). DOI: 10.1016/j.jsv.2020.115895.","meta":"Journal article · 2021","search_text":"on the effects of anisotropic turbulence on leading edge noise gea-aguilera, fernando; karve, ravish; gill, james; zhang, xin; angland, david. “on the effects of anisotropic turbulence on leading edge noise.” journal of sound and vibration, v. 495, article number 115895 (2021). doi: 10.1016/j.jsv.2020.115895. journal article · 2021 gea-aguilera, fernando; karve, ravish; gill, james; zhang, xin; angland, david 2021 10.1016/j.jsv.2020.115895 journal of sound and vibration, v. 495, article number 115895","order":254,"static_url":"/publications/260/"},{"section":"Publications","title":"On the effect of velvet structures on trailing edge noise: Experimental investigation and theoretical analysis","url":"/publications/259/","summary":"Zhou, Peng; Zhong, Siyang; Zhang, Xin. “On the effect of velvet structures on trailing edge noise: Experimental investigation and theoretical analysis.” Journal of Fluid Mechanics, v. 919, article number A11. (2021). DOI: 10.1017/jfm.2021.374.","meta":"Journal article · 2021","search_text":"on the effect of velvet structures on trailing edge noise: experimental investigation and theoretical analysis zhou, peng; zhong, siyang; zhang, xin. “on the effect of velvet structures on trailing edge noise: experimental investigation and theoretical analysis.” journal of fluid mechanics, v. 919, article number a11. (2021). doi: 10.1017/jfm.2021.374. journal article · 2021 zhou, peng; zhong, siyang; zhang, xin 2021 10.1017/jfm.2021.374 journal of fluid mechanics 919 article a11","order":255,"static_url":"/publications/259/"},{"section":"Publications","title":"Experimental study on a compact lined circular duct for small-scale propeller noise reduction","url":"/publications/258/","summary":"Guo, Jingwen; Zhou, Teng; Fang, Yi; Zhang, Xin. “Experimental study on a compact lined circular duct for small-scale propeller noise reduction.” Applied Acoustics, v. 179, article number 108062. (2021). DOI: 10.1016/j.apacoust.2021.108062.","meta":"Journal article · 2021","search_text":"experimental study on a compact lined circular duct for small-scale propeller noise reduction guo, jingwen; zhou, teng; fang, yi; zhang, xin. “experimental study on a compact lined circular duct for small-scale propeller noise reduction.” applied acoustics, v. 179, article number 108062. (2021). doi: 10.1016/j.apacoust.2021.108062. journal article · 2021 guo, jingwen; zhou, teng; fang, yi; zhang, xin 2021 10.1016/j.apacoust.2021.108062 applied acoustics 179 article 108062","order":256,"static_url":"/publications/258/"},{"section":"Publications","title":"Design and characterization of a multifunctional low-speed anechoic wind tunnel at HKUST","url":"/publications/257/","summary":"Yi, Wei; Zhou, Peng; Fang, Yi; Guo, Jingwen; Zhong, Siyang; Zhang, Xin; Huang, Xun; Zhou, Guocheng; Chen, Bao. “Design and characterization of a multifunctional low-speed anechoic wind tunnel at HKUST.” Aerospace Science and Technology, v. 115, article number 106814. (2021). DOI…","meta":"Journal article · 2021","search_text":"design and characterization of a multifunctional low-speed anechoic wind tunnel at hkust yi, wei; zhou, peng; fang, yi; guo, jingwen; zhong, siyang; zhang, xin; huang, xun; zhou, guocheng; chen, bao. “design and characterization of a multifunctional low-speed anechoic wind tunnel at hkust.” aerospace science and technology, v. 115, article number 106814. (2021). doi: 10.1016/j.ast.2021.106814. journal article · 2021 yi, wei; zhou, peng; fang, yi; guo, jingwen; zhong, siyang; zhang, xin; huang, xun; zhou, guocheng; chen, bao 2021 10.1016/j.ast.2021.106814 aerospace science and technology 115 article 106814","order":257,"static_url":"/publications/257/"},{"section":"Publications","title":"Assessment of UAM and drone noise impact on the environment based on virtual flights","url":"/publications/256/","summary":"Bian, Haoyu; Tan, Qichen; Zhong, Siyang; Zhang, Xin. “Assessment of UAM and drone noise impact on the environment based on virtual flights.” Aerospace Science and Technology, v. 118, article number 106996. (2021). DOI: 10.1016/j.ast.2021.106996.","meta":"Journal article · 2021","search_text":"assessment of uam and drone noise impact on the environment based on virtual flights bian, haoyu; tan, qichen; zhong, siyang; zhang, xin. “assessment of uam and drone noise impact on the environment based on virtual flights.” aerospace science and technology, v. 118, article number 106996. (2021). doi: 10.1016/j.ast.2021.106996. journal article · 2021 bian, haoyu; tan, qichen; zhong, siyang; zhang, xin 2021 10.1016/j.ast.2021.106996 aerospace science and technology 118 article 106996","order":258,"static_url":"/publications/256/"},{"section":"Publications","title":"An overview of testing methods for aeroengine fan noise","url":"/publications/255/","summary":"Bu, Huanxian; Huang, Xun; Zhang, Xin. “An overview of testing methods for aeroengine fan noise.” Progress in Aerospace Sciences, v. 124, article number 100722. (2021). DOI: 10.1016/j.paerosci.2021.100722.","meta":"Journal article · 2021","search_text":"an overview of testing methods for aeroengine fan noise bu, huanxian; huang, xun; zhang, xin. “an overview of testing methods for aeroengine fan noise.” progress in aerospace sciences, v. 124, article number 100722. (2021). doi: 10.1016/j.paerosci.2021.100722. journal article · 2021 bu, huanxian; huang, xun; zhang, xin 2021 10.1016/j.paerosci.2021.100722 progress in aerospace sciences 124 article 100722","order":259,"static_url":"/publications/255/"},{"section":"Publications","title":"An investigation on noise attenuation by acoustic liner constructed by Helmholtz resonators with extended necks","url":"/publications/254/","summary":"Guo, Jingwen; Fang, Yi; Jiang, Ziyan; Zhang, Xin. “An investigation on noise attenuation by acoustic liner constructed by Helmholtz resonators with extended necks.” Journal of the Acoustical Society of America, v. 149, (1), p. 70-81. (2021). DOI: 10.1121/10.0002990.","meta":"Journal article · 2021","search_text":"an investigation on noise attenuation by acoustic liner constructed by helmholtz resonators with extended necks guo, jingwen; fang, yi; jiang, ziyan; zhang, xin. “an investigation on noise attenuation by acoustic liner constructed by helmholtz resonators with extended necks.” journal of the acoustical society of america, v. 149, (1), p. 70-81. (2021). doi: 10.1121/10.0002990. journal article · 2021 guo, jingwen; fang, yi; jiang, ziyan; zhang, xin 2021 10.1121/10.0002990 journal of the acoustical society of america 149 (1) 70-81","order":260,"static_url":"/publications/254/"},{"section":"Publications","title":"An extra-broadband compact sound-absorbing structure composing of double-layer resonator with multiple perforations","url":"/publications/253/","summary":"Guo, Jingwen; Fang, Yi; Qu, Renhao; Liu, Qian; Zhang, Xin. “An extra-broadband compact sound-absorbing structure composing of double-layer resonator with multiple perforations.” Journal of the Acoustical Society of America, v. 150, (2), p. 1370-1380. (2021). DOI: 10.1121/10.0005…","meta":"Journal article · 2021","search_text":"an extra-broadband compact sound-absorbing structure composing of double-layer resonator with multiple perforations guo, jingwen; fang, yi; qu, renhao; liu, qian; zhang, xin. “an extra-broadband compact sound-absorbing structure composing of double-layer resonator with multiple perforations.” journal of the acoustical society of america, v. 150, (2), p. 1370-1380. (2021). doi: 10.1121/10.0005912. journal article · 2021 guo, jingwen; fang, yi; qu, renhao; liu, qian; zhang, xin 2021 10.1121/10.0005912 journal of the acoustical society of america 150 (2) 1370-1380","order":261,"static_url":"/publications/253/"},{"section":"Publications","title":"An experimental investigation of drag and noise reduction from a circular cylinder using longitudinal grooves","url":"/publications/252/","summary":"Zheng, Chuntai; Zhou, Peng; Zhong, Siyang; Zhang, Xin; Huang, Xun; So, Raymond Chi Hung. “An experimental investigation of drag and noise reduction from a circular cylinder using longitudinal grooves.” Physics of Fluids, v. 33, (11), article number 115110. (2021). DOI: 10.1063/5…","meta":"Journal article · 2021","search_text":"an experimental investigation of drag and noise reduction from a circular cylinder using longitudinal grooves zheng, chuntai; zhou, peng; zhong, siyang; zhang, xin; huang, xun; so, raymond chi hung. “an experimental investigation of drag and noise reduction from a circular cylinder using longitudinal grooves.” physics of fluids, v. 33, (11), article number 115110. (2021). doi: 10.1063/5.0070959. journal article · 2021 zheng, chuntai; zhou, peng; zhong, siyang; zhang, xin; huang, xun; so, raymond chi hung 2021 10.1063/5.0070959 physics of fluids 33 (11) article 115110","order":262,"static_url":"/publications/252/"},{"section":"Publications","title":"A numerical investigation of the rotor blockage effect on cascade noise using a sliding mesh method","url":"/publications/251/","summary":"Ying, Wei; Fattah, Ryu; Zhong, Siyang; Zhang, Xin; Gea-Aguilera, Fernando. “A numerical investigation of the rotor blockage effect on cascade noise using a sliding mesh method.” Journal of Sound and Vibration, v. 502, article number 116030. (2021). DOI: 10.1016/j.jsv.2021.116030.","meta":"Journal article · 2021","search_text":"a numerical investigation of the rotor blockage effect on cascade noise using a sliding mesh method ying, wei; fattah, ryu; zhong, siyang; zhang, xin; gea-aguilera, fernando. “a numerical investigation of the rotor blockage effect on cascade noise using a sliding mesh method.” journal of sound and vibration, v. 502, article number 116030. (2021). doi: 10.1016/j.jsv.2021.116030. journal article · 2021 ying, wei; fattah, ryu; zhong, siyang; zhang, xin; gea-aguilera, fernando 2021 10.1016/j.jsv.2021.116030 journal of sound and vibration 502 article 116030","order":263,"static_url":"/publications/251/"},{"section":"Publications","title":"Aerodynamic and acoustic measurements of dual small-scale propellers","url":"/publications/143/","summary":"Huanxian, Bu & Wu, Han & Bertin, Celia & Fang, Yi & Zhong, Siyang. (2021). Aerodynamic and acoustic measurements of dual small-scale propellers. Journal of Sound and Vibration. 511. 116330. 10.1016/j.jsv.2021.116330.","meta":"Journal article · 2021","search_text":"aerodynamic and acoustic measurements of dual small-scale propellers huanxian, bu & wu, han & bertin, celia & fang, yi & zhong, siyang. (2021). aerodynamic and acoustic measurements of dual small-scale propellers. journal of sound and vibration. 511. 116330. 10.1016/j.jsv.2021.116330. journal article · 2021 huanxian bu; han wu; celia bertin; yi fang; siyang zhong 2021 10.1016/j.jsv.2021.116330 journal of sound and vibration 511 116330","order":264,"static_url":"/publications/143/"},{"section":"Publications","title":"Spinning Wave Scattering From a Flow Pipe With Serrations","url":"/publications/139/","summary":"Jiang H, Huang X. Spinning wave scattering from a flow pipe with serrations. Journal of Vibration and Acoustics. 2021 Aug 1;143(4).","meta":"Journal article · 2021","search_text":"spinning wave scattering from a flow pipe with serrations jiang h, huang x. spinning wave scattering from a flow pipe with serrations. journal of vibration and acoustics. 2021 aug 1;143(4). journal article · 2021 hanbo jiang; xun huang 2021 10.1115/1.4048891 journal of vibration and acoustics 143 (4)","order":265,"static_url":"/publications/139/"},{"section":"Publications","title":"Efficient storage and interpolation of acoustic transfer functions","url":"/publications/138/","summary":"Jiang, Hanbo; Zhong, Siyang; Zhang, Xin; Huang, Xun. “Efficient storage and interpolation of acoustic transfer functions.” Engineering Analysis with Boundary Elements, v. 124, p. 259-265. (2021). DOI: 10.1016/j.enganabound.2020.12.024.","meta":"Journal article · 2021","search_text":"efficient storage and interpolation of acoustic transfer functions jiang, hanbo; zhong, siyang; zhang, xin; huang, xun. “efficient storage and interpolation of acoustic transfer functions.” engineering analysis with boundary elements, v. 124, p. 259-265. (2021). doi: 10.1016/j.enganabound.2020.12.024. journal article · 2021 jiang, hanbo; zhong, siyang; zhang, xin; huang, xun 2021 10.1016/j.enganabound.2020.12.024 engineering analysis with boundary elements 124 259-265","order":266,"static_url":"/publications/138/"},{"section":"Publications","title":"Multi-rotor powered drone noise assessment","url":"/publications/302/","summary":"Zhang, Xin; Zhong, Siyang. “Multi-rotor powered drone noise assessment.” Paper presented at Quiet Drones 2020: International e-Symposium on Noise of UAV/UAS. (2020).","meta":"Conference paper · 2020","search_text":"multi-rotor powered drone noise assessment zhang, xin; zhong, siyang. “multi-rotor powered drone noise assessment.” paper presented at quiet drones 2020: international e-symposium on noise of uav/uas. (2020). conference paper · 2020 zhang, xin; zhong, siyang 2020 paper presented at quiet drones 2020: international e-symposium on noise of uav/uas","order":267,"static_url":"/publications/302/"},{"section":"Publications","title":"Interpolation based acoustic transfer function for drone noise simulation","url":"/publications/301/","summary":"Jiang, Hanbo; Zhang, Xin; Zhong, Siyang. “Interpolation based acoustic transfer function for drone noise simulation.” Paper presented at Quiet Drones 2020: International e-Symposium on Noise of UAV/UAS. (2020).","meta":"Conference paper · 2020","search_text":"interpolation based acoustic transfer function for drone noise simulation jiang, hanbo; zhang, xin; zhong, siyang. “interpolation based acoustic transfer function for drone noise simulation.” paper presented at quiet drones 2020: international e-symposium on noise of uav/uas. (2020). conference paper · 2020 jiang, hanbo; zhang, xin; zhong, siyang 2020 paper presented at quiet drones 2020: international e-symposium on noise of uav/uas","order":268,"static_url":"/publications/301/"},{"section":"Publications","title":"Geometric shape effects of cavity and neck on acoustic absorption performance of helmholtz resonator with extended neck","url":"/publications/300/","summary":"Jiang, Ziyan; Guo, Jingwen; Fang, Yi; Liu, Qian; Zhang, Xin; Zhou, Guocheng; Chen, Bao. “Geometric shape effects of cavity and neck on acoustic absorption performance of helmholtz resonator with extended neck.” Proceedings of 2020 International Congress on Noise Control Engineer…","meta":"Conference paper · 2020","search_text":"geometric shape effects of cavity and neck on acoustic absorption performance of helmholtz resonator with extended neck jiang, ziyan; guo, jingwen; fang, yi; liu, qian; zhang, xin; zhou, guocheng; chen, bao. “geometric shape effects of cavity and neck on acoustic absorption performance of helmholtz resonator with extended neck.” proceedings of 2020 international congress on noise control engineering, inter-noise 2020 / edited by jeon jin yong. korean society of noise and vibration engineering, 2020. (2020). conference paper · 2020 jiang, ziyan; guo, jingwen; fang, yi; liu, qian; zhang, xin; zhou, guocheng; chen, bao 2020 proceedings of 2020 international congress on noise control engineering, inter-noise 2020 / edited by jeon jin yong. korean society of noise and vibration engineering, 2020","order":269,"static_url":"/publications/300/"},{"section":"Publications","title":"Assessment of the environmental impact of drone noise in virtual flights","url":"/publications/299/","summary":"Bian, Haoyu; Fattah, Ryu Jahangir; Zhang, Xin; Zhong, Siyang. “Assessment of the environmental impact of drone noise in virtual flights.” Paper presented at Quiet Drones 2020: International e-Symposium on Noise of UAV/UAS. (2020).","meta":"Conference paper · 2020","search_text":"assessment of the environmental impact of drone noise in virtual flights bian, haoyu; fattah, ryu jahangir; zhang, xin; zhong, siyang. “assessment of the environmental impact of drone noise in virtual flights.” paper presented at quiet drones 2020: international e-symposium on noise of uav/uas. (2020). conference paper · 2020 bian, haoyu; fattah, ryu jahangir; zhang, xin; zhong, siyang 2020 paper presented at quiet drones 2020: international e-symposium on noise of uav/uas","order":270,"static_url":"/publications/299/"},{"section":"Publications","title":"Aerodynamic measurements of a single wheel in ground effect","url":"/publications/298/","summary":"Yi, Wei; Morris, Sandy Y.; Zhou, Peng; Ying, Wei; Zhang, Xin. “Aerodynamic measurements of a single wheel in ground effect.” AIAA AVIATION 2020 FORUM, American Institute of Aeronautics and Astronautics Inc, AIAA, 2020. (2020). DOI: 10.2514/6.2020-2784.","meta":"Conference paper · 2020","search_text":"aerodynamic measurements of a single wheel in ground effect yi, wei; morris, sandy y.; zhou, peng; ying, wei; zhang, xin. “aerodynamic measurements of a single wheel in ground effect.” aiaa aviation 2020 forum, american institute of aeronautics and astronautics inc, aiaa, 2020. (2020). doi: 10.2514/6.2020-2784. conference paper · 2020 yi, wei; morris, sandy y.; zhou, peng; ying, wei; zhang, xin 2020 10.2514/6.2020-2784 aiaa aviation 2020 forum, american institute of aeronautics and astronautics inc, aiaa, 2020","order":271,"static_url":"/publications/298/"},{"section":"Publications","title":"Aeroacoustic characteristics of metasurfaces with stair-stepping honeycomb structures covered by perforated panels","url":"/publications/297/","summary":"Fang, Yi; Liu, Qian; Guo, Jingwen; Jiang, Ziyan; Wu, Han; Zhong, Siyang; Zhang, Xin. “Aeroacoustic characteristics of metasurfaces with stair-stepping honeycomb structures covered by perforated panels.” INTER-NOISE and NOISE-CON Congress and Conference Proceedings, InterNoise20 …","meta":"Conference paper · 2020","search_text":"aeroacoustic characteristics of metasurfaces with stair-stepping honeycomb structures covered by perforated panels fang, yi; liu, qian; guo, jingwen; jiang, ziyan; wu, han; zhong, siyang; zhang, xin. “aeroacoustic characteristics of metasurfaces with stair-stepping honeycomb structures covered by perforated panels.” inter-noise and noise-con congress and conference proceedings, internoise20 / institute of noise control engineering. institute of noise control engineering, 2020, p. 2467-2475. (2020). conference paper · 2020 fang, yi; liu, qian; guo, jingwen; jiang, ziyan; wu, han; zhong, siyang; zhang, xin 2020 inter-noise and noise-con congress and conference proceedings, internoise20 / institute of noise control engineering. institute of noise control engineering, 2020, p. 2467-2475 2467-2475","order":272,"static_url":"/publications/297/"},{"section":"Publications","title":"A rotor blade aeroacoustics test platform at HKUST","url":"/publications/296/","summary":"Wu, Han; Chen, Weijie; Fattah, Ryu; Guo, Jingwen; Fang, Yi; Zhong, Siyang; Zhang, Xin. “A rotor blade aeroacoustics test platform at HKUST.” Proceedings of 2020 International Congress on Noise Control Engineering, INTER-NOISE 2020 / edited by Jeon Jin Yong. Korean Society of Noi…","meta":"Conference paper · 2020","search_text":"a rotor blade aeroacoustics test platform at hkust wu, han; chen, weijie; fattah, ryu; guo, jingwen; fang, yi; zhong, siyang; zhang, xin. “a rotor blade aeroacoustics test platform at hkust.” proceedings of 2020 international congress on noise control engineering, inter-noise 2020 / edited by jeon jin yong. korean society of noise and vibration engineering, 2020. (2020). conference paper · 2020 wu, han; chen, weijie; fattah, ryu; guo, jingwen; fang, yi; zhong, siyang; zhang, xin 2020 proceedings of 2020 international congress on noise control engineering, inter-noise 2020 / edited by jeon jin yong. korean society of noise and vibration engineering, 2020","order":273,"static_url":"/publications/296/"},{"section":"Publications","title":"Design and testing of a microelectromechanical-system-based high heat flux vaporizing liquid microthruster","url":"/publications/295/","summary":"Kwan, Pok Wang; Huang, Xun; Zhang, Xin. “Design and testing of a microelectromechanical-system-based high heat flux vaporizing liquid microthruster.” Acta Astronautica, v. 170, p. 719-734 (2020). DOI: 10.1016/j.actaastro.2020.01.017.","meta":"Journal article · 2020","search_text":"design and testing of a microelectromechanical-system-based high heat flux vaporizing liquid microthruster kwan, pok wang; huang, xun; zhang, xin. “design and testing of a microelectromechanical-system-based high heat flux vaporizing liquid microthruster.” acta astronautica, v. 170, p. 719-734 (2020). doi: 10.1016/j.actaastro.2020.01.017. journal article · 2020 kwan, pok wang; huang, xun; zhang, xin 2020 10.1016/j.actaastro.2020.01.017 acta astronautica, v. 170, p. 719-734","order":274,"static_url":"/publications/295/"},{"section":"Publications","title":"CAA simulations of the leading edge noise of a heaving airfoil","url":"/publications/294/","summary":"Sun, Yuhao; Zhong, Siyang; Zhou, Teng; Huang, Xun; Zhang, Xin. “CAA simulations of the leading edge noise of a heaving airfoil.” Journal of Sound and Vibration, v. 472, article number 115209. (2020). DOI: 10.1016/j.jsv.2020.115209.","meta":"Journal article · 2020","search_text":"caa simulations of the leading edge noise of a heaving airfoil sun, yuhao; zhong, siyang; zhou, teng; huang, xun; zhang, xin. “caa simulations of the leading edge noise of a heaving airfoil.” journal of sound and vibration, v. 472, article number 115209. (2020). doi: 10.1016/j.jsv.2020.115209. journal article · 2020 sun, yuhao; zhong, siyang; zhou, teng; huang, xun; zhang, xin 2020 10.1016/j.jsv.2020.115209 journal of sound and vibration 472 article 115209","order":275,"static_url":"/publications/294/"},{"section":"Publications","title":"An experimental study of trailing edge noise from a heaving airfoil","url":"/publications/293/","summary":"Zhou, Teng; Zhang, Xin; Zhong, Siyang. “An experimental study of trailing edge noise from a heaving airfoil.” Journal of the Acoustical Society of America, v. 147, (6), p. 4020-4031. (2020). DOI: 10.1121/10.0001419.","meta":"Journal article · 2020","search_text":"an experimental study of trailing edge noise from a heaving airfoil zhou, teng; zhang, xin; zhong, siyang. “an experimental study of trailing edge noise from a heaving airfoil.” journal of the acoustical society of america, v. 147, (6), p. 4020-4031. (2020). doi: 10.1121/10.0001419. journal article · 2020 zhou, teng; zhang, xin; zhong, siyang 2020 10.1121/10.0001419 journal of the acoustical society of america 147 (6) 4020-4031","order":276,"static_url":"/publications/293/"},{"section":"Publications","title":"An efficient rectilinear Gaussian beam tracing method for sound propagation modelling in a non-turbulent medium","url":"/publications/292/","summary":"Bian, Haoyu; Fattah, Ryu; Zhong, Siyang; Zhang, Xin. “An efficient rectilinear Gaussian beam tracing method for sound propagation modelling in a non-turbulent medium.” Journal of the Acoustical Society of America, v. 148, (6), p. 4037-4048. (2020). DOI: 10.1121/10.0002966.","meta":"Journal article · 2020","search_text":"an efficient rectilinear gaussian beam tracing method for sound propagation modelling in a non-turbulent medium bian, haoyu; fattah, ryu; zhong, siyang; zhang, xin. “an efficient rectilinear gaussian beam tracing method for sound propagation modelling in a non-turbulent medium.” journal of the acoustical society of america, v. 148, (6), p. 4037-4048. (2020). doi: 10.1121/10.0002966. journal article · 2020 bian, haoyu; fattah, ryu; zhong, siyang; zhang, xin 2020 10.1121/10.0002966 journal of the acoustical society of america 148 (6) 4037-4048","order":277,"static_url":"/publications/292/"},{"section":"Publications","title":"An analytical correction to Amiet's solution of airfoil leading-edge noise in non-uniform mean flows","url":"/publications/291/","summary":"Zhong, Siyang; Zhang, Xin; Peng, Bo; Huang, Xun. “An analytical correction to Amiet's solution of airfoil leading-edge noise in non-uniform mean flows.” Journal of Fluid Mechanics, v. 882, p. A291-A2932. (2020). DOI: 10.1017/jfm.2019.839.","meta":"Journal article · 2020","search_text":"an analytical correction to amiet's solution of airfoil leading-edge noise in non-uniform mean flows zhong, siyang; zhang, xin; peng, bo; huang, xun. “an analytical correction to amiet's solution of airfoil leading-edge noise in non-uniform mean flows.” journal of fluid mechanics, v. 882, p. a291-a2932. (2020). doi: 10.1017/jfm.2019.839. journal article · 2020 zhong, siyang; zhang, xin; peng, bo; huang, xun 2020 10.1017/jfm.2019.839 journal of fluid mechanics 882 a291-a2932","order":278,"static_url":"/publications/291/"},{"section":"Publications","title":"Acoustic characterizations of Helmholtz resonators with extended necks and their checkerboard combination for sound absorption","url":"/publications/290/","summary":"Guo, Jingwen; Fang, Yi; Jiang, Ziyan; Zhang, Xin. “Acoustic characterizations of Helmholtz resonators with extended necks and their checkerboard combination for sound absorption.” Journal of Physics D: Applied Physics, v. 53, (50), article number 505504. (2020). DOI: 10.1088/136…","meta":"Journal article · 2020","search_text":"acoustic characterizations of helmholtz resonators with extended necks and their checkerboard combination for sound absorption guo, jingwen; fang, yi; jiang, ziyan; zhang, xin. “acoustic characterizations of helmholtz resonators with extended necks and their checkerboard combination for sound absorption.” journal of physics d: applied physics, v. 53, (50), article number 505504. (2020). doi: 10.1088/1361-6463/abb5d8. journal article · 2020 guo, jingwen; fang, yi; jiang, ziyan; zhang, xin 2020 10.1088/1361-6463/abb5d8 journal of physics d: applied physics 53 (50) article 505504","order":279,"static_url":"/publications/290/"},{"section":"Publications","title":"A study of the effect of serration shape and flexibility on trailing edge noise","url":"/publications/289/","summary":"Zhou, Peng; Liu, Qian; Zhong, Siyang; Fang, Yi; Zhang, Xin. “A study of the effect of serration shape and flexibility on trailing edge noise.” Physics of Fluids, v. 32, (12), article number 0032774. (2020). DOI: 10.1063/5.0032774.","meta":"Journal article · 2020","search_text":"a study of the effect of serration shape and flexibility on trailing edge noise zhou, peng; liu, qian; zhong, siyang; fang, yi; zhang, xin. “a study of the effect of serration shape and flexibility on trailing edge noise.” physics of fluids, v. 32, (12), article number 0032774. (2020). doi: 10.1063/5.0032774. journal article · 2020 zhou, peng; liu, qian; zhong, siyang; fang, yi; zhang, xin 2020 10.1063/5.0032774 physics of fluids 32 (12) article 0032774","order":280,"static_url":"/publications/289/"},{"section":"Publications","title":"A revisit of the tonal noise of small rotors","url":"/publications/288/","summary":"Zhong, Siyang; Zhou, Peng; Fattah, Ryu; Zhang, Xin. “A revisit of the tonal noise of small rotors.” Proceedings of the Royal Society A: Mathematical, Physical and Engineering Sciences, v. 476, (2244), article number 20200518. (2020). DOI: 10.1098/rspa.2020.0491.","meta":"Journal article · 2020","search_text":"a revisit of the tonal noise of small rotors zhong, siyang; zhou, peng; fattah, ryu; zhang, xin. “a revisit of the tonal noise of small rotors.” proceedings of the royal society a: mathematical, physical and engineering sciences, v. 476, (2244), article number 20200518. (2020). doi: 10.1098/rspa.2020.0491. journal article · 2020 zhong, siyang; zhou, peng; fattah, ryu; zhang, xin 2020 10.1098/rspa.2020.0491 proceedings of the royal society a: mathematical, physical and engineering sciences 476 (2244) article 20200518","order":281,"static_url":"/publications/288/"},{"section":"Publications","title":"A conceptual study of utilizing compressive-sensing-based fan noise mode detection for aeroengine prognostic and health management","url":"/publications/287/","summary":"Bu, Huanxian; Huang, Xun; Zhang, Xin. “A conceptual study of utilizing compressive-sensing-based fan noise mode detection for aeroengine prognostic and health management.” Journal of the Acoustical Society of America, v. 148, (2), p. 1063-1076. (2020). DOI: 10.1121/10.0001763.","meta":"Journal article · 2020","search_text":"a conceptual study of utilizing compressive-sensing-based fan noise mode detection for aeroengine prognostic and health management bu, huanxian; huang, xun; zhang, xin. “a conceptual study of utilizing compressive-sensing-based fan noise mode detection for aeroengine prognostic and health management.” journal of the acoustical society of america, v. 148, (2), p. 1063-1076. (2020). doi: 10.1121/10.0001763. journal article · 2020 bu, huanxian; huang, xun; zhang, xin 2020 10.1121/10.0001763 journal of the acoustical society of america 148 (2) 1063-1076","order":282,"static_url":"/publications/287/"},{"section":"Publications","title":"A compressive-sensing-based method for radial mode analysis of aeroengine fan noise","url":"/publications/286/","summary":"Bu, Huanxian; Huang, Xun; Zhang, Xin. “A compressive-sensing-based method for radial mode analysis of aeroengine fan noise.” Journal of Sound and Vibration, v. 464, article number 114930. (2020). DOI: 10.1016/j.jsv.2019.114930.","meta":"Journal article · 2020","search_text":"a compressive-sensing-based method for radial mode analysis of aeroengine fan noise bu, huanxian; huang, xun; zhang, xin. “a compressive-sensing-based method for radial mode analysis of aeroengine fan noise.” journal of sound and vibration, v. 464, article number 114930. (2020). doi: 10.1016/j.jsv.2019.114930. journal article · 2020 bu, huanxian; huang, xun; zhang, xin 2020 10.1016/j.jsv.2019.114930 journal of sound and vibration 464 article 114930","order":283,"static_url":"/publications/286/"},{"section":"Publications","title":"A compact low-frequency sound-absorbing metasurface constructed by resonator with embedded spiral neck","url":"/publications/285/","summary":"Guo, Jingwen; Zhang, Xin; Fang, Yi; Jiang, Ziyan. “A compact low-frequency sound-absorbing metasurface constructed by resonator with embedded spiral neck.” Applied Physics Letters, v. 117, (22), article number 221902. (2020). DOI: 10.1063/5.0031891.","meta":"Journal article · 2020","search_text":"a compact low-frequency sound-absorbing metasurface constructed by resonator with embedded spiral neck guo, jingwen; zhang, xin; fang, yi; jiang, ziyan. “a compact low-frequency sound-absorbing metasurface constructed by resonator with embedded spiral neck.” applied physics letters, v. 117, (22), article number 221902. (2020). doi: 10.1063/5.0031891. journal article · 2020 guo, jingwen; zhang, xin; fang, yi; jiang, ziyan 2020 10.1063/5.0031891 applied physics letters 117 (22) article 221902","order":284,"static_url":"/publications/285/"},{"section":"Publications","title":"The effect of uniform mean flow on sound pressure field of metasurface","url":"/publications/327/","summary":"Zhou, Jie; Dan, Sui; Fang, Yi; Zhang, Xin; Huang, Xun. “The effect of uniform mean flow on sound pressure field of metasurface.” 25th AIAA/CEAS Aeroacoustics Conference, 2019, American Institute of Aeronautics and Astronautics Inc, AIAA, 2019. (2019). DOI: 10.2514/6.2019-2704.","meta":"Conference paper · 2019","search_text":"the effect of uniform mean flow on sound pressure field of metasurface zhou, jie; dan, sui; fang, yi; zhang, xin; huang, xun. “the effect of uniform mean flow on sound pressure field of metasurface.” 25th aiaa/ceas aeroacoustics conference, 2019, american institute of aeronautics and astronautics inc, aiaa, 2019. (2019). doi: 10.2514/6.2019-2704. conference paper · 2019 zhou, jie; dan, sui; fang, yi; zhang, xin; huang, xun 2019 10.2514/6.2019-2704 25th aiaa/ceas aeroacoustics conference, 2019, american institute of aeronautics and astronautics inc, aiaa, 2019","order":285,"static_url":"/publications/327/"},{"section":"Publications","title":"Numerical and analytical investigations of the effect of the streamwise disturbance on the airfoil-anisotropic turbulence interaction noise","url":"/publications/326/","summary":"Zhong, Siyang; Zhang, Xin. “Numerical and analytical investigations of the effect of the streamwise disturbance on the airfoil-anisotropic turbulence interaction noise.” 25th AIAA/CEAS Aeroacoustics Conference, 2019, American Institute of Aeronautics and Astronautics Inc, AIAA, …","meta":"Conference paper · 2019","search_text":"numerical and analytical investigations of the effect of the streamwise disturbance on the airfoil-anisotropic turbulence interaction noise zhong, siyang; zhang, xin. “numerical and analytical investigations of the effect of the streamwise disturbance on the airfoil-anisotropic turbulence interaction noise.” 25th aiaa/ceas aeroacoustics conference, 2019, american institute of aeronautics and astronautics inc, aiaa, 2019. (2019). doi: 10.2514/6.2019-2478. conference paper · 2019 zhong, siyang; zhang, xin 2019 10.2514/6.2019-2478 25th aiaa/ceas aeroacoustics conference, 2019, american institute of aeronautics and astronautics inc, aiaa, 2019","order":286,"static_url":"/publications/326/"},{"section":"Publications","title":"Noise prediction of drones in urban environments","url":"/publications/325/","summary":"Bian, Haoyu; Fattah, Ryu; Sun, Yuhao; Zhang, Xin. “Noise prediction of drones in urban environments.” 25th AIAA/CEAS Aeroacoustics Conference, 2019, American Institute of Aeronautics and Astronautics Inc, AIAA, 2019. (2019). DOI: 10.2514/6.2019-2685.","meta":"Conference paper · 2019","search_text":"noise prediction of drones in urban environments bian, haoyu; fattah, ryu; sun, yuhao; zhang, xin. “noise prediction of drones in urban environments.” 25th aiaa/ceas aeroacoustics conference, 2019, american institute of aeronautics and astronautics inc, aiaa, 2019. (2019). doi: 10.2514/6.2019-2685. conference paper · 2019 bian, haoyu; fattah, ryu; sun, yuhao; zhang, xin 2019 10.2514/6.2019-2685 25th aiaa/ceas aeroacoustics conference, 2019, american institute of aeronautics and astronautics inc, aiaa, 2019","order":287,"static_url":"/publications/325/"},{"section":"Publications","title":"Noise measurements of generic small-scale propellers","url":"/publications/324/","summary":"Fattah, Ryu; Chen, Weijie; Wu, Han; Wu, Yan; Zhang, Xin. “Noise measurements of generic small-scale propellers.” 25th AIAA/CEAS Aeroacoustics Conference, 2019, American Institute of Aeronautics and Astronautics Inc, AIAA, 2019. (2019). DOI: 10.2514/6.2019-2498.","meta":"Conference paper · 2019","search_text":"noise measurements of generic small-scale propellers fattah, ryu; chen, weijie; wu, han; wu, yan; zhang, xin. “noise measurements of generic small-scale propellers.” 25th aiaa/ceas aeroacoustics conference, 2019, american institute of aeronautics and astronautics inc, aiaa, 2019. (2019). doi: 10.2514/6.2019-2498. conference paper · 2019 fattah, ryu; chen, weijie; wu, han; wu, yan; zhang, xin 2019 10.2514/6.2019-2498 25th aiaa/ceas aeroacoustics conference, 2019, american institute of aeronautics and astronautics inc, aiaa, 2019","order":288,"static_url":"/publications/324/"},{"section":"Publications","title":"Noise assessment of mulit-rotor flying vehicles","url":"/publications/323/","summary":"Fattah, Ryu; Zhang, Xin; Huang, Xun. “Noise assessment of mulit-rotor flying vehicles.” Proceedings of the 26th International Congress on Sound and Vibration, ICSV 2019, Canadian Acoustical Association, 2019. (2019).","meta":"Conference paper · 2019","search_text":"noise assessment of mulit-rotor flying vehicles fattah, ryu; zhang, xin; huang, xun. “noise assessment of mulit-rotor flying vehicles.” proceedings of the 26th international congress on sound and vibration, icsv 2019, canadian acoustical association, 2019. (2019). conference paper · 2019 fattah, ryu; zhang, xin; huang, xun 2019 proceedings of the 26th international congress on sound and vibration, icsv 2019, canadian acoustical association, 2019","order":289,"static_url":"/publications/323/"},{"section":"Publications","title":"Multi-rotor noise scattering by a drone fuselage","url":"/publications/322/","summary":"Jiang, Hanbo; Zhou, Teng; Fattah, Ryu J.; Zhang, Xin; Huang, Xun. “Multi-rotor noise scattering by a drone fuselage.” 25th AIAA/CEAS Aeroacoustics Conference, 2019, American Institute of Aeronautics and Astronautics Inc, AIAA, 2019. (2019). DOI: 10.2514/6.2019-2586.","meta":"Conference paper · 2019","search_text":"multi-rotor noise scattering by a drone fuselage jiang, hanbo; zhou, teng; fattah, ryu j.; zhang, xin; huang, xun. “multi-rotor noise scattering by a drone fuselage.” 25th aiaa/ceas aeroacoustics conference, 2019, american institute of aeronautics and astronautics inc, aiaa, 2019. (2019). doi: 10.2514/6.2019-2586. conference paper · 2019 jiang, hanbo; zhou, teng; fattah, ryu j.; zhang, xin; huang, xun 2019 10.2514/6.2019-2586 25th aiaa/ceas aeroacoustics conference, 2019, american institute of aeronautics and astronautics inc, aiaa, 2019","order":290,"static_url":"/publications/322/"},{"section":"Publications","title":"Modification of broadband trailing edge noise through hairy coating","url":"/publications/321/","summary":"Zhou, Peng; Zhong, Siyang; Zhang, Xin. “Modification of broadband trailing edge noise through hairy coating.” Proceedings of the 26th International Congress on Sound and Vibration, ICSV 2019, Canadian Acoustical Association, 2019. (2019).","meta":"Conference paper · 2019","search_text":"modification of broadband trailing edge noise through hairy coating zhou, peng; zhong, siyang; zhang, xin. “modification of broadband trailing edge noise through hairy coating.” proceedings of the 26th international congress on sound and vibration, icsv 2019, canadian acoustical association, 2019. (2019). conference paper · 2019 zhou, peng; zhong, siyang; zhang, xin 2019 proceedings of the 26th international congress on sound and vibration, icsv 2019, canadian acoustical association, 2019","order":291,"static_url":"/publications/321/"},{"section":"Publications","title":"Measurement of trailing edge noise from a heaving airfoil","url":"/publications/320/","summary":"Zhou, Teng; Sun, Yuhao; Zhang, Xin; Chen, Wangqiao; Huang, Xun. “Measurement of trailing edge noise from a heaving airfoil.” Proceedings of the 26th International Congress on Sound and Vibration, ICSV 2019, Canadian Acoustical Association, 2019. (2019).","meta":"Conference paper · 2019","search_text":"measurement of trailing edge noise from a heaving airfoil zhou, teng; sun, yuhao; zhang, xin; chen, wangqiao; huang, xun. “measurement of trailing edge noise from a heaving airfoil.” proceedings of the 26th international congress on sound and vibration, icsv 2019, canadian acoustical association, 2019. (2019). conference paper · 2019 zhou, teng; sun, yuhao; zhang, xin; chen, wangqiao; huang, xun 2019 proceedings of the 26th international congress on sound and vibration, icsv 2019, canadian acoustical association, 2019","order":292,"static_url":"/publications/320/"},{"section":"Publications","title":"Low-frequency sound absorber based on checkerboard Helmholtz resonators with different extended necks","url":"/publications/319/","summary":"Guo, Jingwen; Zhang, Xin. “Low-frequency sound absorber based on checkerboard Helmholtz resonators with different extended necks.” INTER-NOISE 2019 MADRID - 48th International Congress and Exhibition on Noise Control Engineering / edited by Calvo-Manzano Antonio; Delgado Ana; Pe…","meta":"Conference paper · 2019","search_text":"low-frequency sound absorber based on checkerboard helmholtz resonators with different extended necks guo, jingwen; zhang, xin. “low-frequency sound absorber based on checkerboard helmholtz resonators with different extended necks.” inter-noise 2019 madrid - 48th international congress and exhibition on noise control engineering / edited by calvo-manzano antonio; delgado ana; perez-lopez antonio; santiago jose salvador. sociedad espanola de acustica - spanish acoustical society, sea, 2019. (2019). conference paper · 2019 guo, jingwen; zhang, xin 2019 inter-noise 2019 madrid - 48th international congress and exhibition on noise control engineering / edited by calvo-manzano antonio; delgado ana; perez-lopez antonio; santiago jose salvador. sociedad espanola de acustica - spanish acoustical society, sea, 2019","order":293,"static_url":"/publications/319/"},{"section":"Publications","title":"Inverted wedge porous acoustic metamaterials","url":"/publications/318/","summary":"Ji, Guosheng; Zhang, Xin; Fang, Yi; Zhou, Jie. “Inverted wedge porous acoustic metamaterials.” 25th AIAA/CEAS Aeroacoustics Conference, 2019, American Institute of Aeronautics and Astronautics Inc, AIAA, 2019. (2019). DOI: 10.2514/6.2019-2706.","meta":"Conference paper · 2019","search_text":"inverted wedge porous acoustic metamaterials ji, guosheng; zhang, xin; fang, yi; zhou, jie. “inverted wedge porous acoustic metamaterials.” 25th aiaa/ceas aeroacoustics conference, 2019, american institute of aeronautics and astronautics inc, aiaa, 2019. (2019). doi: 10.2514/6.2019-2706. conference paper · 2019 ji, guosheng; zhang, xin; fang, yi; zhou, jie 2019 10.2514/6.2019-2706 25th aiaa/ceas aeroacoustics conference, 2019, american institute of aeronautics and astronautics inc, aiaa, 2019","order":294,"static_url":"/publications/318/"},{"section":"Publications","title":"High-resolution acoustical imaging for rotating acoustic source based on compressive sensing beamforming","url":"/publications/317/","summary":"Huanxian, Bu; Xun, Huang; Xin, Zhang. “High-resolution acoustical imaging for rotating acoustic source based on compressive sensing beamforming.” 25th AIAA/CEAS Aeroacoustics Conference, 2019, American Institute of Aeronautics and Astronautics Inc, AIAA, 2019. (2019). DOI: 10.25…","meta":"Conference paper · 2019","search_text":"high-resolution acoustical imaging for rotating acoustic source based on compressive sensing beamforming huanxian, bu; xun, huang; xin, zhang. “high-resolution acoustical imaging for rotating acoustic source based on compressive sensing beamforming.” 25th aiaa/ceas aeroacoustics conference, 2019, american institute of aeronautics and astronautics inc, aiaa, 2019. (2019). doi: 10.2514/6.2019-2410. conference paper · 2019 huanxian, bu; xun, huang; xin, zhang 2019 10.2514/6.2019-2410 25th aiaa/ceas aeroacoustics conference, 2019, american institute of aeronautics and astronautics inc, aiaa, 2019","order":295,"static_url":"/publications/317/"},{"section":"Publications","title":"Distortion of anisotropic turbulence spectrum in the vicinity of aerofoil leading edge","url":"/publications/316/","summary":"Shen, Zhen; Zhang, Xin. “Distortion of anisotropic turbulence spectrum in the vicinity of aerofoil leading edge.” INTER-NOISE 2019 MADRID - 48th International Congress and Exhibition on Noise Control Engineering / edited by Calvo-Manzano Antonio; Delgado Ana; Perez-Lopez Antonio…","meta":"Conference paper · 2019","search_text":"distortion of anisotropic turbulence spectrum in the vicinity of aerofoil leading edge shen, zhen; zhang, xin. “distortion of anisotropic turbulence spectrum in the vicinity of aerofoil leading edge.” inter-noise 2019 madrid - 48th international congress and exhibition on noise control engineering / edited by calvo-manzano antonio; delgado ana; perez-lopez antonio; santiago jose salvador. sociedad espanola de acustica - spanish acoustical society, sea, 2019, (2019). conference paper · 2019 shen, zhen; zhang, xin 2019 inter-noise 2019 madrid - 48th international congress and exhibition on noise control engineering / edited by calvo-manzano antonio; delgado ana; perez-lopez antonio; santiago jose salvador. sociedad espanola de acustica - spanish acoustical society, sea, 2019,","order":296,"static_url":"/publications/316/"},{"section":"Publications","title":"Design and commission of a low speed anechoic wind tunnel at HKUST","url":"/publications/315/","summary":"Zhang, Xin; Fattah, Ryu; Wei, Yi; Huang, Xun. “Design and commission of a low speed anechoic wind tunnel at HKUST.” Proceedings of the 26th International Congress on Sound and Vibration, ICSV 2019, Canadian Acoustical Association, 2019. (2019).","meta":"Conference paper · 2019","search_text":"design and commission of a low speed anechoic wind tunnel at hkust zhang, xin; fattah, ryu; wei, yi; huang, xun. “design and commission of a low speed anechoic wind tunnel at hkust.” proceedings of the 26th international congress on sound and vibration, icsv 2019, canadian acoustical association, 2019. (2019). conference paper · 2019 zhang, xin; fattah, ryu; wei, yi; huang, xun 2019 proceedings of the 26th international congress on sound and vibration, icsv 2019, canadian acoustical association, 2019","order":297,"static_url":"/publications/315/"},{"section":"Publications","title":"Broadband forbidden transmission by multiple CPA-based detuned Helmholtz resonators","url":"/publications/314/","summary":"Guo, Jingwen; Zhang, Xin; Fang, Yi. “Broadband forbidden transmission by multiple CPA-based detuned Helmholtz resonators.” Proceedings of the 26th International Congress on Sound and Vibration, ICSV 2019, Canadian Acoustical Association, 2019. (2019).","meta":"Conference paper · 2019","search_text":"broadband forbidden transmission by multiple cpa-based detuned helmholtz resonators guo, jingwen; zhang, xin; fang, yi. “broadband forbidden transmission by multiple cpa-based detuned helmholtz resonators.” proceedings of the 26th international congress on sound and vibration, icsv 2019, canadian acoustical association, 2019. (2019). conference paper · 2019 guo, jingwen; zhang, xin; fang, yi 2019 proceedings of the 26th international congress on sound and vibration, icsv 2019, canadian acoustical association, 2019","order":298,"static_url":"/publications/314/"},{"section":"Publications","title":"An experimental investigation of the effect of owl-inspired velvety coating on trailing edge noise","url":"/publications/313/","summary":"Zhou, Peng; Lui, Go Nam; Zhang, Xin. “An experimental investigation of the effect of owl-inspired velvety coating on trailing edge noise.” 25th AIAA/CEAS Aeroacoustics Conference, 2019, American Institute of Aeronautics and Astronautics Inc, AIAA, 2019. (2019). DOI: 10.2514/6.20…","meta":"Conference paper · 2019","search_text":"an experimental investigation of the effect of owl-inspired velvety coating on trailing edge noise zhou, peng; lui, go nam; zhang, xin. “an experimental investigation of the effect of owl-inspired velvety coating on trailing edge noise.” 25th aiaa/ceas aeroacoustics conference, 2019, american institute of aeronautics and astronautics inc, aiaa, 2019. (2019). doi: 10.2514/6.2019-2622. conference paper · 2019 zhou, peng; lui, go nam; zhang, xin 2019 10.2514/6.2019-2622 25th aiaa/ceas aeroacoustics conference, 2019, american institute of aeronautics and astronautics inc, aiaa, 2019","order":299,"static_url":"/publications/313/"},{"section":"Publications","title":"An analytical model for the prediction of airfoil cascade-turbulence interaction noise","url":"/publications/312/","summary":"Zhong, Siyang; Jiang, Hanbo; Ying, Wei; Zhang, Xin. “An analytical model for the prediction of airfoil cascade-turbulence interaction noise.” 25th AIAA/CEAS Aeroacoustics Conference, 2019, American Institute of Aeronautics and Astronautics Inc, AIAA, 2019. (2019). DOI: 10.2514/6…","meta":"Conference paper · 2019","search_text":"an analytical model for the prediction of airfoil cascade-turbulence interaction noise zhong, siyang; jiang, hanbo; ying, wei; zhang, xin. “an analytical model for the prediction of airfoil cascade-turbulence interaction noise.” 25th aiaa/ceas aeroacoustics conference, 2019, american institute of aeronautics and astronautics inc, aiaa, 2019. (2019). doi: 10.2514/6.2019-2479. conference paper · 2019 zhong, siyang; jiang, hanbo; ying, wei; zhang, xin 2019 10.2514/6.2019-2479 25th aiaa/ceas aeroacoustics conference, 2019, american institute of aeronautics and astronautics inc, aiaa, 2019","order":300,"static_url":"/publications/312/"},{"section":"Publications","title":"Acoustic mapping of drones in complex environments","url":"/publications/311/","summary":"Zhang, Xin; Bian, Haoyu; Fattah, Ryu; Sun, Yuhao. “Acoustic mapping of drones in complex environments.” Proceedings of the 26th International Congress on Sound and Vibration, ICSV 2019, Canadian Acoustical Association, 2019. (2019).","meta":"Conference paper · 2019","search_text":"acoustic mapping of drones in complex environments zhang, xin; bian, haoyu; fattah, ryu; sun, yuhao. “acoustic mapping of drones in complex environments.” proceedings of the 26th international congress on sound and vibration, icsv 2019, canadian acoustical association, 2019. (2019). conference paper · 2019 zhang, xin; bian, haoyu; fattah, ryu; sun, yuhao 2019 proceedings of the 26th international congress on sound and vibration, icsv 2019, canadian acoustical association, 2019","order":301,"static_url":"/publications/311/"},{"section":"Publications","title":"Acoustic characteristics of a quad-copter under realistic flight conditions","url":"/publications/310/","summary":"Zhou, Teng; Jiang, Hanbo; Sun, Yuhao; Fattah, Ryu J.; Zhang, Xin; Huang, Ben; Cheng, Lei. “Acoustic characteristics of a quad-copter under realistic flight conditions.” 25th AIAA/CEAS Aeroacoustics Conference, 2019, American Institute of Aeronautics and Astronautics Inc, AIAA, 2…","meta":"Conference paper · 2019","search_text":"acoustic characteristics of a quad-copter under realistic flight conditions zhou, teng; jiang, hanbo; sun, yuhao; fattah, ryu j.; zhang, xin; huang, ben; cheng, lei. “acoustic characteristics of a quad-copter under realistic flight conditions.” 25th aiaa/ceas aeroacoustics conference, 2019, american institute of aeronautics and astronautics inc, aiaa, 2019. (2019). doi: 10.2514/6.2019-2587. conference paper · 2019 zhou, teng; jiang, hanbo; sun, yuhao; fattah, ryu j.; zhang, xin; huang, ben; cheng, lei 2019 10.2514/6.2019-2587 25th aiaa/ceas aeroacoustics conference, 2019, american institute of aeronautics and astronautics inc, aiaa, 2019","order":302,"static_url":"/publications/310/"},{"section":"Publications","title":"On the effects of fan wake modelling and vane design on cascade noise","url":"/publications/309/","summary":"Gea-Aguilera, Fernando; Gill, J.; Zhang, Xin. “On the effects of fan wake modelling and vane design on cascade noise.” Journal of Sound and Vibration, v. 459, article number 114859 (2019). DOI: 10.1016/j.jsv.2019.114859.","meta":"Journal article · 2019","search_text":"on the effects of fan wake modelling and vane design on cascade noise gea-aguilera, fernando; gill, j.; zhang, xin. “on the effects of fan wake modelling and vane design on cascade noise.” journal of sound and vibration, v. 459, article number 114859 (2019). doi: 10.1016/j.jsv.2019.114859. journal article · 2019 gea-aguilera, fernando; gill, j.; zhang, xin 2019 10.1016/j.jsv.2019.114859 journal of sound and vibration, v. 459, article number 114859","order":303,"static_url":"/publications/309/"},{"section":"Publications","title":"Geometry effect on the airfoil-gust interaction noise in transonic flows","url":"/publications/308/","summary":"Zhong, Siyang; Zhang, Xin; Gill, James; Fattah, Ryu; Sun, Yuhao. “Geometry effect on the airfoil-gust interaction noise in transonic flows.” Aerospace Science and Technology, v. 92, p. 181-191. (2019). DOI: 10.1016/j.ast.2019.06.006.","meta":"Journal article · 2019","search_text":"geometry effect on the airfoil-gust interaction noise in transonic flows zhong, siyang; zhang, xin; gill, james; fattah, ryu; sun, yuhao. “geometry effect on the airfoil-gust interaction noise in transonic flows.” aerospace science and technology, v. 92, p. 181-191. (2019). doi: 10.1016/j.ast.2019.06.006. journal article · 2019 zhong, siyang; zhang, xin; gill, james; fattah, ryu; sun, yuhao 2019 10.1016/j.ast.2019.06.006 aerospace science and technology 92 181-191","order":304,"static_url":"/publications/308/"},{"section":"Publications","title":"Direct anisotropic filter method of generating synthetic turbulence applied to turbulence-airfoil interaction noise prediction","url":"/publications/307/","summary":"Shen, Zhen; Zhang, Xin. “Direct anisotropic filter method of generating synthetic turbulence applied to turbulence-airfoil interaction noise prediction.” Journal of Sound and Vibration, v. 458, p. 544-564 (2019). DOI: 10.1016/j.jsv.2019.07.003.","meta":"Journal article · 2019","search_text":"direct anisotropic filter method of generating synthetic turbulence applied to turbulence-airfoil interaction noise prediction shen, zhen; zhang, xin. “direct anisotropic filter method of generating synthetic turbulence applied to turbulence-airfoil interaction noise prediction.” journal of sound and vibration, v. 458, p. 544-564 (2019). doi: 10.1016/j.jsv.2019.07.003. journal article · 2019 shen, zhen; zhang, xin 2019 10.1016/j.jsv.2019.07.003 journal of sound and vibration, v. 458, p. 544-564","order":305,"static_url":"/publications/307/"},{"section":"Publications","title":"Compressive sensing method with enhanced sparsity for aeroengine duct mode detection","url":"/publications/306/","summary":"Bu, Huanxian; Huang, Xun; Zhang, Xin. “Compressive sensing method with enhanced sparsity for aeroengine duct mode detection.” Journal of the Acoustical Society of America, v. 146, (1), p. EL39-EL44. (2019). DOI: 10.1121/1.5116893.","meta":"Journal article · 2019","search_text":"compressive sensing method with enhanced sparsity for aeroengine duct mode detection bu, huanxian; huang, xun; zhang, xin. “compressive sensing method with enhanced sparsity for aeroengine duct mode detection.” journal of the acoustical society of america, v. 146, (1), p. el39-el44. (2019). doi: 10.1121/1.5116893. journal article · 2019 bu, huanxian; huang, xun; zhang, xin 2019 10.1121/1.5116893 journal of the acoustical society of america 146 (1) el39-el44","order":306,"static_url":"/publications/306/"},{"section":"Publications","title":"An experimental study of trailing edge noise from a pitching airfoil","url":"/publications/305/","summary":"Zhou, Teng; Sun, Yuaho; Fattah, Ryu; Zhang, Xin; Huang, Xun. “An experimental study of trailing edge noise from a pitching airfoil.” Journal of the Acoustical Society of America, v. 145, (4), p. 2009-2021. (2019). DOI: 10.1121/1.5094898.","meta":"Journal article · 2019","search_text":"an experimental study of trailing edge noise from a pitching airfoil zhou, teng; sun, yuaho; fattah, ryu; zhang, xin; huang, xun. “an experimental study of trailing edge noise from a pitching airfoil.” journal of the acoustical society of america, v. 145, (4), p. 2009-2021. (2019). doi: 10.1121/1.5094898. journal article · 2019 zhou, teng; sun, yuaho; fattah, ryu; zhang, xin; huang, xun 2019 10.1121/1.5094898 journal of the acoustical society of america 145 (4) 2009-2021","order":307,"static_url":"/publications/305/"},{"section":"Publications","title":"Acoustic metaporous layer with composite structures for perfect and quasi-omnidirectional sound absorption","url":"/publications/304/","summary":"Fang, Yi; Zhang, Xin; Zhou, Jie; Guo, Jingwen; Huang, Xun. “Acoustic metaporous layer with composite structures for perfect and quasi-omnidirectional sound absorption.” Composite Structures, v. 223, article number 110948. (2019). DOI: 10.1016/j.compstruct.2019.110948.","meta":"Journal article · 2019","search_text":"acoustic metaporous layer with composite structures for perfect and quasi-omnidirectional sound absorption fang, yi; zhang, xin; zhou, jie; guo, jingwen; huang, xun. “acoustic metaporous layer with composite structures for perfect and quasi-omnidirectional sound absorption.” composite structures, v. 223, article number 110948. (2019). doi: 10.1016/j.compstruct.2019.110948. journal article · 2019 fang, yi; zhang, xin; zhou, jie; guo, jingwen; huang, xun 2019 10.1016/j.compstruct.2019.110948 composite structures 223 article 110948","order":308,"static_url":"/publications/304/"},{"section":"Publications","title":"A comparison of acoustic far-field prediction methods for turbulent flows","url":"/publications/303/","summary":"Zhong, Siyang; Zhang, Xin; Huang, Xun. “A comparison of acoustic far-field prediction methods for turbulent flows.” International Journal of Aeroacoustics, v. 18, (6-7), p. 579-595. (2019). DOI: 10.1177/1475472x19871525.","meta":"Journal article · 2019","search_text":"a comparison of acoustic far-field prediction methods for turbulent flows zhong, siyang; zhang, xin; huang, xun. “a comparison of acoustic far-field prediction methods for turbulent flows.” international journal of aeroacoustics, v. 18, (6-7), p. 579-595. (2019). doi: 10.1177/1475472x19871525. journal article · 2019 zhong, siyang; zhang, xin; huang, xun 2019 10.1177/1475472x19871525 international journal of aeroacoustics 18 (6-7) 579-595","order":309,"static_url":"/publications/303/"},{"section":"Publications","title":"Reduced-basis boundary element method for efficient broadband acoustic simulation","url":"/publications/141/","summary":"Jiang, Hanbo; Zhang, Xin; Huang, Xun. “Reduced-basis boundary element method for efficient broadband acoustic simulation.” Journal of Sound and Vibration, v. 456, p. 374-385. (2019). DOI: 10.1016/j.jsv.2019.05.017.","meta":"Journal article · 2019","search_text":"reduced-basis boundary element method for efficient broadband acoustic simulation jiang, hanbo; zhang, xin; huang, xun. “reduced-basis boundary element method for efficient broadband acoustic simulation.” journal of sound and vibration, v. 456, p. 374-385. (2019). doi: 10.1016/j.jsv.2019.05.017. journal article · 2019 jiang, hanbo; zhang, xin; huang, xun 2019 10.1016/j.jsv.2019.05.017 journal of sound and vibration 456 374-385","order":310,"static_url":"/publications/141/"},{"section":"Publications","title":"Tonal Fan-Noise Radiation From Aero-Engine Bypass With Serrated End Treatments","url":"/publications/140/","summary":"Jiang H, Huang X. Tonal Fan-Noise Radiation From Aero-Engine Bypass With Serrated End Treatments. Journal of Turbomachinery. 2019 Oct 1;141(10).","meta":"Journal article · 2019","search_text":"tonal fan-noise radiation from aero-engine bypass with serrated end treatments jiang h, huang x. tonal fan-noise radiation from aero-engine bypass with serrated end treatments. journal of turbomachinery. 2019 oct 1;141(10). journal article · 2019 hanbo jiang; xun huang 2019 10.1115/1.4043882 journal of turbomachinery 141 (10)","order":311,"static_url":"/publications/140/"},{"section":"Publications","title":"An efficient computation of cascade-gust interaction noise based on a hybrid analytical and boundary element method","url":"/publications/137/","summary":"Zhong, Siyang; Jiang, Hanbo; Ying, Wei; Zhang, Xin; Huang, Xun. “An efficient computation of cascade-gust interaction noise based on a hybrid analytical and boundary element method.” Journal of Sound and Vibration, v. 461, article number 114911. (2019). DOI: 10.1016/j.jsv.2019.1…","meta":"Journal article · 2019","search_text":"an efficient computation of cascade-gust interaction noise based on a hybrid analytical and boundary element method zhong, siyang; jiang, hanbo; ying, wei; zhang, xin; huang, xun. “an efficient computation of cascade-gust interaction noise based on a hybrid analytical and boundary element method.” journal of sound and vibration, v. 461, article number 114911. (2019). doi: 10.1016/j.jsv.2019.114911. journal article · 2019 zhong, siyang; jiang, hanbo; ying, wei; zhang, xin; huang, xun 2019 10.1016/j.jsv.2019.114911 journal of sound and vibration 461 article 114911","order":312,"static_url":"/publications/137/"},{"section":"Publications","title":"On the effect of streamwise disturbance on the airfoil-turbulence interaction noise","url":"/publications/136/","summary":"Zhong, Siyang; Zhang, Xin. “On the effect of streamwise disturbance on the airfoil-turbulence interaction noise.” Journal of the Acoustical Society of America, v. 145, (4), p. 2530-2539. (2019). DOI: 10.1121/1.5098783.","meta":"Journal article · 2019","search_text":"on the effect of streamwise disturbance on the airfoil-turbulence interaction noise zhong, siyang; zhang, xin. “on the effect of streamwise disturbance on the airfoil-turbulence interaction noise.” journal of the acoustical society of america, v. 145, (4), p. 2530-2539. (2019). doi: 10.1121/1.5098783. journal article · 2019 zhong, siyang; zhang, xin 2019 10.1121/1.5098783 journal of the acoustical society of america 145 (4) 2530-2539","order":313,"static_url":"/publications/136/"},{"section":"Publications","title":"Turbulent-wake-cascade interaction noise simulations using a hybrid sliding mesh method","url":"/publications/338/","summary":"Ying, Wei; Fattah, Ryu; Zhang, Xin; Gea-Aguilera, Fernando. “Turbulent-wake-cascade interaction noise simulations using a hybrid sliding mesh method.” 25th International Congress on Sound and Vibration 2018, ICSV 2018, International Institute of Acoustics and Vibration, IIAV, 20…","meta":"Conference paper · 2018","search_text":"turbulent-wake-cascade interaction noise simulations using a hybrid sliding mesh method ying, wei; fattah, ryu; zhang, xin; gea-aguilera, fernando. “turbulent-wake-cascade interaction noise simulations using a hybrid sliding mesh method.” 25th international congress on sound and vibration 2018, icsv 2018, international institute of acoustics and vibration, iiav, 2018, p. 1358-1365. (2018). conference paper · 2018 ying, wei; fattah, ryu; zhang, xin; gea-aguilera, fernando 2018 25th international congress on sound and vibration 2018, icsv 2018, international institute of acoustics and vibration, iiav, 2018, p. 1358-1365 1358-1365","order":314,"static_url":"/publications/338/"},{"section":"Publications","title":"Sound extrapolation methods for turbulent flows based on indirect acoustic variables","url":"/publications/337/","summary":"Zhong, Siyang; Zhang, Xin; Morfey, Christopher L.; Sandberg, Richard; Fattah, Ryu. “Sound extrapolation methods for turbulent flows based on indirect acoustic variables.” 2018 AIAA/CEAS Aeroacoustics Conference, American Institute of Aeronautics and Astronautics Inc, AIAA, 2018,…","meta":"Conference paper · 2018","search_text":"sound extrapolation methods for turbulent flows based on indirect acoustic variables zhong, siyang; zhang, xin; morfey, christopher l.; sandberg, richard; fattah, ryu. “sound extrapolation methods for turbulent flows based on indirect acoustic variables.” 2018 aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc, aiaa, 2018, article number aiaa 2018-2804. (2018). doi: 10.2514/6.2018-2804. conference paper · 2018 zhong, siyang; zhang, xin; morfey, christopher l.; sandberg, richard; fattah, ryu 2018 10.2514/6.2018-2804 2018 aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc, aiaa, 2018, article number aiaa 2018-2804 article aiaa 2018-2804","order":315,"static_url":"/publications/337/"},{"section":"Publications","title":"Reflected wave manipulation by varying-depth acoustic liners","url":"/publications/336/","summary":"Guo, Jingwen; Zhang, Xin; Fang, Yi; Fattah, Ryu; Miao, Shuming; Zhou, Guocheng; Chen, Bao. “Reflected wave manipulation by varying-depth acoustic liners.” 2018 AIAA/CEAS Aeroacoustics Conference, American Institute of Aeronautics and Astronautics Inc, AIAA, 2018, article number …","meta":"Conference paper · 2018","search_text":"reflected wave manipulation by varying-depth acoustic liners guo, jingwen; zhang, xin; fang, yi; fattah, ryu; miao, shuming; zhou, guocheng; chen, bao. “reflected wave manipulation by varying-depth acoustic liners.” 2018 aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc, aiaa, 2018, article number aiaa 2018-4103. (2018). doi: 10.2514/6.2018-40103. conference paper · 2018 guo, jingwen; zhang, xin; fang, yi; fattah, ryu; miao, shuming; zhou, guocheng; chen, bao 2018 10.2514/6.2018-40103 2018 aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc, aiaa, 2018, article number aiaa 2018-4103 article aiaa 2018-4103","order":316,"static_url":"/publications/336/"},{"section":"Publications","title":"Random-eddy-superposition technique for leading edge noise predictions","url":"/publications/335/","summary":"Shen, Zhen; Zhangy, Xin. “Random-eddy-superposition technique for leading edge noise predictions.” 2018 AIAA/CEAS Aeroacoustics Conference, American Institute of Aeronautics and Astronautics Inc, AIAA, 2018, article number AIAA 2018-3597 (2018). DOI: 10.2514/6.2018-3597.","meta":"Conference paper · 2018","search_text":"random-eddy-superposition technique for leading edge noise predictions shen, zhen; zhangy, xin. “random-eddy-superposition technique for leading edge noise predictions.” 2018 aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc, aiaa, 2018, article number aiaa 2018-3597 (2018). doi: 10.2514/6.2018-3597. conference paper · 2018 shen, zhen; zhangy, xin 2018 10.2514/6.2018-3597 2018 aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc, aiaa, 2018, article number aiaa 2018-3597","order":317,"static_url":"/publications/335/"},{"section":"Publications","title":"Modified non-Gaussian filters for synthetic turbulence","url":"/publications/334/","summary":"Shen, Zhen; Zhang, Xin. “Modified non-Gaussian filters for synthetic turbulence.” 25th International Congress on Sound and Vibration 2018, ICSV 2018, International Institute of Acoustics and Vibration, IIAV, 2018, p. 1462-1469 (2018).","meta":"Conference paper · 2018","search_text":"modified non-gaussian filters for synthetic turbulence shen, zhen; zhang, xin. “modified non-gaussian filters for synthetic turbulence.” 25th international congress on sound and vibration 2018, icsv 2018, international institute of acoustics and vibration, iiav, 2018, p. 1462-1469 (2018). conference paper · 2018 shen, zhen; zhang, xin 2018 25th international congress on sound and vibration 2018, icsv 2018, international institute of acoustics and vibration, iiav, 2018, p. 1462-1469","order":318,"static_url":"/publications/334/"},{"section":"Publications","title":"Leading edge noise simulations of a heaving airfoil","url":"/publications/333/","summary":"Sun, Yuhao; Fattah, Ryu; Zhou, Teng; Zhang, Xin. “Leading edge noise simulations of a heaving airfoil.” 25th International Congress on Sound and Vibration 2018, ICSV 2018, International Institute of Acoustics and Vibration, IIAV, 2018, p. 1307-1314. (2018).","meta":"Conference paper · 2018","search_text":"leading edge noise simulations of a heaving airfoil sun, yuhao; fattah, ryu; zhou, teng; zhang, xin. “leading edge noise simulations of a heaving airfoil.” 25th international congress on sound and vibration 2018, icsv 2018, international institute of acoustics and vibration, iiav, 2018, p. 1307-1314. (2018). conference paper · 2018 sun, yuhao; fattah, ryu; zhou, teng; zhang, xin 2018 25th international congress on sound and vibration 2018, icsv 2018, international institute of acoustics and vibration, iiav, 2018, p. 1307-1314 1307-1314","order":319,"static_url":"/publications/333/"},{"section":"Publications","title":"An experimental investigation of trailing edge noise of a pitching airfoil","url":"/publications/332/","summary":"Zhou, Teng; Sun, Yuhao; Fattah, Ryu; Zhang, Xin. “An experimental investigation of trailing edge noise of a pitching airfoil.” 25th International Congress on Sound and Vibration 2018, ICSV 2018, International Institute of Acoustics and Vibration, IIAV, 2018, p. 1446-1453. (2018).","meta":"Conference paper · 2018","search_text":"an experimental investigation of trailing edge noise of a pitching airfoil zhou, teng; sun, yuhao; fattah, ryu; zhang, xin. “an experimental investigation of trailing edge noise of a pitching airfoil.” 25th international congress on sound and vibration 2018, icsv 2018, international institute of acoustics and vibration, iiav, 2018, p. 1446-1453. (2018). conference paper · 2018 zhou, teng; sun, yuhao; fattah, ryu; zhang, xin 2018 25th international congress on sound and vibration 2018, icsv 2018, international institute of acoustics and vibration, iiav, 2018, p. 1446-1453 1446-1453","order":320,"static_url":"/publications/332/"},{"section":"Publications","title":"Acoustic metaporous layer for sound absorption enhancement","url":"/publications/331/","summary":"Fang, Yi; Zhang, Xin; Zhou, Jie; Zhou, Guocheng; Chen, Bao. “Acoustic metaporous layer for sound absorption enhancement.” 25th International Congress on Sound and Vibration 2018, ICSV 2018, International Institute of Acoustics and Vibration, IIAV, 2018, p. 3330-3337. (2018).","meta":"Conference paper · 2018","search_text":"acoustic metaporous layer for sound absorption enhancement fang, yi; zhang, xin; zhou, jie; zhou, guocheng; chen, bao. “acoustic metaporous layer for sound absorption enhancement.” 25th international congress on sound and vibration 2018, icsv 2018, international institute of acoustics and vibration, iiav, 2018, p. 3330-3337. (2018). conference paper · 2018 fang, yi; zhang, xin; zhou, jie; zhou, guocheng; chen, bao 2018 25th international congress on sound and vibration 2018, icsv 2018, international institute of acoustics and vibration, iiav, 2018, p. 3330-3337 3330-3337","order":321,"static_url":"/publications/331/"},{"section":"Publications","title":"Acoustic metamaterials applied on circular interfaces","url":"/publications/330/","summary":"Ji, Guosheng; Zhang, Xin; Fang, Yi; Zhou, Guocheng; Chen, Bao. “Acoustic metamaterials applied on circular interfaces.” 25th International Congress on Sound and Vibration 2018, ICSV 2018, International Institute of Acoustics and Vibration, IIAV, 2018, p. 3379-3386. (2018).","meta":"Conference paper · 2018","search_text":"acoustic metamaterials applied on circular interfaces ji, guosheng; zhang, xin; fang, yi; zhou, guocheng; chen, bao. “acoustic metamaterials applied on circular interfaces.” 25th international congress on sound and vibration 2018, icsv 2018, international institute of acoustics and vibration, iiav, 2018, p. 3379-3386. (2018). conference paper · 2018 ji, guosheng; zhang, xin; fang, yi; zhou, guocheng; chen, bao 2018 25th international congress on sound and vibration 2018, icsv 2018, international institute of acoustics and vibration, iiav, 2018, p. 3379-3386 3379-3386","order":322,"static_url":"/publications/330/"},{"section":"Publications","title":"Acoustic characterization of a porous metasurface with embedded partitions","url":"/publications/329/","summary":"Fang, Yi; Zhang, Xin; Zhou, Jie; Guo, Jingwen; Fattah, Ryu; Zhou, Guocheng; Chen, Bao. “Acoustic characterization of a porous metasurface with embedded partitions.” 2018 AIAA/CEAS Aeroacoustics Conference, American Institute of Aeronautics and Astronautics Inc, AIAA, 2018, artic…","meta":"Conference paper · 2018","search_text":"acoustic characterization of a porous metasurface with embedded partitions fang, yi; zhang, xin; zhou, jie; guo, jingwen; fattah, ryu; zhou, guocheng; chen, bao. “acoustic characterization of a porous metasurface with embedded partitions.” 2018 aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc, aiaa, 2018, article number aiaa 2018-3277. (2018). doi: 10.2514/6.2018-3277. conference paper · 2018 fang, yi; zhang, xin; zhou, jie; guo, jingwen; fattah, ryu; zhou, guocheng; chen, bao 2018 10.2514/6.2018-3277 2018 aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc, aiaa, 2018, article number aiaa 2018-3277 article aiaa 2018-3277","order":323,"static_url":"/publications/329/"},{"section":"Publications","title":"On the frequency domain formulation of the generalized sound extrapolation method","url":"/publications/328/","summary":"Zhong, Siyang; Zhang, Xin. “On the frequency domain formulation of the generalized sound extrapolation method.” Journal of the Acoustical Society of America, v. 144, (1), p. 24-31. (2018). DOI: 10.1121/1.5044515.","meta":"Journal article · 2018","search_text":"on the frequency domain formulation of the generalized sound extrapolation method zhong, siyang; zhang, xin. “on the frequency domain formulation of the generalized sound extrapolation method.” journal of the acoustical society of america, v. 144, (1), p. 24-31. (2018). doi: 10.1121/1.5044515. journal article · 2018 zhong, siyang; zhang, xin 2018 10.1121/1.5044515 journal of the acoustical society of america 144 (1) 24-31","order":324,"static_url":"/publications/328/"},{"section":"Publications","title":"A numerical investigation of the airfoil-gust interaction noise in transonic flows: Acoustic processes","url":"/publications/135/","summary":"Zhong, Siyang; Zhang, Xin; Gill, James; Fattah, Ryu; Sun, Yuhao. “A numerical investigation of the airfoil-gust interaction noise in transonic flows: Acoustic processes.” Journal of Sound and Vibration, v. 425, p. 239-256. (2018). DOI: 10.1016/j.jsv.2018.04.010.","meta":"Journal article · 2018","search_text":"a numerical investigation of the airfoil-gust interaction noise in transonic flows: acoustic processes zhong, siyang; zhang, xin; gill, james; fattah, ryu; sun, yuhao. “a numerical investigation of the airfoil-gust interaction noise in transonic flows: acoustic processes.” journal of sound and vibration, v. 425, p. 239-256. (2018). doi: 10.1016/j.jsv.2018.04.010. journal article · 2018 zhong, siyang; zhang, xin; gill, james; fattah, ryu; sun, yuhao 2018 10.1016/j.jsv.2018.04.010 journal of sound and vibration 425 239-256","order":325,"static_url":"/publications/135/"},{"section":"Publications","title":"A generalized sound extrapolation method for turbulent flows","url":"/publications/134/","summary":"Zhong, Siyang; Zhang, Xin. “A generalized sound extrapolation method for turbulent flows.” Proceedings of the Royal Society A: Mathematical, Physical and Engineering Sciences, v. 474, (2210), article number 20170614. (2018). DOI: 10.1098/rspa.2017.0614.","meta":"Journal article · 2018","search_text":"a generalized sound extrapolation method for turbulent flows zhong, siyang; zhang, xin. “a generalized sound extrapolation method for turbulent flows.” proceedings of the royal society a: mathematical, physical and engineering sciences, v. 474, (2210), article number 20170614. (2018). doi: 10.1098/rspa.2017.0614. journal article · 2018 zhong, siyang; zhang, xin 2018 10.1098/rspa.2017.0614 proceedings of the royal society a: mathematical, physical and engineering sciences 474 (2210) article 20170614","order":326,"static_url":"/publications/134/"},{"section":"Publications","title":"On modeling the sound propagation through a lined duct with a modified Ingard-Myers boundary condition","url":"/publications/133/","summary":"Yang, Cheng; Fang, Yi; Zhao, Chao; Zhang, Xin. “On modeling the sound propagation through a lined duct with a modified Ingard-Myers boundary condition.” Journal of Sound and Vibration, v. 424, p. 173-191. (2018). DOI: 10.1016/j.jsv.2018.03.022.","meta":"Journal article · 2018","search_text":"on modeling the sound propagation through a lined duct with a modified ingard-myers boundary condition yang, cheng; fang, yi; zhao, chao; zhang, xin. “on modeling the sound propagation through a lined duct with a modified ingard-myers boundary condition.” journal of sound and vibration, v. 424, p. 173-191. (2018). doi: 10.1016/j.jsv.2018.03.022. journal article · 2018 yang, cheng; fang, yi; zhao, chao; zhang, xin 2018 10.1016/j.jsv.2018.03.022 journal of sound and vibration 424 173-191","order":327,"static_url":"/publications/133/"},{"section":"Publications","title":"Experiments on reflection and transmission of acoustic porous metasurface with composite structure","url":"/publications/131/","summary":"Fang, Yi; Zhang, Xin; Zhou, Jie. “Experiments on reflection and transmission of acoustic porous metasurface with composite structure.” Composite Structures, v. 185, p. 508-514. (2018). DOI: 10.1016/j.compstruct.2017.11.054.","meta":"Journal article · 2018","search_text":"experiments on reflection and transmission of acoustic porous metasurface with composite structure fang, yi; zhang, xin; zhou, jie. “experiments on reflection and transmission of acoustic porous metasurface with composite structure.” composite structures, v. 185, p. 508-514. (2018). doi: 10.1016/j.compstruct.2017.11.054. journal article · 2018 fang, yi; zhang, xin; zhou, jie 2018 10.1016/j.compstruct.2017.11.054 composite structures 185 508-514","order":328,"static_url":"/publications/131/"},{"section":"Publications","title":"Acoustic porous metasurface for excellent sound absorption based on wave manipulation","url":"/publications/129/","summary":"Fang, Yi; Zhang, Xin; Zhou, Jie. “Acoustic porous metasurface for excellent sound absorption based on wave manipulation.” Journal of Sound and Vibration, v. 434, p. 273-283. (2018). DOI: 10.1016/j.jsv.2018.08.003.","meta":"Journal article · 2018","search_text":"acoustic porous metasurface for excellent sound absorption based on wave manipulation fang, yi; zhang, xin; zhou, jie. “acoustic porous metasurface for excellent sound absorption based on wave manipulation.” journal of sound and vibration, v. 434, p. 273-283. (2018). doi: 10.1016/j.jsv.2018.08.003. journal article · 2018 fang, yi; zhang, xin; zhou, jie 2018 10.1016/j.jsv.2018.08.003 journal of sound and vibration 434 273-283","order":329,"static_url":"/publications/129/"},{"section":"Publications","title":"Stable time-domain CAA simulations with linearised governing equations","url":"/publications/128/","summary":"Sun, Yuhao; Fattah, Ryu; Zhong, Siyang; Zhang, Xin. “Stable time-domain CAA simulations with linearised governing equations.” Computers and Fluids, v. 167, p. 187-195. (2018). DOI: 10.1016/j.compfluid.2018.03.025.","meta":"Journal article · 2018","search_text":"stable time-domain caa simulations with linearised governing equations sun, yuhao; fattah, ryu; zhong, siyang; zhang, xin. “stable time-domain caa simulations with linearised governing equations.” computers and fluids, v. 167, p. 187-195. (2018). doi: 10.1016/j.compfluid.2018.03.025. journal article · 2018 sun, yuhao; fattah, ryu; zhong, siyang; zhang, xin 2018 10.1016/j.compfluid.2018.03.025 computers and fluids 167 187-195","order":330,"static_url":"/publications/128/"},{"section":"Publications","title":"Reflected wave manipulation by inhomogeneous impedance via varying-depth acoustic liners","url":"/publications/127/","summary":"Guo, Jingwen; Zhang, Xin; Fang, Yi; Fattah, Ryu. “Reflected wave manipulation by inhomogeneous impedance via varying-depth acoustic liners.” Journal of Applied Physics, v. 123, (17), article number 174902. (2018). DOI: 10.1063/1.5022127.","meta":"Journal article · 2018","search_text":"reflected wave manipulation by inhomogeneous impedance via varying-depth acoustic liners guo, jingwen; zhang, xin; fang, yi; fattah, ryu. “reflected wave manipulation by inhomogeneous impedance via varying-depth acoustic liners.” journal of applied physics, v. 123, (17), article number 174902. (2018). doi: 10.1063/1.5022127. journal article · 2018 guo, jingwen; zhang, xin; fang, yi; fattah, ryu 2018 10.1063/1.5022127 journal of applied physics 123 (17) article 174902","order":331,"static_url":"/publications/127/"},{"section":"Publications","title":"Manipulating reflected acoustic wave via Helmholtz resonators with varying-length extended necks","url":"/publications/126/","summary":"Guo, Jingwen; Zhang, Xin; Fang, Yi; Fattah, Ryu. “Manipulating reflected acoustic wave via Helmholtz resonators with varying-length extended necks.” Journal of Applied Physics, v. 124, (10), article number 104902. (2018). DOI: 10.1063/1.5042152.","meta":"Journal article · 2018","search_text":"manipulating reflected acoustic wave via helmholtz resonators with varying-length extended necks guo, jingwen; zhang, xin; fang, yi; fattah, ryu. “manipulating reflected acoustic wave via helmholtz resonators with varying-length extended necks.” journal of applied physics, v. 124, (10), article number 104902. (2018). doi: 10.1063/1.5042152. journal article · 2018 guo, jingwen; zhang, xin; fang, yi; fattah, ryu 2018 10.1063/1.5042152 journal of applied physics 124 (10) article 104902","order":332,"static_url":"/publications/126/"},{"section":"Publications","title":"Analytical modelling for predicting the sound field of planar acoustic metasurface","url":"/publications/124/","summary":"Zhou, Jie; Zhang, Xin; Fang, Yi. “Analytical modelling for predicting the sound field of planar acoustic metasurface.” Journal of Applied Physics, v. 123, (3), article number 033106. (2018). DOI: 10.1063/1.5000055.","meta":"Journal article · 2018","search_text":"analytical modelling for predicting the sound field of planar acoustic metasurface zhou, jie; zhang, xin; fang, yi. “analytical modelling for predicting the sound field of planar acoustic metasurface.” journal of applied physics, v. 123, (3), article number 033106. (2018). doi: 10.1063/1.5000055. journal article · 2018 zhou, jie; zhang, xin; fang, yi 2018 10.1063/1.5000055 journal of applied physics 123 (3) article 033106","order":333,"static_url":"/publications/124/"},{"section":"Publications","title":"Extension of roughness noise to bluff bodies using the boundary element method","url":"/publications/120/","summary":"Alomar, Antoni; Angland, David; Zhang, Xin. “Extension of roughness noise to bluff bodies using the boundary element method.” Journal of Sound and Vibration, v. 414, p. 318-337 (2018). DOI: 10.1016/j.jsv.2017.09.021.","meta":"Journal article · 2018","search_text":"extension of roughness noise to bluff bodies using the boundary element method alomar, antoni; angland, david; zhang, xin. “extension of roughness noise to bluff bodies using the boundary element method.” journal of sound and vibration, v. 414, p. 318-337 (2018). doi: 10.1016/j.jsv.2017.09.021. journal article · 2018 alomar, antoni; angland, david; zhang, xin 2018 10.1016/j.jsv.2017.09.021 journal of sound and vibration, v. 414, p. 318-337","order":334,"static_url":"/publications/120/"},{"section":"Publications","title":"Wavy leading edge airfoils interacting with anisotropic turbulence","url":"/publications/346/","summary":"Gea-Aguilera, Fernando; Gill, James; Angland, David; Zhang, Xin. “Wavy leading edge airfoils interacting with anisotropic turbulence.” 23rd AIAA/CEAS Aeroacoustics Conference, 2017, American Institute of Aeronautics and Astronautics Inc, AIAA, 2017, (2017). DOI: 10.2514/6.2017-3…","meta":"Conference paper · 2017","search_text":"wavy leading edge airfoils interacting with anisotropic turbulence gea-aguilera, fernando; gill, james; angland, david; zhang, xin. “wavy leading edge airfoils interacting with anisotropic turbulence.” 23rd aiaa/ceas aeroacoustics conference, 2017, american institute of aeronautics and astronautics inc, aiaa, 2017, (2017). doi: 10.2514/6.2017-3370. conference paper · 2017 gea-aguilera, fernando; gill, james; angland, david; zhang, xin 2017 10.2514/6.2017-3370 23rd aiaa/ceas aeroacoustics conference, 2017, american institute of aeronautics and astronautics inc, aiaa, 2017,","order":335,"static_url":"/publications/346/"},{"section":"Publications","title":"An experimental and numerical study of the tonal noise from two scall-scale propellers","url":"/publications/345/","summary":"Fattah, Ryu; Zhou, Teng; Zhang, Xin. “An experimental and numerical study of the tonal noise from two scall-scale propellers.” Paper presented at 46th International Congress and Exposition on Noise Control Engineering: Taming Noise and Moving Quiet, INTER-NOISE 2017, Hong Kong, …","meta":"Conference paper · 2017","search_text":"an experimental and numerical study of the tonal noise from two scall-scale propellers fattah, ryu; zhou, teng; zhang, xin. “an experimental and numerical study of the tonal noise from two scall-scale propellers.” paper presented at 46th international congress and exposition on noise control engineering: taming noise and moving quiet, inter-noise 2017, hong kong, china. (2017). conference paper · 2017 fattah, ryu; zhou, teng; zhang, xin 2017 paper presented at 46th international congress and exposition on noise control engineering: taming noise and moving quiet, inter-noise 2017, hong kong, china","order":336,"static_url":"/publications/345/"},{"section":"Publications","title":"Airfoil leading edge noise predictions using a viscous mean flow","url":"/publications/344/","summary":"Sun, Yuhao; Fattah, Ryu; Zhang, Xin. “Airfoil leading edge noise predictions using a viscous mean flow.” Paper presented at 24th International Congress on Sound and Vibration, ICSV 2017, London, United Kingdom. (2017). DOI: 10.25144/24789.","meta":"Conference paper · 2017","search_text":"airfoil leading edge noise predictions using a viscous mean flow sun, yuhao; fattah, ryu; zhang, xin. “airfoil leading edge noise predictions using a viscous mean flow.” paper presented at 24th international congress on sound and vibration, icsv 2017, london, united kingdom. (2017). doi: 10.25144/24789. conference paper · 2017 sun, yuhao; fattah, ryu; zhang, xin 2017 10.25144/24789 paper presented at 24th international congress on sound and vibration, icsv 2017, london, united kingdom","order":337,"static_url":"/publications/344/"},{"section":"Publications","title":"A numerical study of the airfoil leading edge noise in transonic flows","url":"/publications/343/","summary":"Zhong, Siyang; Zhang, Xin; Gill, James; Fattah, Ryu. “A numerical study of the airfoil leading edge noise in transonic flows.” Paper presented at 46th International Congress and Exposition on Noise Control Engineering: Taming Noise and Moving Quiet, INTER-NOISE 2017, Hong Kong, …","meta":"Conference paper · 2017","search_text":"a numerical study of the airfoil leading edge noise in transonic flows zhong, siyang; zhang, xin; gill, james; fattah, ryu. “a numerical study of the airfoil leading edge noise in transonic flows.” paper presented at 46th international congress and exposition on noise control engineering: taming noise and moving quiet, inter-noise 2017, hong kong, china. (2017). conference paper · 2017 zhong, siyang; zhang, xin; gill, james; fattah, ryu 2017 paper presented at 46th international congress and exposition on noise control engineering: taming noise and moving quiet, inter-noise 2017, hong kong, china","order":338,"static_url":"/publications/343/"},{"section":"Publications","title":"A numerical investigation of the airfoil-gust interaction noise in transonic flows","url":"/publications/342/","summary":"Zhong, Siyang; Zhang, Xin; Gill, James; Fattah, Ryu. “A numerical investigation of the airfoil-gust interaction noise in transonic flows.” 23rd AIAA/CEAS Aeroacoustics Conference, 2017, American Institute of Aeronautics and Astronautics Inc, AIAA, 2017. (2017). DOI: 10.2514/6.20…","meta":"Conference paper · 2017","search_text":"a numerical investigation of the airfoil-gust interaction noise in transonic flows zhong, siyang; zhang, xin; gill, james; fattah, ryu. “a numerical investigation of the airfoil-gust interaction noise in transonic flows.” 23rd aiaa/ceas aeroacoustics conference, 2017, american institute of aeronautics and astronautics inc, aiaa, 2017. (2017). doi: 10.2514/6.2017-3369. conference paper · 2017 zhong, siyang; zhang, xin; gill, james; fattah, ryu 2017 10.2514/6.2017-3369 23rd aiaa/ceas aeroacoustics conference, 2017, american institute of aeronautics and astronautics inc, aiaa, 2017","order":339,"static_url":"/publications/342/"},{"section":"Publications","title":"A numerical investigation of the airfoil leading edge noise in transonic flows","url":"/publications/341/","summary":"Gill, James; Fattah, Ryu Jahangir; Zhang, Xin; Zhong, Siyang. “A numerical investigation of the airfoil leading edge noise in transonic flows.” Paper presented at INTER-NOISE and NOISE-CON Congress and Conference Proceedings, InterNoise17, p. 3915-3926. (2017).","meta":"Conference paper · 2017","search_text":"a numerical investigation of the airfoil leading edge noise in transonic flows gill, james; fattah, ryu jahangir; zhang, xin; zhong, siyang. “a numerical investigation of the airfoil leading edge noise in transonic flows.” paper presented at inter-noise and noise-con congress and conference proceedings, internoise17, p. 3915-3926. (2017). conference paper · 2017 gill, james; fattah, ryu jahangir; zhang, xin; zhong, siyang 2017 paper presented at inter-noise and noise-con congress and conference proceedings, internoise17, p. 3915-3926 3915-3926","order":340,"static_url":"/publications/341/"},{"section":"Publications","title":"A hybrid high-order sliding mesh interface for finite difference schemes","url":"/publications/340/","summary":"Fattah, Ryu; Zhang, Xin. “A hybrid high-order sliding mesh interface for finite difference schemes.” Paper presented at 24th International Congress on Sound and Vibration, ICSV 2017, London, United Kingdom. (2017). DOI: 10.25144/24480.","meta":"Conference paper · 2017","search_text":"a hybrid high-order sliding mesh interface for finite difference schemes fattah, ryu; zhang, xin. “a hybrid high-order sliding mesh interface for finite difference schemes.” paper presented at 24th international congress on sound and vibration, icsv 2017, london, united kingdom. (2017). doi: 10.25144/24480. conference paper · 2017 fattah, ryu; zhang, xin 2017 10.25144/24480 paper presented at 24th international congress on sound and vibration, icsv 2017, london, united kingdom","order":341,"static_url":"/publications/340/"},{"section":"Publications","title":"A study of the sound transmission mechanisms of a finite thickness opening without or with an acoustic seal","url":"/publications/339/","summary":"Yang, Cheng; Zhang, Xin; Tao, Fuyang; Lam, David Chuenchun. “A study of the sound transmission mechanisms of a finite thickness opening without or with an acoustic seal.” Applied Acoustics, v. 122, p. 156-166 (2017). DOI: 10.1016/j.apacoust.2017.02.012.","meta":"Journal article · 2017","search_text":"a study of the sound transmission mechanisms of a finite thickness opening without or with an acoustic seal yang, cheng; zhang, xin; tao, fuyang; lam, david chuenchun. “a study of the sound transmission mechanisms of a finite thickness opening without or with an acoustic seal.” applied acoustics, v. 122, p. 156-166 (2017). doi: 10.1016/j.apacoust.2017.02.012. journal article · 2017 yang, cheng; zhang, xin; tao, fuyang; lam, david chuenchun 2017 10.1016/j.apacoust.2017.02.012 applied acoustics, v. 122, p. 156-166","order":342,"static_url":"/publications/339/"},{"section":"Publications","title":"Sound transmission through an acoustic porous metasurface with periodic structures","url":"/publications/132/","summary":"Fang, Yi; Zhang, Xin; Zhou, Jie. “Sound transmission through an acoustic porous metasurface with periodic structures.” Applied Physics Letters, v. 110, (17), article number 171904. (2017). DOI: 10.1063/1.4982633.","meta":"Journal article · 2017","search_text":"sound transmission through an acoustic porous metasurface with periodic structures fang, yi; zhang, xin; zhou, jie. “sound transmission through an acoustic porous metasurface with periodic structures.” applied physics letters, v. 110, (17), article number 171904. (2017). doi: 10.1063/1.4982633. journal article · 2017 fang, yi; zhang, xin; zhou, jie 2017 10.1063/1.4982633 applied physics letters 110 (17) article 171904","order":343,"static_url":"/publications/132/"},{"section":"Publications","title":"Investigation of the sound generation mechanisms for in-duct orifice plates","url":"/publications/122/","summary":"Tao, Fuyang; Joseph, Phillip; Zhang, Xin; Stalnov, Oksana; Siercke, Matthias; Scheel, Henning. “Investigation of the sound generation mechanisms for in-duct orifice plates.” Journal of the Acoustical Society of America, v. 142, (2), p. 561-572 (2017). DOI: 10.1121/1.4996459.","meta":"Journal article · 2017","search_text":"investigation of the sound generation mechanisms for in-duct orifice plates tao, fuyang; joseph, phillip; zhang, xin; stalnov, oksana; siercke, matthias; scheel, henning. “investigation of the sound generation mechanisms for in-duct orifice plates.” journal of the acoustical society of america, v. 142, (2), p. 561-572 (2017). doi: 10.1121/1.4996459. journal article · 2017 tao, fuyang; joseph, phillip; zhang, xin; stalnov, oksana; siercke, matthias; scheel, henning 2017 10.1121/1.4996459 journal of the acoustical society of america, v. 142, (2), p. 561-572","order":344,"static_url":"/publications/122/"},{"section":"Publications","title":"Synthetic turbulence methods for computational aeroacoustic simulations of leading edge noise","url":"/publications/121/","summary":"Gea-Aguilera, Fernando; Gill, James; Zhang, Xin. “Synthetic turbulence methods for computational aeroacoustic simulations of leading edge noise.” Computers and Fluids, v. 157, p. 240-252 (2017). DOI: 10.1016/j.compfluid.2017.08.039.","meta":"Journal article · 2017","search_text":"synthetic turbulence methods for computational aeroacoustic simulations of leading edge noise gea-aguilera, fernando; gill, james; zhang, xin. “synthetic turbulence methods for computational aeroacoustic simulations of leading edge noise.” computers and fluids, v. 157, p. 240-252 (2017). doi: 10.1016/j.compfluid.2017.08.039. journal article · 2017 gea-aguilera, fernando; gill, james; zhang, xin 2017 10.1016/j.compfluid.2017.08.039 computers and fluids, v. 157, p. 240-252","order":345,"static_url":"/publications/121/"},{"section":"Publications","title":"The noise generated by a landing gear wheel with hub and rim cavities","url":"/publications/119/","summary":"Wang, Meng; Angland, David; Zhang, Xin. “The noise generated by a landing gear wheel with hub and rim cavities.” Journal of Sound and Vibration, v. 392, p. 127-141 (2017). DOI: 10.1016/j.jsv.2016.12.045.","meta":"Journal article · 2017","search_text":"the noise generated by a landing gear wheel with hub and rim cavities wang, meng; angland, david; zhang, xin. “the noise generated by a landing gear wheel with hub and rim cavities.” journal of sound and vibration, v. 392, p. 127-141 (2017). doi: 10.1016/j.jsv.2016.12.045. journal article · 2017 wang, meng; angland, david; zhang, xin 2017 10.1016/j.jsv.2016.12.045 journal of sound and vibration, v. 392, p. 127-141","order":346,"static_url":"/publications/119/"},{"section":"Publications","title":"Towards an effective non-reflective boundary condition for computational aeroacoustics","url":"/publications/118/","summary":"Gill, James; Fattah, Ryu; Zhang, Xin. “Towards an effective non-reflective boundary condition for computational aeroacoustics.” Journal of Sound and Vibration, v. 392, p. 217-231. (2017). DOI: 10.1016/j.jsv.2016.11.036.","meta":"Journal article · 2017","search_text":"towards an effective non-reflective boundary condition for computational aeroacoustics gill, james; fattah, ryu; zhang, xin. “towards an effective non-reflective boundary condition for computational aeroacoustics.” journal of sound and vibration, v. 392, p. 217-231. (2017). doi: 10.1016/j.jsv.2016.11.036. journal article · 2017 gill, james; fattah, ryu; zhang, xin 2017 10.1016/j.jsv.2016.11.036 journal of sound and vibration 392 217-231","order":347,"static_url":"/publications/118/"},{"section":"Publications","title":"Unsteady aerodynamics of single and tandem wheels","url":"/publications/117/","summary":"Spagnolo, Stefano; Zhang, Xin; Hu, Zhiwei; Stalnov, Oksana; Angland, David. “Unsteady aerodynamics of single and tandem wheels.” Journal of Fluids and Structures, v. 69, p. 121-136 (2017). DOI: 10.1016/j.jfluidstructs.2016.11.022.","meta":"Journal article · 2017","search_text":"unsteady aerodynamics of single and tandem wheels spagnolo, stefano; zhang, xin; hu, zhiwei; stalnov, oksana; angland, david. “unsteady aerodynamics of single and tandem wheels.” journal of fluids and structures, v. 69, p. 121-136 (2017). doi: 10.1016/j.jfluidstructs.2016.11.022. journal article · 2017 spagnolo, stefano; zhang, xin; hu, zhiwei; stalnov, oksana; angland, david 2017 10.1016/j.jfluidstructs.2016.11.022 journal of fluids and structures, v. 69, p. 121-136","order":348,"static_url":"/publications/117/"},{"section":"Publications","title":"A sound extrapolation method for aeroacoustics far-field prediction in presence of vortical waves","url":"/publications/116/","summary":"Zhong, Siyang; Zhang, Xin. “A sound extrapolation method for aeroacoustics far-field prediction in presence of vortical waves.” Journal of Fluid Mechanics, v. 820, p. 424-450. (2017). DOI: 10.1017/jfm.2017.219.","meta":"Journal article · 2017","search_text":"a sound extrapolation method for aeroacoustics far-field prediction in presence of vortical waves zhong, siyang; zhang, xin. “a sound extrapolation method for aeroacoustics far-field prediction in presence of vortical waves.” journal of fluid mechanics, v. 820, p. 424-450. (2017). doi: 10.1017/jfm.2017.219. journal article · 2017 zhong, siyang; zhang, xin 2017 10.1017/jfm.2017.219 journal of fluid mechanics 820 424-450","order":349,"static_url":"/publications/116/"},{"section":"Publications","title":"Three-dimensional acoustic characteristic study of porous metasurface","url":"/publications/113/","summary":"Zhou, Jie; Zhang, Xin; Fang, Yi. “Three-dimensional acoustic characteristic study of porous metasurface.” Composite Structures, v. 176, p. 1005-1012. (2017). DOI: 10.1016/j.compstruct.2017.06.050.","meta":"Journal article · 2017","search_text":"three-dimensional acoustic characteristic study of porous metasurface zhou, jie; zhang, xin; fang, yi. “three-dimensional acoustic characteristic study of porous metasurface.” composite structures, v. 176, p. 1005-1012. (2017). doi: 10.1016/j.compstruct.2017.06.050. journal article · 2017 zhou, jie; zhang, xin; fang, yi 2017 10.1016/j.compstruct.2017.06.050 composite structures 176 1005-1012","order":350,"static_url":"/publications/113/"},{"section":"Publications","title":"Turbulence-cascade interaction noise using an advanced digital filter method","url":"/publications/354/","summary":"Gea-Aguilera, Fernando; Gill, James; Zhang, Xin; Nodé-Langlois, Thomas. “Turbulence-cascade interaction noise using an advanced digital filter method.” ICSV 2016 - 23rd International Congress on Sound and Vibration, International Institute of Acoustics and Vibrations, 2016, (201…","meta":"Conference paper · 2016","search_text":"turbulence-cascade interaction noise using an advanced digital filter method gea-aguilera, fernando; gill, james; zhang, xin; nodé-langlois, thomas. “turbulence-cascade interaction noise using an advanced digital filter method.” icsv 2016 - 23rd international congress on sound and vibration, international institute of acoustics and vibrations, 2016, (2016). conference paper · 2016 gea-aguilera, fernando; gill, james; zhang, xin; nodé-langlois, thomas 2016 icsv 2016 - 23rd international congress on sound and vibration, international institute of acoustics and vibrations, 2016,","order":351,"static_url":"/publications/354/"},{"section":"Publications","title":"On the acoustic properties of a hole in a wall of finite thickness","url":"/publications/353/","summary":"Yang, Cheng; Zhang, Xin; Tao, Fuyang. “On the acoustic properties of a hole in a wall of finite thickness.” 2nd Australasian Acoustical Societies Conference, ACOUSTICS 2016, Australian Acoustical Society, 2016, p. 1058-1067 (2016).","meta":"Conference paper · 2016","search_text":"on the acoustic properties of a hole in a wall of finite thickness yang, cheng; zhang, xin; tao, fuyang. “on the acoustic properties of a hole in a wall of finite thickness.” 2nd australasian acoustical societies conference, acoustics 2016, australian acoustical society, 2016, p. 1058-1067 (2016). conference paper · 2016 yang, cheng; zhang, xin; tao, fuyang 2016 2nd australasian acoustical societies conference, acoustics 2016, australian acoustical society, 2016, p. 1058-1067","order":352,"static_url":"/publications/353/"},{"section":"Publications","title":"Experimental study of the mechanisms of sound generation due to an in-duct orifice plate","url":"/publications/352/","summary":"Tao, Fuyang; Zhang, Xin; Joseph, Phillip; Stalnov, Oksana; Siercke, Matthias; Scheel, Henning. “Experimental study of the mechanisms of sound generation due to an in-duct orifice plate.” 21st AIAA/CEAS Aeroacoustics Conference, American Institute of Aeronautics and Astronautics …","meta":"Conference paper · 2016","search_text":"experimental study of the mechanisms of sound generation due to an in-duct orifice plate tao, fuyang; zhang, xin; joseph, phillip; stalnov, oksana; siercke, matthias; scheel, henning. “experimental study of the mechanisms of sound generation due to an in-duct orifice plate.” 21st aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc, aiaa, 2016, (2016). doi: 10.2514/6.2015-2231. conference paper · 2016 tao, fuyang; zhang, xin; joseph, phillip; stalnov, oksana; siercke, matthias; scheel, henning 2016 10.2514/6.2015-2231 21st aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc, aiaa, 2016,","order":353,"static_url":"/publications/352/"},{"section":"Publications","title":"Evaluation and development of non-reflective boundary conditions for aeroacoustic simulations","url":"/publications/351/","summary":"Gill, James; Fattah, Ryu; Zhang, Xin. “Evaluation and development of non-reflective boundary conditions for aeroacoustic simulations.” 21st AIAA/CEAS Aeroacoustics Conference, American Institute of Aeronautics and Astronautics Inc, AIAA, 2016. (2016). DOI: 10.2514/6.2015-2677.","meta":"Conference paper · 2016","search_text":"evaluation and development of non-reflective boundary conditions for aeroacoustic simulations gill, james; fattah, ryu; zhang, xin. “evaluation and development of non-reflective boundary conditions for aeroacoustic simulations.” 21st aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc, aiaa, 2016. (2016). doi: 10.2514/6.2015-2677. conference paper · 2016 gill, james; fattah, ryu; zhang, xin 2016 10.2514/6.2015-2677 21st aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc, aiaa, 2016","order":354,"static_url":"/publications/351/"},{"section":"Publications","title":"An evaluation of gradient term modification methods for linearized euler equations","url":"/publications/350/","summary":"Sun, Yuhao; Zhong, Siyang; Fattah, Ryu; Zhang, Xin; Chen, Xiaoxian. “An evaluation of gradient term modification methods for linearized euler equations.” ICSV 2016 - 23rd International Congress on Sound and Vibration, International Institute of Acoustics and Vibrations, 2016. (2…","meta":"Conference paper · 2016","search_text":"an evaluation of gradient term modification methods for linearized euler equations sun, yuhao; zhong, siyang; fattah, ryu; zhang, xin; chen, xiaoxian. “an evaluation of gradient term modification methods for linearized euler equations.” icsv 2016 - 23rd international congress on sound and vibration, international institute of acoustics and vibrations, 2016. (2016). conference paper · 2016 sun, yuhao; zhong, siyang; fattah, ryu; zhang, xin; chen, xiaoxian 2016 icsv 2016 - 23rd international congress on sound and vibration, international institute of acoustics and vibrations, 2016","order":355,"static_url":"/publications/350/"},{"section":"Publications","title":"A comparison of wall functions for bluff body aeroacoustic simulations","url":"/publications/349/","summary":"Hou, Yu; Angland, David; Zhang, Xin. “A comparison of wall functions for bluff body aeroacoustic simulations.” 22nd AIAA/CEAS Aeroacoustics Conference, American Institute of Aeronautics and Astronautics Inc, AIAA, 2016, (2016). DOI: 10.2514/6.2016-2771.","meta":"Conference paper · 2016","search_text":"a comparison of wall functions for bluff body aeroacoustic simulations hou, yu; angland, david; zhang, xin. “a comparison of wall functions for bluff body aeroacoustic simulations.” 22nd aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc, aiaa, 2016, (2016). doi: 10.2514/6.2016-2771. conference paper · 2016 hou, yu; angland, david; zhang, xin 2016 10.2514/6.2016-2771 22nd aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc, aiaa, 2016,","order":356,"static_url":"/publications/349/"},{"section":"Publications","title":"Aircraft Noise Modeling","url":"/publications/348/","summary":"Zhang, Xin; Gill, James; Angland, David. “Aircraft Noise Modeling.” Green Aviation / John Wiley & Sons, Ltd., 2016, p. 277-286 (2016). DOI: 10.1002/9780470686652.eae1046.","meta":"Book chapter · 2016","search_text":"aircraft noise modeling zhang, xin; gill, james; angland, david. “aircraft noise modeling.” green aviation / john wiley & sons, ltd., 2016, p. 277-286 (2016). doi: 10.1002/9780470686652.eae1046. book chapter · 2016 zhang, xin; gill, james; angland, david 2016 10.1002/9780470686652.eae1046 green aviation / john wiley & sons, ltd., 2016, p. 277-286","order":357,"static_url":"/publications/348/"},{"section":"Publications","title":"Aerodynamics of a pitching and heaving airfoil in ground effect","url":"/publications/347/","summary":"Molina, Juan; Zhang, Xin; Alomar, Antoni. “Aerodynamics of a pitching and heaving airfoil in ground effect.” AIAA Journal, v. 54, (4), p. 1158-1171 (2016). DOI: 10.2514/1.j053350.","meta":"Journal article · 2016","search_text":"aerodynamics of a pitching and heaving airfoil in ground effect molina, juan; zhang, xin; alomar, antoni. “aerodynamics of a pitching and heaving airfoil in ground effect.” aiaa journal, v. 54, (4), p. 1158-1171 (2016). doi: 10.2514/1.j053350. journal article · 2016 molina, juan; zhang, xin; alomar, antoni 2016 10.2514/1.j053350 aiaa journal, v. 54, (4), p. 1158-1171","order":358,"static_url":"/publications/347/"},{"section":"Publications","title":"A priori grid quality estimation for high-order finite differencing","url":"/publications/115/","summary":"Fattah, Ryu; Angland, David; Zhang, Xin. “A priori grid quality estimation for high-order finite differencing.” Journal of Computational Physics, v. 315, p. 629-643. (2016). DOI: 10.1016/j.jcp.2016.03.063.","meta":"Journal article · 2016","search_text":"a priori grid quality estimation for high-order finite differencing fattah, ryu; angland, david; zhang, xin. “a priori grid quality estimation for high-order finite differencing.” journal of computational physics, v. 315, p. 629-643. (2016). doi: 10.1016/j.jcp.2016.03.063. journal article · 2016 fattah, ryu; angland, david; zhang, xin 2016 10.1016/j.jcp.2016.03.063 journal of computational physics 315 629-643","order":359,"static_url":"/publications/115/"},{"section":"Publications","title":"A controllable canonical form implementation of time domain impedance boundary conditions for broadband aeroacoustic computation","url":"/publications/114/","summary":"Zhong, Siyang; Zhang, Xin; Huang, Xun. “A controllable canonical form implementation of time domain impedance boundary conditions for broadband aeroacoustic computation.” Journal of Computational Physics, v. 313, p. 713-725. (2016). DOI: 10.1016/j.jcp.2016.03.002.","meta":"Journal article · 2016","search_text":"a controllable canonical form implementation of time domain impedance boundary conditions for broadband aeroacoustic computation zhong, siyang; zhang, xin; huang, xun. “a controllable canonical form implementation of time domain impedance boundary conditions for broadband aeroacoustic computation.” journal of computational physics, v. 313, p. 713-725. (2016). doi: 10.1016/j.jcp.2016.03.002. journal article · 2016 zhong, siyang; zhang, xin; huang, xun 2016 10.1016/j.jcp.2016.03.002 journal of computational physics 313 713-725","order":360,"static_url":"/publications/114/"},{"section":"Publications","title":"Synthetic turbulence methods for leading edge noise predictions","url":"/publications/112/","summary":"Gea-Aguilera, Fernando; Zhang, Xin; Chen, Xiaoxian; Gill, James; Nodé-Langlois, Thomas. “Synthetic turbulence methods for leading edge noise predictions.” 21st AIAA/CEAS Aeroacoustics Conference, American Institute of Aeronautics and Astronautics Inc, AIAA, 2016, (2016). DOI: 10…","meta":"Conference paper · 2016","search_text":"synthetic turbulence methods for leading edge noise predictions gea-aguilera, fernando; zhang, xin; chen, xiaoxian; gill, james; nodé-langlois, thomas. “synthetic turbulence methods for leading edge noise predictions.” 21st aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc, aiaa, 2016, (2016). doi: 10.2514/6.2015-2670. conference paper · 2016 gea-aguilera, fernando; zhang, xin; chen, xiaoxian; gill, james; nodé-langlois, thomas 2016 10.2514/6.2015-2670 21st aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc, aiaa, 2016,","order":361,"static_url":"/publications/112/"},{"section":"Publications","title":"Sound transmission through a circular hole without and with an acoustic seal","url":"/publications/111/","summary":"Yang, Cheng; Zhang, Xin; Tao, Fuyang; Lam, David Chuen Chun, \"Sound transmission through a circular hole without and with an acoustic seal,\" Proceedings of ACOUSTICS, 2016","meta":"Conference paper · 2016","search_text":"sound transmission through a circular hole without and with an acoustic seal yang, cheng; zhang, xin; tao, fuyang; lam, david chuen chun, \"sound transmission through a circular hole without and with an acoustic seal,\" proceedings of acoustics, 2016 conference paper · 2016 yang, cheng; zhang, xin; tao, fuyang; lam, david chuen chun 2016 proceedings of acoustics","order":362,"static_url":"/publications/111/"},{"section":"Publications","title":"Design and characterization of acoustic porous metasurface","url":"/publications/110/","summary":"Fang, Yi; Zhang, Xin; Zhou, Jie. “Design and characterization of acoustic porous metasurface.” ICSV 2016 - 23rd International Congress on Sound and Vibration, International Institute of Acoustics and Vibrations, 2016. (2016).","meta":"Conference paper · 2016","search_text":"design and characterization of acoustic porous metasurface fang, yi; zhang, xin; zhou, jie. “design and characterization of acoustic porous metasurface.” icsv 2016 - 23rd international congress on sound and vibration, international institute of acoustics and vibrations, 2016. (2016). conference paper · 2016 fang, yi; zhang, xin; zhou, jie 2016 icsv 2016 - 23rd international congress on sound and vibration, international institute of acoustics and vibrations, 2016","order":363,"static_url":"/publications/110/"},{"section":"Publications","title":"An evaluation of gradient term modification method for linearized Euler equations","url":"/publications/109/","summary":"Sun, Y., Zhong, S., Fattah, R., and Zhang, X., \"An evaluation of gradient term modification method for linearized Euler equations\" 23th International Congress on Sound & Vibration, Athens, Greece, from 10 to 14 July 2016, no.98, 2016.","meta":"Conference paper · 2016","search_text":"an evaluation of gradient term modification method for linearized euler equations sun, y., zhong, s., fattah, r., and zhang, x., \"an evaluation of gradient term modification method for linearized euler equations\" 23th international congress on sound & vibration, athens, greece, from 10 to 14 july 2016, no.98, 2016. conference paper · 2016 sun, y., zhong, s., fattah, r., and zhang, x 2016 23th international congress on sound & vibration no. 98","order":364,"static_url":"/publications/109/"},{"section":"Publications","title":"Artificial damping methods for stable computations with linearized euler equations","url":"/publications/108/","summary":"Sun, Yuhao; Zhong, Siyang; Zhang, Xin; Gill, James; Chen, Xiaoxian. “Artificial damping methods for stable computations with linearized euler equations.” 22nd AIAA/CEAS Aeroacoustics Conference, American Institute of Aeronautics and Astronautics Inc, AIAA, 2016. (2016). DOI: 10.…","meta":"Conference paper · 2016","search_text":"artificial damping methods for stable computations with linearized euler equations sun, yuhao; zhong, siyang; zhang, xin; gill, james; chen, xiaoxian. “artificial damping methods for stable computations with linearized euler equations.” 22nd aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc, aiaa, 2016. (2016). doi: 10.2514/6.2016-2971. conference paper · 2016 sun, yuhao; zhong, siyang; zhang, xin; gill, james; chen, xiaoxian 2016 10.2514/6.2016-2971 22nd aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc, aiaa, 2016","order":365,"static_url":"/publications/108/"},{"section":"Publications","title":"Airfoil-Gust Interactions in Transonic Flow","url":"/publications/107/","summary":"James Gill; Xin Zhang; Siyang Zhong; Ryu Fattah; David Angland. “Airfoil-Gust Interactions in Transonic Flow.” (2016). DOI: 10.2514/6.2016-2872.","meta":"Conference paper · 2016","search_text":"airfoil-gust interactions in transonic flow james gill; xin zhang; siyang zhong; ryu fattah; david angland. “airfoil-gust interactions in transonic flow.” (2016). doi: 10.2514/6.2016-2872. conference paper · 2016 james gill; xin zhang; siyang zhong; ryu fattah; david angland 2016 10.2514/6.2016-2872","order":366,"static_url":"/publications/107/"},{"section":"Publications","title":"Aerodynamic interactions between landing-gear components","url":"/publications/106/","summary":"Spagnolo, Stefano; Zhang, Xin; Hu, Zhiwei; Angland, David. “Aerodynamic interactions between landing-gear components.” 34th AIAA Applied Aerodynamics Conference, American Institute of Aeronautics and Astronautics Inc, AIAA, 2016, (2016). DOI: 10.2514/6.2016-3268.","meta":"Conference paper · 2016","search_text":"aerodynamic interactions between landing-gear components spagnolo, stefano; zhang, xin; hu, zhiwei; angland, david. “aerodynamic interactions between landing-gear components.” 34th aiaa applied aerodynamics conference, american institute of aeronautics and astronautics inc, aiaa, 2016, (2016). doi: 10.2514/6.2016-3268. conference paper · 2016 spagnolo, stefano; zhang, xin; hu, zhiwei; angland, david 2016 10.2514/6.2016-3268 34th aiaa applied aerodynamics conference, american institute of aeronautics and astronautics inc, aiaa, 2016,","order":367,"static_url":"/publications/106/"},{"section":"Publications","title":"Towards a Generic Non-Reflective Characteristic Boundary Condition for Aeroacoustic Simulations","url":"/publications/105/","summary":"Fattah Ryu, Gill James, Zhang Xin, \"Towards a Generic Non-Reflective Characteristic Boundary Condition for Aeroacoustic Simulations\" 22nd AIAA/CEAS Aeroacoustics Conference, Lyon, France, 30 May - 1 June 2016, AIAA Paper 2016-2914","meta":"Conference paper · 2016","search_text":"towards a generic non-reflective characteristic boundary condition for aeroacoustic simulations fattah ryu, gill james, zhang xin, \"towards a generic non-reflective characteristic boundary condition for aeroacoustic simulations\" 22nd aiaa/ceas aeroacoustics conference, lyon, france, 30 may - 1 june 2016, aiaa paper 2016-2914 conference paper · 2016 ryu j fattah; james r gill; xin zhang 2016 10.2514/6.2016-2914 22nd aiaa/ceas aeroacoustics conference","order":368,"static_url":"/publications/105/"},{"section":"Publications","title":"Computational analysis of partially-covered cavity with and without side walls","url":"/publications/104/","summary":"Premachandran, Sarah; Hu, Zhiwei; Zhang, Xin. “Computational analysis of partially-covered cavity with and without side walls.” 8th AIAA Flow Control Conference, American Institute of Aeronautics and Astronautics Inc, AIAA, 2016, (2016). DOI: 10.2514/6.2016-3174.","meta":"Conference paper · 2016","search_text":"computational analysis of partially-covered cavity with and without side walls premachandran, sarah; hu, zhiwei; zhang, xin. “computational analysis of partially-covered cavity with and without side walls.” 8th aiaa flow control conference, american institute of aeronautics and astronautics inc, aiaa, 2016, (2016). doi: 10.2514/6.2016-3174. conference paper · 2016 premachandran, sarah; hu, zhiwei; zhang, xin 2016 10.2514/6.2016-3174 8th aiaa flow control conference, american institute of aeronautics and astronautics inc, aiaa, 2016,","order":369,"static_url":"/publications/104/"},{"section":"Publications","title":"DDES simulation of a complex main landing gear with a six-wheel Bogie","url":"/publications/103/","summary":"Oza, Utsav; Hu, Zhiwei; Angland, David; Zhang, Xin. “DDES simulation of a complex main landing gear with a six-wheel Bogie.” 34th AIAA Applied Aerodynamics Conference, American Institute of Aeronautics and Astronautics Inc, AIAA, 2016, (2016). DOI: 10.2514/6.2016-3269.","meta":"Conference paper · 2016","search_text":"ddes simulation of a complex main landing gear with a six-wheel bogie oza, utsav; hu, zhiwei; angland, david; zhang, xin. “ddes simulation of a complex main landing gear with a six-wheel bogie.” 34th aiaa applied aerodynamics conference, american institute of aeronautics and astronautics inc, aiaa, 2016, (2016). doi: 10.2514/6.2016-3269. conference paper · 2016 oza, utsav; hu, zhiwei; angland, david; zhang, xin 2016 10.2514/6.2016-3269 34th aiaa applied aerodynamics conference, american institute of aeronautics and astronautics inc, aiaa, 2016,","order":370,"static_url":"/publications/103/"},{"section":"Publications","title":"High-order numerical simulations of an isolated landing gear wheel with a hub cavity","url":"/publications/102/","summary":"Wang, Meng; Angland, David; Zhang, Xin; Fattah, Ryu. “High-order numerical simulations of an isolated landing gear wheel with a hub cavity.” 22nd AIAA/CEAS Aeroacoustics Conference, American Institute of Aeronautics and Astronautics Inc, AIAA, 2016. (2016). DOI: 10.2514/6.2016-2…","meta":"Conference paper · 2016","search_text":"high-order numerical simulations of an isolated landing gear wheel with a hub cavity wang, meng; angland, david; zhang, xin; fattah, ryu. “high-order numerical simulations of an isolated landing gear wheel with a hub cavity.” 22nd aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc, aiaa, 2016. (2016). doi: 10.2514/6.2016-2902. conference paper · 2016 wang, meng; angland, david; zhang, xin; fattah, ryu 2016 10.2514/6.2016-2902 22nd aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc, aiaa, 2016","order":371,"static_url":"/publications/102/"},{"section":"Publications","title":"Leading edge noise predictions using anisotropic synthetic turbulence","url":"/publications/101/","summary":"Gea-Aguilera, Fernando; Gill, James; Zhang, Xin; Chen, Xiaoxian; Nodé-Langlois, Thomas. “Leading edge noise predictions using anisotropic synthetic turbulence.” 22nd AIAA/CEAS Aeroacoustics Conference, American Institute of Aeronautics and Astronautics Inc, AIAA, 2016, (2016). D…","meta":"Conference paper · 2016","search_text":"leading edge noise predictions using anisotropic synthetic turbulence gea-aguilera, fernando; gill, james; zhang, xin; chen, xiaoxian; nodé-langlois, thomas. “leading edge noise predictions using anisotropic synthetic turbulence.” 22nd aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc, aiaa, 2016, (2016). doi: 10.2514/6.2016-2840. conference paper · 2016 gea-aguilera, fernando; gill, james; zhang, xin; chen, xiaoxian; nodé-langlois, thomas 2016 10.2514/6.2016-2840 22nd aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc, aiaa, 2016,","order":372,"static_url":"/publications/101/"},{"section":"Publications","title":"Unsteady force and flow features of single and tandem wheels","url":"/publications/363/","summary":"Spagnolo, Stefano; Zhang, Xin; Hu, Zhiwei; Stalnov, Oksana; Angland, David. “Unsteady force and flow features of single and tandem wheels.” 53rd AIAA Aerospace Sciences Meeting, American Institute of Aeronautics and Astronautics Inc, AIAA, 2015, article number AIAA 2015-0261 (20…","meta":"Conference paper · 2015","search_text":"unsteady force and flow features of single and tandem wheels spagnolo, stefano; zhang, xin; hu, zhiwei; stalnov, oksana; angland, david. “unsteady force and flow features of single and tandem wheels.” 53rd aiaa aerospace sciences meeting, american institute of aeronautics and astronautics inc, aiaa, 2015, article number aiaa 2015-0261 (2015). doi: 10.2514/6.2015-0261. conference paper · 2015 spagnolo, stefano; zhang, xin; hu, zhiwei; stalnov, oksana; angland, david 2015 10.2514/6.2015-0261 53rd aiaa aerospace sciences meeting, american institute of aeronautics and astronautics inc, aiaa, 2015, article number aiaa 2015-0261","order":373,"static_url":"/publications/363/"},{"section":"Publications","title":"The effect of flow circulation on the scattering of landing gear noise","url":"/publications/362/","summary":"Heffernon, Timothy; Angland, David; Zhang, Xin; Smith, Malcolm. “The effect of flow circulation on the scattering of landing gear noise.” 21st AIAA/CEAS Aeroacoustics Conference, American Institute of Aeronautics and Astronautics Inc, AIAA, 2015, (2015). DOI: 10.2514/6.2015-3257.","meta":"Conference paper · 2015","search_text":"the effect of flow circulation on the scattering of landing gear noise heffernon, timothy; angland, david; zhang, xin; smith, malcolm. “the effect of flow circulation on the scattering of landing gear noise.” 21st aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc, aiaa, 2015, (2015). doi: 10.2514/6.2015-3257. conference paper · 2015 heffernon, timothy; angland, david; zhang, xin; smith, malcolm 2015 10.2514/6.2015-3257 21st aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc, aiaa, 2015,","order":374,"static_url":"/publications/362/"},{"section":"Publications","title":"Numerical simulations of single and tandem wheels for aerodynamic loads prediction","url":"/publications/361/","summary":"Spagnolo, Stefano; Zhang, Xin; Hu, Zhiwei; Angland, David. “Numerical simulations of single and tandem wheels for aerodynamic loads prediction.” 22nd AIAA Computational Fluid Dynamics Conference, American Institute of Aeronautics and Astronautics Inc, AIAA, 2015, (2015). DOI: 10…","meta":"Conference paper · 2015","search_text":"numerical simulations of single and tandem wheels for aerodynamic loads prediction spagnolo, stefano; zhang, xin; hu, zhiwei; angland, david. “numerical simulations of single and tandem wheels for aerodynamic loads prediction.” 22nd aiaa computational fluid dynamics conference, american institute of aeronautics and astronautics inc, aiaa, 2015, (2015). doi: 10.2514/6.2015-3066. conference paper · 2015 spagnolo, stefano; zhang, xin; hu, zhiwei; angland, david 2015 10.2514/6.2015-3066 22nd aiaa computational fluid dynamics conference, american institute of aeronautics and astronautics inc, aiaa, 2015,","order":375,"static_url":"/publications/361/"},{"section":"Publications","title":"Interior noise of cylindrical shell lined with porous material under turbulent boundary layer excitation","url":"/publications/360/","summary":"Zhou, Jie; Zhang, Xin. “Interior noise of cylindrical shell lined with porous material under turbulent boundary layer excitation.” 22nd International Congress on Sound and Vibration, ICSV 2015, International Institute of Acoustics and Vibrations, 2015, (2015).","meta":"Conference paper · 2015","search_text":"interior noise of cylindrical shell lined with porous material under turbulent boundary layer excitation zhou, jie; zhang, xin. “interior noise of cylindrical shell lined with porous material under turbulent boundary layer excitation.” 22nd international congress on sound and vibration, icsv 2015, international institute of acoustics and vibrations, 2015, (2015). conference paper · 2015 zhou, jie; zhang, xin 2015 22nd international congress on sound and vibration, icsv 2015, international institute of acoustics and vibrations, 2015,","order":376,"static_url":"/publications/360/"},{"section":"Publications","title":"High-order hybrid cell-centered method for computational aeroacoustics","url":"/publications/359/","summary":"Wang, Meng; Fattah, Ryu; Angland, David; Zhang, Xin. “High-order hybrid cell-centered method for computational aeroacoustics.” 21st AIAA/CEAS Aeroacoustics Conference, American Institute of Aeronautics and Astronautics Inc, AIAA, 2015. (2015). DOI: 10.2514/6.2015-3279.","meta":"Conference paper · 2015","search_text":"high-order hybrid cell-centered method for computational aeroacoustics wang, meng; fattah, ryu; angland, david; zhang, xin. “high-order hybrid cell-centered method for computational aeroacoustics.” 21st aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc, aiaa, 2015. (2015). doi: 10.2514/6.2015-3279. conference paper · 2015 wang, meng; fattah, ryu; angland, david; zhang, xin 2015 10.2514/6.2015-3279 21st aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc, aiaa, 2015","order":377,"static_url":"/publications/359/"},{"section":"Publications","title":"Evaluation and comparison of linearized euler equations and equivalent source method","url":"/publications/358/","summary":"Miao, Shuming; Hou, Yu; Zhang, Xin. “Evaluation and comparison of linearized euler equations and equivalent source method.” 22nd International Congress on Sound and Vibration, ICSV 2015, International Institute of Acoustics and Vibrations, 2015, (2015).","meta":"Conference paper · 2015","search_text":"evaluation and comparison of linearized euler equations and equivalent source method miao, shuming; hou, yu; zhang, xin. “evaluation and comparison of linearized euler equations and equivalent source method.” 22nd international congress on sound and vibration, icsv 2015, international institute of acoustics and vibrations, 2015, (2015). conference paper · 2015 miao, shuming; hou, yu; zhang, xin 2015 22nd international congress on sound and vibration, icsv 2015, international institute of acoustics and vibrations, 2015,","order":378,"static_url":"/publications/358/"},{"section":"Publications","title":"Effect of cavity flow on landing gear aerodynamic loads","url":"/publications/357/","summary":"Oza, Utsav; Hu, Zhiwei; Zhang, Xin. “Effect of cavity flow on landing gear aerodynamic loads.” 22nd AIAA Computational Fluid Dynamics Conference, American Institute of Aeronautics and Astronautics Inc, AIAA, 2015, (2015). DOI: 10.2514/6.2015-2288.","meta":"Conference paper · 2015","search_text":"effect of cavity flow on landing gear aerodynamic loads oza, utsav; hu, zhiwei; zhang, xin. “effect of cavity flow on landing gear aerodynamic loads.” 22nd aiaa computational fluid dynamics conference, american institute of aeronautics and astronautics inc, aiaa, 2015, (2015). doi: 10.2514/6.2015-2288. conference paper · 2015 oza, utsav; hu, zhiwei; zhang, xin 2015 10.2514/6.2015-2288 22nd aiaa computational fluid dynamics conference, american institute of aeronautics and astronautics inc, aiaa, 2015,","order":379,"static_url":"/publications/357/"},{"section":"Publications","title":"Aerofoil geometry effects on turbulence interaction noise","url":"/publications/356/","summary":"Chaitanya, P.; Gill, J.; Narayanan, S.; Joseph, P.; Vanderwel, C.; Zhang, X.; Ganapathisubramani, B.. “Aerofoil geometry effects on turbulence interaction noise.” 21st AIAA/CEAS Aeroacoustics Conference, American Institute of Aeronautics and Astronautics Inc, AIAA, 2015, (2015).…","meta":"Conference paper · 2015","search_text":"aerofoil geometry effects on turbulence interaction noise chaitanya, p.; gill, j.; narayanan, s.; joseph, p.; vanderwel, c.; zhang, x.; ganapathisubramani, b.. “aerofoil geometry effects on turbulence interaction noise.” 21st aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc, aiaa, 2015, (2015). doi: 10.2514/6.2015-2830. conference paper · 2015 chaitanya, p.; gill, j.; narayanan, s.; joseph, p.; vanderwel, c.; zhang, x.; ganapathisubramani, b. 2015 10.2514/6.2015-2830 21st aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc, aiaa, 2015,","order":380,"static_url":"/publications/356/"},{"section":"Publications","title":"Iterative learning control for trailing-edge flap lift enhancement with pulsed blowing","url":"/publications/355/","summary":"Cai, Zhonglun; Angland, David; Zhang, Xin; Chen, Peng. “Iterative learning control for trailing-edge flap lift enhancement with pulsed blowing.” AIAA Journal, v. 53, (7), p. 1969-1979 (2015). DOI: 10.2514/1.j053556.","meta":"Journal article · 2015","search_text":"iterative learning control for trailing-edge flap lift enhancement with pulsed blowing cai, zhonglun; angland, david; zhang, xin; chen, peng. “iterative learning control for trailing-edge flap lift enhancement with pulsed blowing.” aiaa journal, v. 53, (7), p. 1969-1979 (2015). doi: 10.2514/1.j053556. journal article · 2015 cai, zhonglun; angland, david; zhang, xin; chen, peng 2015 10.2514/1.j053556 aiaa journal, v. 53, (7), p. 1969-1979","order":381,"static_url":"/publications/355/"},{"section":"Publications","title":"Sound transmission through double cylindrical shells lined with porous material under turbulent boundary layer excitation","url":"/publications/100/","summary":"Zhou, Jie; Bhaskar, Atul; Zhang, Xin. “Sound transmission through double cylindrical shells lined with porous material under turbulent boundary layer excitation.” Journal of Sound and Vibration, v. 357, p. 253-268 (2015). DOI: 10.1016/j.jsv.2015.07.014.","meta":"Journal article · 2015","search_text":"sound transmission through double cylindrical shells lined with porous material under turbulent boundary layer excitation zhou, jie; bhaskar, atul; zhang, xin. “sound transmission through double cylindrical shells lined with porous material under turbulent boundary layer excitation.” journal of sound and vibration, v. 357, p. 253-268 (2015). doi: 10.1016/j.jsv.2015.07.014. journal article · 2015 zhou, jie; bhaskar, atul; zhang, xin 2015 10.1016/j.jsv.2015.07.014 journal of sound and vibration, v. 357, p. 253-268","order":382,"static_url":"/publications/100/"},{"section":"Publications","title":"Single velocity-component modeling of leading edge turbulence interaction noise","url":"/publications/99/","summary":"Gill, J.; Zhang, X.; Joseph, P.. “Single velocity-component modeling of leading edge turbulence interaction noise.” Journal of the Acoustical Society of America, v. 137, (6), p. 3209-3220 (2015). DOI: 10.1121/1.4921547.","meta":"Journal article · 2015","search_text":"single velocity-component modeling of leading edge turbulence interaction noise gill, j.; zhang, x.; joseph, p.. “single velocity-component modeling of leading edge turbulence interaction noise.” journal of the acoustical society of america, v. 137, (6), p. 3209-3220 (2015). doi: 10.1121/1.4921547. journal article · 2015 gill, j.; zhang, x.; joseph, p. 2015 10.1121/1.4921547 journal of the acoustical society of america, v. 137, (6), p. 3209-3220","order":383,"static_url":"/publications/99/"},{"section":"Publications","title":"A fast GPU based bidiagonal solver for computational aeroacoustics","url":"/publications/98/","summary":"Miao, Shuming; Zhang, Xin; Parchment, Oswald G.; Chen, Xiaoxian. “A fast GPU based bidiagonal solver for computational aeroacoustics.” Computer Methods in Applied Mechanics and Engineering, v. 286, p. 22-39 (2015). DOI: 10.1016/j.cma.2014.12.020.","meta":"Journal article · 2015","search_text":"a fast gpu based bidiagonal solver for computational aeroacoustics miao, shuming; zhang, xin; parchment, oswald g.; chen, xiaoxian. “a fast gpu based bidiagonal solver for computational aeroacoustics.” computer methods in applied mechanics and engineering, v. 286, p. 22-39 (2015). doi: 10.1016/j.cma.2014.12.020. journal article · 2015 miao, shuming; zhang, xin; parchment, oswald g.; chen, xiaoxian 2015 10.1016/j.cma.2014.12.020 computer methods in applied mechanics and engineering, v. 286, p. 22-39","order":384,"static_url":"/publications/98/"},{"section":"Publications","title":"Two-dimensional optimisation by iterative learning for flow separation control","url":"/publications/370/","summary":"Cai, Zhonglun; Angland, David; Zhang, Xin; Chen, Peng. “Two-dimensional optimisation by iterative learning for flow separation control.” AIAA AVIATION 2014 -7th AIAA Flow Control Conference, American Institute of Aeronautics and Astronautics Inc., 2014, (2014). DOI: 10.2514/6.20…","meta":"Conference paper · 2014","search_text":"two-dimensional optimisation by iterative learning for flow separation control cai, zhonglun; angland, david; zhang, xin; chen, peng. “two-dimensional optimisation by iterative learning for flow separation control.” aiaa aviation 2014 -7th aiaa flow control conference, american institute of aeronautics and astronautics inc., 2014, (2014). doi: 10.2514/6.2014-2937. conference paper · 2014 cai, zhonglun; angland, david; zhang, xin; chen, peng 2014 10.2514/6.2014-2937 aiaa aviation 2014 -7th aiaa flow control conference, american institute of aeronautics and astronautics inc., 2014,","order":385,"static_url":"/publications/370/"},{"section":"Publications","title":"Reduced dimension modeling of leading edge turbulent interaction noise","url":"/publications/369/","summary":"Gill, James; Zhang, Xin; Joseph, Phillip; Node-Langlois, Thomas. “Reduced dimension modeling of leading edge turbulent interaction noise.” 20th AIAA/CEAS Aeroacoustics Conference, American Institute of Aeronautics and Astronautics Inc., 2014, (2014). DOI: 10.2514/6.2014-2321.","meta":"Conference paper · 2014","search_text":"reduced dimension modeling of leading edge turbulent interaction noise gill, james; zhang, xin; joseph, phillip; node-langlois, thomas. “reduced dimension modeling of leading edge turbulent interaction noise.” 20th aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc., 2014, (2014). doi: 10.2514/6.2014-2321. conference paper · 2014 gill, james; zhang, xin; joseph, phillip; node-langlois, thomas 2014 10.2514/6.2014-2321 20th aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc., 2014,","order":386,"static_url":"/publications/369/"},{"section":"Publications","title":"Prediction of contra-rotating open rotor broadband noise in isolated and installed configurations","url":"/publications/368/","summary":"Nodé-Langlois, T.; Wlassow, F.; Languille, V.; Colin, Y.; Caruelle, B.; Gill, J.; Chen, X.; Zhang, X.; Parry, A. B.. “Prediction of contra-rotating open rotor broadband noise in isolated and installed configurations.” 20th AIAA/CEAS Aeroacoustics Conference, American Institute o…","meta":"Conference paper · 2014","search_text":"prediction of contra-rotating open rotor broadband noise in isolated and installed configurations nodé-langlois, t.; wlassow, f.; languille, v.; colin, y.; caruelle, b.; gill, j.; chen, x.; zhang, x.; parry, a. b.. “prediction of contra-rotating open rotor broadband noise in isolated and installed configurations.” 20th aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc., 2014, (2014). doi: 10.2514/6.2014-2610. conference paper · 2014 nodé-langlois, t.; wlassow, f.; languille, v.; colin, y.; caruelle, b.; gill, j.; chen, x.; zhang, x.; parry, a. b. 2014 10.2514/6.2014-2610 20th aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc., 2014,","order":387,"static_url":"/publications/368/"},{"section":"Publications","title":"Numerical investigation of active flow control using steady blowing for landing gear noise reduction","url":"/publications/367/","summary":"Aubert, Mathias; Stalnov, Oksana; Angland, David; Zhang, Xin. “Numerical investigation of active flow control using steady blowing for landing gear noise reduction.” 20th AIAA/CEAS Aeroacoustics Conference, American Institute of Aeronautics and Astronautics Inc., 2014, (2014). D…","meta":"Conference paper · 2014","search_text":"numerical investigation of active flow control using steady blowing for landing gear noise reduction aubert, mathias; stalnov, oksana; angland, david; zhang, xin. “numerical investigation of active flow control using steady blowing for landing gear noise reduction.” 20th aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc., 2014, (2014). doi: 10.2514/6.2014-2893. conference paper · 2014 aubert, mathias; stalnov, oksana; angland, david; zhang, xin 2014 10.2514/6.2014-2893 20th aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc., 2014,","order":388,"static_url":"/publications/367/"},{"section":"Publications","title":"Gradient term filtering for stable sound propagation with linearized euler equations","url":"/publications/366/","summary":"Zhang, Xin; Chen, Xiaoxian; Gill, James; Huang, Xun. “Gradient term filtering for stable sound propagation with linearized euler equations.” 20th AIAA/CEAS Aeroacoustics Conference, American Institute of Aeronautics and Astronautics Inc., 2014, (2014). DOI: 10.2514/6.2014-3306.","meta":"Conference paper · 2014","search_text":"gradient term filtering for stable sound propagation with linearized euler equations zhang, xin; chen, xiaoxian; gill, james; huang, xun. “gradient term filtering for stable sound propagation with linearized euler equations.” 20th aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc., 2014, (2014). doi: 10.2514/6.2014-3306. conference paper · 2014 zhang, xin; chen, xiaoxian; gill, james; huang, xun 2014 10.2514/6.2014-3306 20th aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc., 2014,","order":389,"static_url":"/publications/366/"},{"section":"Publications","title":"A fast GPU based bidiagonal solver for computational aeroacoustics","url":"/publications/365/","summary":"Miao, Shuming; Zhang, Xin; Parchment, Oswald G.; Chen, Xiaoxian. “A fast GPU based bidiagonal solver for computational aeroacoustics.” 20th AIAA/CEAS Aeroacoustics Conference, American Institute of Aeronautics and Astronautics Inc., 2014, (2014). DOI: 10.2514/6.2014-2317.","meta":"Conference paper · 2014","search_text":"a fast gpu based bidiagonal solver for computational aeroacoustics miao, shuming; zhang, xin; parchment, oswald g.; chen, xiaoxian. “a fast gpu based bidiagonal solver for computational aeroacoustics.” 20th aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc., 2014, (2014). doi: 10.2514/6.2014-2317. conference paper · 2014 miao, shuming; zhang, xin; parchment, oswald g.; chen, xiaoxian 2014 10.2514/6.2014-2317 20th aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc., 2014,","order":390,"static_url":"/publications/365/"},{"section":"Publications","title":"A complex equivalent source method for scattering effect of aircraft noise","url":"/publications/364/","summary":"Hou, Yu; Zhang, Xin; Angland, David. “A complex equivalent source method for scattering effect of aircraft noise.” 20th AIAA/CEAS Aeroacoustics Conference, American Institute of Aeronautics and Astronautics Inc., 2014, (2014). DOI: 10.2514/6.2014-3302.","meta":"Conference paper · 2014","search_text":"a complex equivalent source method for scattering effect of aircraft noise hou, yu; zhang, xin; angland, david. “a complex equivalent source method for scattering effect of aircraft noise.” 20th aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc., 2014, (2014). doi: 10.2514/6.2014-3302. conference paper · 2014 hou, yu; zhang, xin; angland, david 2014 10.2514/6.2014-3302 20th aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc., 2014,","order":391,"static_url":"/publications/364/"},{"section":"Publications","title":"Stability analysis and design of time-domain acoustic impedance boundary conditions for lined duct with mean flow","url":"/publications/97/","summary":"Liu, Xin; Huang, Xun; Zhang, Xin. “Stability analysis and design of time-domain acoustic impedance boundary conditions for lined duct with mean flow.” Journal of the Acoustical Society of America, v. 136, (5), p. 2441-2452 (2014). DOI: 10.1121/1.4896746.","meta":"Journal article · 2014","search_text":"stability analysis and design of time-domain acoustic impedance boundary conditions for lined duct with mean flow liu, xin; huang, xun; zhang, xin. “stability analysis and design of time-domain acoustic impedance boundary conditions for lined duct with mean flow.” journal of the acoustical society of america, v. 136, (5), p. 2441-2452 (2014). doi: 10.1121/1.4896746. journal article · 2014 liu, xin; huang, xun; zhang, xin 2014 10.1121/1.4896746 journal of the acoustical society of america, v. 136, (5), p. 2441-2452","order":392,"static_url":"/publications/97/"},{"section":"Publications","title":"Broadband wave propagation from an aeroengine duct","url":"/publications/96/","summary":"Zhang, X.; Chen, X. X.. “Broadband wave propagation from an aeroengine duct.” AIAA Journal, v. 52, (1), p. 43-51 (2014). DOI: 10.2514/1.j052285.","meta":"Journal article · 2014","search_text":"broadband wave propagation from an aeroengine duct zhang, x.; chen, x. x.. “broadband wave propagation from an aeroengine duct.” aiaa journal, v. 52, (1), p. 43-51 (2014). doi: 10.2514/1.j052285. journal article · 2014 zhang, x.; chen, x. x. 2014 10.2514/1.j052285 aiaa journal, v. 52, (1), p. 43-51","order":393,"static_url":"/publications/96/"},{"section":"Publications","title":"Experimental study of noise emitted by circular cylinders with large roughness","url":"/publications/94/","summary":"Alomar, Antoni; Angland, David; Zhang, Xin; Molin, Nicolas. “Experimental study of noise emitted by circular cylinders with large roughness.” Journal of Sound and Vibration, v. 333, (24), p. 6474-6497 (2014). DOI: 10.1016/j.jsv.2014.07.013.","meta":"Journal article · 2014","search_text":"experimental study of noise emitted by circular cylinders with large roughness alomar, antoni; angland, david; zhang, xin; molin, nicolas. “experimental study of noise emitted by circular cylinders with large roughness.” journal of sound and vibration, v. 333, (24), p. 6474-6497 (2014). doi: 10.1016/j.jsv.2014.07.013. journal article · 2014 alomar, antoni; angland, david; zhang, xin; molin, nicolas 2014 10.1016/j.jsv.2014.07.013 journal of sound and vibration, v. 333, (24), p. 6474-6497","order":394,"static_url":"/publications/94/"},{"section":"Publications","title":"The effect of external mean flow on sound transmission through double-walled cylindrical shells lined with poroelastic material","url":"/publications/93/","summary":"Zhou, Jie; Bhaskar, Atul; Zhang, Xin. “The effect of external mean flow on sound transmission through double-walled cylindrical shells lined with poroelastic material.” Journal of Sound and Vibration, v. 333, (7), p. 1972-1990 (2014). DOI: 10.1016/j.jsv.2013.11.038.","meta":"Journal article · 2014","search_text":"the effect of external mean flow on sound transmission through double-walled cylindrical shells lined with poroelastic material zhou, jie; bhaskar, atul; zhang, xin. “the effect of external mean flow on sound transmission through double-walled cylindrical shells lined with poroelastic material.” journal of sound and vibration, v. 333, (7), p. 1972-1990 (2014). doi: 10.1016/j.jsv.2013.11.038. journal article · 2014 zhou, jie; bhaskar, atul; zhang, xin 2014 10.1016/j.jsv.2013.11.038 journal of sound and vibration, v. 333, (7), p. 1972-1990","order":395,"static_url":"/publications/93/"},{"section":"Publications","title":"Active flow separation control by a position-based iterative learning control algorithm with experimental validation","url":"/publications/92/","summary":"Cai, Zhonglun; Chen, Peng; Angland, David; Zhang, Xin. “Active flow separation control by a position-based iterative learning control algorithm with experimental validation.” International Journal of Control, v. 87, (3), p. 633-641 (2014). DOI: 10.1080/00207179.2013.852251.","meta":"Journal article · 2014","search_text":"active flow separation control by a position-based iterative learning control algorithm with experimental validation cai, zhonglun; chen, peng; angland, david; zhang, xin. “active flow separation control by a position-based iterative learning control algorithm with experimental validation.” international journal of control, v. 87, (3), p. 633-641 (2014). doi: 10.1080/00207179.2013.852251. journal article · 2014 cai, zhonglun; chen, peng; angland, david; zhang, xin 2014 10.1080/00207179.2013.852251 international journal of control, v. 87, (3), p. 633-641","order":396,"static_url":"/publications/92/"},{"section":"Publications","title":"On the contribution of individual components to landing gear loads and noise","url":"/publications/376/","summary":"Stalnov, Oksana; Windiate, Sarah; Angland, David; Zhang, Xin; Ashworth, Richard. “On the contribution of individual components to landing gear loads and noise.” Paper presented at 31st AIAA Applied Aerodynamics Conference, San Diego, CA, United States (2013). DOI: 10.2514/6.2013…","meta":"Conference paper · 2013","search_text":"on the contribution of individual components to landing gear loads and noise stalnov, oksana; windiate, sarah; angland, david; zhang, xin; ashworth, richard. “on the contribution of individual components to landing gear loads and noise.” paper presented at 31st aiaa applied aerodynamics conference, san diego, ca, united states (2013). doi: 10.2514/6.2013-3153. conference paper · 2013 stalnov, oksana; windiate, sarah; angland, david; zhang, xin; ashworth, richard 2013 10.2514/6.2013-3153 paper presented at 31st aiaa applied aerodynamics conference, san diego, ca, united states","order":397,"static_url":"/publications/376/"},{"section":"Publications","title":"Installation effects of landing gears","url":"/publications/375/","summary":"Angland, D.; Zhang, X.. “Installation effects of landing gears.” 19th AIAA/CEAS Aeroacoustics Conference, American Institute of Aeronautics and Astronautics Inc., 2013, p. 134 (2013). DOI: 10.2514/6.2013-2138.","meta":"Conference paper · 2013","search_text":"installation effects of landing gears angland, d.; zhang, x.. “installation effects of landing gears.” 19th aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc., 2013, p. 134 (2013). doi: 10.2514/6.2013-2138. conference paper · 2013 angland, d.; zhang, x. 2013 10.2514/6.2013-2138 19th aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc., 2013, p. 134","order":398,"static_url":"/publications/375/"},{"section":"Publications","title":"Effects of real airfoil geometry on leading edge gust interaction noise","url":"/publications/374/","summary":"Gill, James; Zhang, Xin; Joseph, Phillip; Node-Langlois, Thomas. “Effects of real airfoil geometry on leading edge gust interaction noise.” 19th AIAA/CEAS Aeroacoustics Conference, 2013, p. 195 (2013). DOI: 10.2514/6.2013-2203.","meta":"Conference paper · 2013","search_text":"effects of real airfoil geometry on leading edge gust interaction noise gill, james; zhang, xin; joseph, phillip; node-langlois, thomas. “effects of real airfoil geometry on leading edge gust interaction noise.” 19th aiaa/ceas aeroacoustics conference, 2013, p. 195 (2013). doi: 10.2514/6.2013-2203. conference paper · 2013 gill, james; zhang, xin; joseph, phillip; node-langlois, thomas 2013 10.2514/6.2013-2203 19th aiaa/ceas aeroacoustics conference, 2013, p. 195","order":399,"static_url":"/publications/374/"},{"section":"Publications","title":"Aerodynamic and aeroacoustic measurements of a landing gear torque link","url":"/publications/373/","summary":"Windiate, Sarah; Stalnov, Oksana; Angland, David; Zhang, Xin; Ashworth, Richard. “Aerodynamic and aeroacoustic measurements of a landing gear torque link.” Paper presented at 31st AIAA Applied Aerodynamics Conference, San Diego, CA, United States (2013). DOI: 10.2514/6.2013-2537.","meta":"Conference paper · 2013","search_text":"aerodynamic and aeroacoustic measurements of a landing gear torque link windiate, sarah; stalnov, oksana; angland, david; zhang, xin; ashworth, richard. “aerodynamic and aeroacoustic measurements of a landing gear torque link.” paper presented at 31st aiaa applied aerodynamics conference, san diego, ca, united states (2013). doi: 10.2514/6.2013-2537. conference paper · 2013 windiate, sarah; stalnov, oksana; angland, david; zhang, xin; ashworth, richard 2013 10.2514/6.2013-2537 paper presented at 31st aiaa applied aerodynamics conference, san diego, ca, united states","order":400,"static_url":"/publications/373/"},{"section":"Publications","title":"Aerodynamic and acoustic measurements of a single landing gear wheel","url":"/publications/372/","summary":"Zhang, Xin; Ma, Zhaokai; Smith, Malcolm; Sanderson, Michael; Bissessur, Prithiraj. “Aerodynamic and acoustic measurements of a single landing gear wheel.” 19th AIAA/CEAS Aeroacoustics Conference, 2013, p. 155 (2013). DOI: 10.2514/6.2013-2160.","meta":"Conference paper · 2013","search_text":"aerodynamic and acoustic measurements of a single landing gear wheel zhang, xin; ma, zhaokai; smith, malcolm; sanderson, michael; bissessur, prithiraj. “aerodynamic and acoustic measurements of a single landing gear wheel.” 19th aiaa/ceas aeroacoustics conference, 2013, p. 155 (2013). doi: 10.2514/6.2013-2160. conference paper · 2013 zhang, xin; ma, zhaokai; smith, malcolm; sanderson, michael; bissessur, prithiraj 2013 10.2514/6.2013-2160 19th aiaa/ceas aeroacoustics conference, 2013, p. 155","order":401,"static_url":"/publications/372/"},{"section":"Publications","title":"A position based iterative learning control applied to active flow control","url":"/publications/371/","summary":"Cai, Zhonglun; Chen, Peng; Angland, David; Zhang, Xin. “A position based iterative learning control applied to active flow control.” 2013 American Control Conference, ACC 2013, 2013, p. 5177-5182article number 6580643 (2013). DOI: 10.1109/acc.2013.6580643.","meta":"Conference paper · 2013","search_text":"a position based iterative learning control applied to active flow control cai, zhonglun; chen, peng; angland, david; zhang, xin. “a position based iterative learning control applied to active flow control.” 2013 american control conference, acc 2013, 2013, p. 5177-5182article number 6580643 (2013). doi: 10.1109/acc.2013.6580643. conference paper · 2013 cai, zhonglun; chen, peng; angland, david; zhang, xin 2013 10.1109/acc.2013.6580643 2013 american control conference, acc 2013, 2013, p. 5177-5182article number 6580643","order":402,"static_url":"/publications/371/"},{"section":"Publications","title":"Symmetric airfoil geometry effects on leading edge noise","url":"/publications/91/","summary":"Gill, James; Zhang, X.; Joseph, P.. “Symmetric airfoil geometry effects on leading edge noise.” Journal of the Acoustical Society of America, v. 134, (4), p. 2669-2680 (2013). DOI: 10.1121/1.4818769.","meta":"Journal article · 2013","search_text":"symmetric airfoil geometry effects on leading edge noise gill, james; zhang, x.; joseph, p.. “symmetric airfoil geometry effects on leading edge noise.” journal of the acoustical society of america, v. 134, (4), p. 2669-2680 (2013). doi: 10.1121/1.4818769. journal article · 2013 gill, james; zhang, x.; joseph, p. 2013 10.1121/1.4818769 journal of the acoustical society of america, v. 134, (4), p. 2669-2680","order":403,"static_url":"/publications/91/"},{"section":"Publications","title":"Aeroacoustic effects of high-lift wing slat track and cut-out system","url":"/publications/90/","summary":"Wang, Xin; Hu, Zhiwei; Zhang, Xin. “Aeroacoustic effects of high-lift wing slat track and cut-out system.” International Journal of Aeroacoustics, v. 12, (3), p. 283-308 (2013). DOI: 10.1260/1475-472x.12.3.283.","meta":"Journal article · 2013","search_text":"aeroacoustic effects of high-lift wing slat track and cut-out system wang, xin; hu, zhiwei; zhang, xin. “aeroacoustic effects of high-lift wing slat track and cut-out system.” international journal of aeroacoustics, v. 12, (3), p. 283-308 (2013). doi: 10.1260/1475-472x.12.3.283. journal article · 2013 wang, xin; hu, zhiwei; zhang, xin 2013 10.1260/1475-472x.12.3.283 international journal of aeroacoustics, v. 12, (3), p. 283-308","order":404,"static_url":"/publications/90/"},{"section":"Publications","title":"Optimization for sound transmission through a double-wall panel","url":"/publications/89/","summary":"Zhou, Jie; Bhaskar, Atul; Zhang, Xin. “Optimization for sound transmission through a double-wall panel.” Applied Acoustics, v. 74, (12), p. 1422-1428 (2013). DOI: 10.1016/j.apacoust.2013.06.002.","meta":"Journal article · 2013","search_text":"optimization for sound transmission through a double-wall panel zhou, jie; bhaskar, atul; zhang, xin. “optimization for sound transmission through a double-wall panel.” applied acoustics, v. 74, (12), p. 1422-1428 (2013). doi: 10.1016/j.apacoust.2013.06.002. journal article · 2013 zhou, jie; bhaskar, atul; zhang, xin 2013 10.1016/j.apacoust.2013.06.002 applied acoustics, v. 74, (12), p. 1422-1428","order":405,"static_url":"/publications/89/"},{"section":"Publications","title":"Attenuation of noise from an airfoil equipped with a high-lift device using plasma actuators","url":"/publications/88/","summary":"Angland, D.; Cai, Z.; Chappell, S.; Chen, P.; Zhang, Xin. “Attenuation of noise from an airfoil equipped with a high-lift device using plasma actuators.” ERCOFTAC Bulletin, v. 94, p. 65-69 (2013).","meta":"Journal article · 2013","search_text":"attenuation of noise from an airfoil equipped with a high-lift device using plasma actuators angland, d.; cai, z.; chappell, s.; chen, p.; zhang, xin. “attenuation of noise from an airfoil equipped with a high-lift device using plasma actuators.” ercoftac bulletin, v. 94, p. 65-69 (2013). journal article · 2013 angland, d.; cai, z.; chappell, s.; chen, p.; zhang, xin 2013 ercoftac bulletin, v. 94, p. 65-69","order":406,"static_url":"/publications/88/"},{"section":"Publications","title":"Landing-gear noise prediction using high-order finite difference schemes","url":"/publications/87/","summary":"Liu, Wen; Wook Kim, Jae; Zhang, Xin; Angland, David; Caruelle, Bastien. “Landing-gear noise prediction using high-order finite difference schemes.” Journal of Sound and Vibration, v. 332, (14), p. 3517-3534 (2013). DOI: 10.1016/j.jsv.2013.01.035.","meta":"Journal article · 2013","search_text":"landing-gear noise prediction using high-order finite difference schemes liu, wen; wook kim, jae; zhang, xin; angland, david; caruelle, bastien. “landing-gear noise prediction using high-order finite difference schemes.” journal of sound and vibration, v. 332, (14), p. 3517-3534 (2013). doi: 10.1016/j.jsv.2013.01.035. journal article · 2013 liu, wen; wook kim, jae; zhang, xin; angland, david; caruelle, bastien 2013 10.1016/j.jsv.2013.01.035 journal of sound and vibration, v. 332, (14), p. 3517-3534","order":407,"static_url":"/publications/87/"},{"section":"Publications","title":"Sound transmission through a double-panel construction lined with poroelastic material in the presence of mean flow","url":"/publications/86/","summary":"Zhou, Jie; Bhaskar, Atul; Zhang, Xin. “Sound transmission through a double-panel construction lined with poroelastic material in the presence of mean flow.” Journal of Sound and Vibration, v. 332, (16), p. 3724-3734 (2013). DOI: 10.1016/j.jsv.2013.02.020.","meta":"Journal article · 2013","search_text":"sound transmission through a double-panel construction lined with poroelastic material in the presence of mean flow zhou, jie; bhaskar, atul; zhang, xin. “sound transmission through a double-panel construction lined with poroelastic material in the presence of mean flow.” journal of sound and vibration, v. 332, (16), p. 3724-3734 (2013). doi: 10.1016/j.jsv.2013.02.020. journal article · 2013 zhou, jie; bhaskar, atul; zhang, xin 2013 10.1016/j.jsv.2013.02.020 journal of sound and vibration, v. 332, (16), p. 3724-3734","order":408,"static_url":"/publications/86/"},{"section":"Publications","title":"High-order interface for aeroacoustic computation using overset grid","url":"/publications/85/","summary":"Chen, X. X.; Zhang, X.. “High-order interface for aeroacoustic computation using overset grid.” AIAA Journal, v. 51, (2), p. 519-523 (2013). DOI: 10.2514/1.j051810.","meta":"Journal article · 2013","search_text":"high-order interface for aeroacoustic computation using overset grid chen, x. x.; zhang, x.. “high-order interface for aeroacoustic computation using overset grid.” aiaa journal, v. 51, (2), p. 519-523 (2013). doi: 10.2514/1.j051810. journal article · 2013 chen, x. x.; zhang, x. 2013 10.2514/1.j051810 aiaa journal, v. 51, (2), p. 519-523","order":409,"static_url":"/publications/85/"},{"section":"Publications","title":"Sound transmission through laminated composite doublewall panel lined with poroelastic material","url":"/publications/381/","summary":"Zhou, J.; Bhaskar, A.; Zhang, X.. “Sound transmission through laminated composite doublewall panel lined with poroelastic material.” International Conference on Noise and Vibration Engineering 2012, ISMA 2012, including USD 2012, Katholieke Universiteit Leuven, 2012, p. 1933-194…","meta":"Conference paper · 2012","search_text":"sound transmission through laminated composite doublewall panel lined with poroelastic material zhou, j.; bhaskar, a.; zhang, x.. “sound transmission through laminated composite doublewall panel lined with poroelastic material.” international conference on noise and vibration engineering 2012, isma 2012, including usd 2012, katholieke universiteit leuven, 2012, p. 1933-1941 (2012). conference paper · 2012 zhou, j.; bhaskar, a.; zhang, x. 2012 international conference on noise and vibration engineering 2012, isma 2012, including usd 2012, katholieke universiteit leuven, 2012, p. 1933-1941","order":410,"static_url":"/publications/381/"},{"section":"Publications","title":"Slat noise feedback control with a dielectric barrier discharge plasma actuator","url":"/publications/380/","summary":"Chappell, S.; Cai, Z.; Zhang, X.; Angland, D.. “Slat noise feedback control with a dielectric barrier discharge plasma actuator.” 6th AIAA Flow Control Conference 2012, American Institute of Aeronautics and Astronautics Inc., 2012, (2012). DOI: 10.2514/6.2012-2806.","meta":"Conference paper · 2012","search_text":"slat noise feedback control with a dielectric barrier discharge plasma actuator chappell, s.; cai, z.; zhang, x.; angland, d.. “slat noise feedback control with a dielectric barrier discharge plasma actuator.” 6th aiaa flow control conference 2012, american institute of aeronautics and astronautics inc., 2012, (2012). doi: 10.2514/6.2012-2806. conference paper · 2012 chappell, s.; cai, z.; zhang, x.; angland, d. 2012 10.2514/6.2012-2806 6th aiaa flow control conference 2012, american institute of aeronautics and astronautics inc., 2012,","order":411,"static_url":"/publications/380/"},{"section":"Publications","title":"Simulation of a generic two-wheel nose landing gear using high-order finite difference schemes","url":"/publications/379/","summary":"Liu, Wen; Kim, Jae Wook; Zhang, Xin; Caruelle, Bastien. “Simulation of a generic two-wheel nose landing gear using high-order finite difference schemes.” 18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference), 2012, (2012). DOI: 10.2514/6.2012-2278.","meta":"Conference paper · 2012","search_text":"simulation of a generic two-wheel nose landing gear using high-order finite difference schemes liu, wen; kim, jae wook; zhang, xin; caruelle, bastien. “simulation of a generic two-wheel nose landing gear using high-order finite difference schemes.” 18th aiaa/ceas aeroacoustics conference (33rd aiaa aeroacoustics conference), 2012, (2012). doi: 10.2514/6.2012-2278. conference paper · 2012 liu, wen; kim, jae wook; zhang, xin; caruelle, bastien 2012 10.2514/6.2012-2278 18th aiaa/ceas aeroacoustics conference (33rd aiaa aeroacoustics conference), 2012,","order":412,"static_url":"/publications/379/"},{"section":"Publications","title":"Large-eddy simulation of the interaction of a jet with a wing","url":"/publications/378/","summary":"Bondarenko, Maksym; Hu, Zhiwei; Zhang, Xin. “Large-eddy simulation of the interaction of a jet with a wing.” 18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference), 2012, (2012). DOI: 10.2514/6.2012-2254.","meta":"Conference paper · 2012","search_text":"large-eddy simulation of the interaction of a jet with a wing bondarenko, maksym; hu, zhiwei; zhang, xin. “large-eddy simulation of the interaction of a jet with a wing.” 18th aiaa/ceas aeroacoustics conference (33rd aiaa aeroacoustics conference), 2012, (2012). doi: 10.2514/6.2012-2254. conference paper · 2012 bondarenko, maksym; hu, zhiwei; zhang, xin 2012 10.2514/6.2012-2254 18th aiaa/ceas aeroacoustics conference (33rd aiaa aeroacoustics conference), 2012,","order":413,"static_url":"/publications/378/"},{"section":"Publications","title":"A Numerical study to optimise blowing flow control for flap side-edge noise reduction","url":"/publications/377/","summary":"Kanjere, Kondwani; Angland, David; Zhang, Xin. “A Numerical study to optimise blowing flow control for flap side-edge noise reduction.” 18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference), American Institute of Aeronautics and Astronautics Inc., 2012, (2…","meta":"Conference paper · 2012","search_text":"a numerical study to optimise blowing flow control for flap side-edge noise reduction kanjere, kondwani; angland, david; zhang, xin. “a numerical study to optimise blowing flow control for flap side-edge noise reduction.” 18th aiaa/ceas aeroacoustics conference (33rd aiaa aeroacoustics conference), american institute of aeronautics and astronautics inc., 2012, (2012). doi: 10.2514/6.2012-2097. conference paper · 2012 kanjere, kondwani; angland, david; zhang, xin 2012 10.2514/6.2012-2097 18th aiaa/ceas aeroacoustics conference (33rd aiaa aeroacoustics conference), american institute of aeronautics and astronautics inc., 2012,","order":414,"static_url":"/publications/377/"},{"section":"Publications","title":"Use of blowing flow control to reduce bluff body interaction noise","url":"/publications/84/","summary":"Angland, D.; Zhang, X.; Goodyer, M.. “Use of blowing flow control to reduce bluff body interaction noise.” AIAA Journal, v. 50, (8), p. 1670-1684 (2012). DOI: 10.2514/1.j051074.","meta":"Journal article · 2012","search_text":"use of blowing flow control to reduce bluff body interaction noise angland, d.; zhang, x.; goodyer, m.. “use of blowing flow control to reduce bluff body interaction noise.” aiaa journal, v. 50, (8), p. 1670-1684 (2012). doi: 10.2514/1.j051074. journal article · 2012 angland, d.; zhang, x.; goodyer, m. 2012 10.2514/1.j051074 aiaa journal, v. 50, (8), p. 1670-1684","order":415,"static_url":"/publications/84/"},{"section":"Publications","title":"Aircraft noise and its nearfield propagation computations","url":"/publications/83/","summary":"Zhang, Xin. “Aircraft noise and its nearfield propagation computations.” Acta Mechanica Sinica/Lixue Xuebao, v. 28, (4), p. 960-977 (2012). DOI: 10.1007/s10409-012-0136-1.","meta":"Journal article · 2012","search_text":"aircraft noise and its nearfield propagation computations zhang, xin. “aircraft noise and its nearfield propagation computations.” acta mechanica sinica/lixue xuebao, v. 28, (4), p. 960-977 (2012). doi: 10.1007/s10409-012-0136-1. journal article · 2012 zhang, xin 2012 10.1007/s10409-012-0136-1 acta mechanica sinica/lixue xuebao, v. 28, (4), p. 960-977","order":416,"static_url":"/publications/83/"},{"section":"Publications","title":"Measurement and control of aircraft landing gear broadband noise","url":"/publications/75/","summary":"Li, Yong; Smith, Malcolm; Zhang, Xin. “Measurement and control of aircraft landing gear broadband noise.” Aerospace Science and Technology, v. 23, (1), p. 213-223 (2012). DOI: 10.1016/j.ast.2011.07.009.","meta":"Journal article · 2012","search_text":"measurement and control of aircraft landing gear broadband noise li, yong; smith, malcolm; zhang, xin. “measurement and control of aircraft landing gear broadband noise.” aerospace science and technology, v. 23, (1), p. 213-223 (2012). doi: 10.1016/j.ast.2011.07.009. journal article · 2012 li, yong; smith, malcolm; zhang, xin 2012 10.1016/j.ast.2011.07.009 aerospace science and technology, v. 23, (1), p. 213-223","order":417,"static_url":"/publications/75/"},{"section":"Publications","title":"Slat Noise Reduction using Leading Edge Strips","url":"/publications/386/","summary":"Chen, Peng; Zhang, Xin; Angland, David. “Slat Noise Reduction using Leading Edge Strips.” 17th AIAA/CEAS Aeroacoustics Conference 2011 (32nd AIAA Aeroacoustics Conference), 2011, (2011). DOI: 10.2514/6.2011-2908.","meta":"Conference paper · 2011","search_text":"slat noise reduction using leading edge strips chen, peng; zhang, xin; angland, david. “slat noise reduction using leading edge strips.” 17th aiaa/ceas aeroacoustics conference 2011 (32nd aiaa aeroacoustics conference), 2011, (2011). doi: 10.2514/6.2011-2908. conference paper · 2011 chen, peng; zhang, xin; angland, david 2011 10.2514/6.2011-2908 17th aiaa/ceas aeroacoustics conference 2011 (32nd aiaa aeroacoustics conference), 2011,","order":418,"static_url":"/publications/386/"},{"section":"Publications","title":"Linearised divergence equations for sound propagation","url":"/publications/385/","summary":"Zhang, Xin; Chen, Xiao Xian. “Linearised divergence equations for sound propagation.” 17th AIAA/CEAS Aeroacoustics Conference 2011 (32nd AIAA Aeroacoustics Conference), American Institute of Aeronautics and Astronautics Inc., 2011, (2011). DOI: 10.2514/6.2011-2930.","meta":"Conference paper · 2011","search_text":"linearised divergence equations for sound propagation zhang, xin; chen, xiao xian. “linearised divergence equations for sound propagation.” 17th aiaa/ceas aeroacoustics conference 2011 (32nd aiaa aeroacoustics conference), american institute of aeronautics and astronautics inc., 2011, (2011). doi: 10.2514/6.2011-2930. conference paper · 2011 zhang, xin; chen, xiao xian 2011 10.2514/6.2011-2930 17th aiaa/ceas aeroacoustics conference 2011 (32nd aiaa aeroacoustics conference), american institute of aeronautics and astronautics inc., 2011,","order":419,"static_url":"/publications/385/"},{"section":"Publications","title":"Dielectric barrier discharge based jet actuator for flow control","url":"/publications/384/","summary":"Luo, Xinfu; Zhang, Xin. “Dielectric barrier discharge based jet actuator for flow control.” 41st AIAA Fluid Dynamics Conference and Exhibit, American Institute of Aeronautics and Astronautics Inc., 2011, (2011). DOI: 10.2514/6.2011-3988.","meta":"Conference paper · 2011","search_text":"dielectric barrier discharge based jet actuator for flow control luo, xinfu; zhang, xin. “dielectric barrier discharge based jet actuator for flow control.” 41st aiaa fluid dynamics conference and exhibit, american institute of aeronautics and astronautics inc., 2011, (2011). doi: 10.2514/6.2011-3988. conference paper · 2011 luo, xinfu; zhang, xin 2011 10.2514/6.2011-3988 41st aiaa fluid dynamics conference and exhibit, american institute of aeronautics and astronautics inc., 2011,","order":420,"static_url":"/publications/384/"},{"section":"Publications","title":"Airfoil flow control usiug plasma actuation and coauda effect","url":"/publications/383/","summary":"Zhang, Xin; Luo, Xinfu; Chen, Peng. “Airfoil flow control usiug plasma actuation and coauda effect.” 29th AIAA Applied Aerodynamics Conference 2011, American Institute of Aeronautics and Astronautics Inc., 2011, (2011). DOI: 10.2514/6.2011-3516.","meta":"Conference paper · 2011","search_text":"airfoil flow control usiug plasma actuation and coauda effect zhang, xin; luo, xinfu; chen, peng. “airfoil flow control usiug plasma actuation and coauda effect.” 29th aiaa applied aerodynamics conference 2011, american institute of aeronautics and astronautics inc., 2011, (2011). doi: 10.2514/6.2011-3516. conference paper · 2011 zhang, xin; luo, xinfu; chen, peng 2011 10.2514/6.2011-3516 29th aiaa applied aerodynamics conference 2011, american institute of aeronautics and astronautics inc., 2011,","order":421,"static_url":"/publications/383/"},{"section":"Publications","title":"Large-scale vortex generation modeling","url":"/publications/382/","summary":"Booker, Christopher D.; Zhang, Xin; Chernyshenko, Sergei I.. “Large-scale vortex generation modeling.” Journal of Fluids Engineering, Transactions of the ASME, v. 133, (12), article number 121201 (2011). DOI: 10.1115/1.4005314.","meta":"Journal article · 2011","search_text":"large-scale vortex generation modeling booker, christopher d.; zhang, xin; chernyshenko, sergei i.. “large-scale vortex generation modeling.” journal of fluids engineering, transactions of the asme, v. 133, (12), article number 121201 (2011). doi: 10.1115/1.4005314. journal article · 2011 booker, christopher d.; zhang, xin; chernyshenko, sergei i. 2011 10.1115/1.4005314 journal of fluids engineering, transactions of the asme, v. 133, (12), article number 121201","order":422,"static_url":"/publications/382/"},{"section":"Publications","title":"Aerodynamics of a heaving airfoil in ground effect","url":"/publications/82/","summary":"Molina, Juan; Zhang, Xin. “Aerodynamics of a heaving airfoil in ground effect.” AIAA Journal, v. 49, (6), p. 1168-1179 (2011). DOI: 10.2514/1.j050369.","meta":"Journal article · 2011","search_text":"aerodynamics of a heaving airfoil in ground effect molina, juan; zhang, xin. “aerodynamics of a heaving airfoil in ground effect.” aiaa journal, v. 49, (6), p. 1168-1179 (2011). doi: 10.2514/1.j050369. journal article · 2011 molina, juan; zhang, xin 2011 10.2514/1.j050369 aiaa journal, v. 49, (6), p. 1168-1179","order":423,"static_url":"/publications/82/"},{"section":"Publications","title":"On the unsteady motion and stability of a heaving airfoil in ground effect","url":"/publications/81/","summary":"Molina, Juan; Zhang, Xin; Angland, David. “On the unsteady motion and stability of a heaving airfoil in ground effect.” Acta Mechanica Sinica/Lixue Xuebao, v. 27, (2), p. 164-178 (2011). DOI: 10.1007/s10409-011-0445-9.","meta":"Journal article · 2011","search_text":"on the unsteady motion and stability of a heaving airfoil in ground effect molina, juan; zhang, xin; angland, david. “on the unsteady motion and stability of a heaving airfoil in ground effect.” acta mechanica sinica/lixue xuebao, v. 27, (2), p. 164-178 (2011). doi: 10.1007/s10409-011-0445-9. journal article · 2011 molina, juan; zhang, xin; angland, david 2011 10.1007/s10409-011-0445-9 acta mechanica sinica/lixue xuebao, v. 27, (2), p. 164-178","order":424,"static_url":"/publications/81/"},{"section":"Publications","title":"Multifidelity surrogate modeling of experimental and computational aerodynamic data sets","url":"/publications/78/","summary":"Kuya, Yuichi; Takeda, Kenji; Zhang, Xin; Forrester, Alexander I.J.. “Multifidelity surrogate modeling of experimental and computational aerodynamic data sets.” AIAA Journal, v. 49, (2), p. 289-298 (2011). DOI: 10.2514/1.j050384.","meta":"Journal article · 2011","search_text":"multifidelity surrogate modeling of experimental and computational aerodynamic data sets kuya, yuichi; takeda, kenji; zhang, xin; forrester, alexander i.j.. “multifidelity surrogate modeling of experimental and computational aerodynamic data sets.” aiaa journal, v. 49, (2), p. 289-298 (2011). doi: 10.2514/1.j050384. journal article · 2011 kuya, yuichi; takeda, kenji; zhang, xin; forrester, alexander i.j. 2011 10.2514/1.j050384 aiaa journal, v. 49, (2), p. 289-298","order":425,"static_url":"/publications/78/"},{"section":"Publications","title":"Time-domain broadband liner optimization","url":"/publications/394/","summary":"Chen, Xiaoxian; Zhang, Xin. “Time-domain broadband liner optimization.” 16th AIAA/CEAS Aeroacoustics Conference (31st AIAA Aeroacoustics Conference), 2010, article number 2010-3719 (2010). DOI: 10.2514/6.2010-3719.","meta":"Conference paper · 2010","search_text":"time-domain broadband liner optimization chen, xiaoxian; zhang, xin. “time-domain broadband liner optimization.” 16th aiaa/ceas aeroacoustics conference (31st aiaa aeroacoustics conference), 2010, article number 2010-3719 (2010). doi: 10.2514/6.2010-3719. conference paper · 2010 chen, xiaoxian; zhang, xin 2010 10.2514/6.2010-3719 16th aiaa/ceas aeroacoustics conference (31st aiaa aeroacoustics conference), 2010, article number 2010-3719","order":426,"static_url":"/publications/394/"},{"section":"Publications","title":"The use of blowing flow control to reduce bluff body interaction noise","url":"/publications/393/","summary":"Angland, D.; Zhang, X.; Goodyer, M.. “The use of blowing flow control to reduce bluff body interaction noise.” 16th AIAA/CEAS Aeroacoustics Conference (31st AIAA Aeroacoustics Conference), American Institute of Aeronautics and Astronautics Inc., 2010, article number 2010-3786 (2…","meta":"Conference paper · 2010","search_text":"the use of blowing flow control to reduce bluff body interaction noise angland, d.; zhang, x.; goodyer, m.. “the use of blowing flow control to reduce bluff body interaction noise.” 16th aiaa/ceas aeroacoustics conference (31st aiaa aeroacoustics conference), american institute of aeronautics and astronautics inc., 2010, article number 2010-3786 (2010). doi: 10.2514/6.2010-3786. conference paper · 2010 angland, d.; zhang, x.; goodyer, m. 2010 10.2514/6.2010-3786 16th aiaa/ceas aeroacoustics conference (31st aiaa aeroacoustics conference), american institute of aeronautics and astronautics inc., 2010, article number 2010-3786","order":427,"static_url":"/publications/393/"},{"section":"Publications","title":"Detached-eddy simulation of a double-element wing in ground effect","url":"/publications/392/","summary":"Heyder-Bruckner, Jacques; Zhang, Xin. “Detached-eddy simulation of a double-element wing in ground effect.” 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, American Institute of Aeronautics and Astronautics Inc., 2010, article numb…","meta":"Conference paper · 2010","search_text":"detached-eddy simulation of a double-element wing in ground effect heyder-bruckner, jacques; zhang, xin. “detached-eddy simulation of a double-element wing in ground effect.” 48th aiaa aerospace sciences meeting including the new horizons forum and aerospace exposition, american institute of aeronautics and astronautics inc., 2010, article number 2010-0059 (2010). doi: 10.2514/6.2010-59. conference paper · 2010 heyder-bruckner, jacques; zhang, xin 2010 10.2514/6.2010-59 48th aiaa aerospace sciences meeting including the new horizons forum and aerospace exposition, american institute of aeronautics and astronautics inc., 2010, article number 2010-0059","order":428,"static_url":"/publications/392/"},{"section":"Publications","title":"Aerodynamics of an oscillating wing in ground effect","url":"/publications/391/","summary":"Molina, Juan; Zhang, Xin. “Aerodynamics of an oscillating wing in ground effect.” 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, American Institute of Aeronautics and Astronautics Inc., 2010, article number 2010-0318 (2010). DOI: …","meta":"Conference paper · 2010","search_text":"aerodynamics of an oscillating wing in ground effect molina, juan; zhang, xin. “aerodynamics of an oscillating wing in ground effect.” 48th aiaa aerospace sciences meeting including the new horizons forum and aerospace exposition, american institute of aeronautics and astronautics inc., 2010, article number 2010-0318 (2010). doi: 10.2514/6.2010-318. conference paper · 2010 molina, juan; zhang, xin 2010 10.2514/6.2010-318 48th aiaa aerospace sciences meeting including the new horizons forum and aerospace exposition, american institute of aeronautics and astronautics inc., 2010, article number 2010-0318","order":429,"static_url":"/publications/391/"},{"section":"Publications","title":"Aeroacoustic investigation of deployed spoiler during steep approach landing","url":"/publications/390/","summary":"Kanjere, Kondwani; Zhang, Xin; Hu, Zhiwei; Angland, David. “Aeroacoustic investigation of deployed spoiler during steep approach landing.” 16th AIAA/CEAS Aeroacoustics Conference (31st AIAA Aeroacoustics Conference), American Institute of Aeronautics and Astronautics Inc., 2010,…","meta":"Conference paper · 2010","search_text":"aeroacoustic investigation of deployed spoiler during steep approach landing kanjere, kondwani; zhang, xin; hu, zhiwei; angland, david. “aeroacoustic investigation of deployed spoiler during steep approach landing.” 16th aiaa/ceas aeroacoustics conference (31st aiaa aeroacoustics conference), american institute of aeronautics and astronautics inc., 2010, article number 2010-3992 (2010). doi: 10.2514/6.2010-3992. conference paper · 2010 kanjere, kondwani; zhang, xin; hu, zhiwei; angland, david 2010 10.2514/6.2010-3992 16th aiaa/ceas aeroacoustics conference (31st aiaa aeroacoustics conference), american institute of aeronautics and astronautics inc., 2010, article number 2010-3992","order":430,"static_url":"/publications/390/"},{"section":"Publications","title":"“Encyclopedia in Aerospace Engineering” – acoustics and noise","url":"/publications/389/","summary":"Zhang, Xin. ““Encyclopedia in Aerospace Engineering” – acoustics and noise.” Encyclopedia of Aerospace Engineering / wiley, 2010, (2010).","meta":"Book chapter · 2010","search_text":"“encyclopedia in aerospace engineering” – acoustics and noise zhang, xin. ““encyclopedia in aerospace engineering” – acoustics and noise.” encyclopedia of aerospace engineering / wiley, 2010, (2010). book chapter · 2010 zhang, xin 2010 encyclopedia of aerospace engineering / wiley, 2010,","order":431,"static_url":"/publications/389/"},{"section":"Publications","title":"Time-domain computation of multimode propagation in an aeroengine duct","url":"/publications/388/","summary":"Zhang, Xin; Chen, Xiaoxian. “Time-domain computation of multimode propagation in an aeroengine duct.” Procedia Engineering, v. 6, p. 173-182 (2010). DOI: 10.1016/j.proeng.2010.09.019.","meta":"Journal article · 2010","search_text":"time-domain computation of multimode propagation in an aeroengine duct zhang, xin; chen, xiaoxian. “time-domain computation of multimode propagation in an aeroengine duct.” procedia engineering, v. 6, p. 173-182 (2010). doi: 10.1016/j.proeng.2010.09.019. journal article · 2010 zhang, xin; chen, xiaoxian 2010 10.1016/j.proeng.2010.09.019 procedia engineering, v. 6, p. 173-182","order":432,"static_url":"/publications/388/"},{"section":"Publications","title":"Reprint of: Time-domain computation of multimode propagation in an aeroengine duct","url":"/publications/387/","summary":"Zhang, Xin; Chen, Xiaoxian. “Reprint of: Time-domain computation of multimode propagation in an aeroengine duct.” Procedia IUTAM, v. 1, p. 173-182 (2010). DOI: 10.1016/j.piutam.2010.10.019.","meta":"Journal article · 2010","search_text":"reprint of: time-domain computation of multimode propagation in an aeroengine duct zhang, xin; chen, xiaoxian. “reprint of: time-domain computation of multimode propagation in an aeroengine duct.” procedia iutam, v. 1, p. 173-182 (2010). doi: 10.1016/j.piutam.2010.10.019. journal article · 2010 zhang, xin; chen, xiaoxian 2010 10.1016/j.piutam.2010.10.019 procedia iutam, v. 1, p. 173-182","order":433,"static_url":"/publications/387/"},{"section":"Publications","title":"Ground Effect Aerodynamics","url":"/publications/80/","summary":"Cui, Erjie; Zhang, Xin. “Ground Effect Aerodynamics.” Encyclopedia of Aerospace Engineering / wiley, 2010, p. 246-256 (2010). DOI: 10.1002/9780470686652.eae022.","meta":"Book chapter · 2010","search_text":"ground effect aerodynamics cui, erjie; zhang, xin. “ground effect aerodynamics.” encyclopedia of aerospace engineering / wiley, 2010, p. 246-256 (2010). doi: 10.1002/9780470686652.eae022. book chapter · 2010 cui, erjie; zhang, xin 2010 10.1002/9780470686652.eae022 encyclopedia of aerospace engineering / wiley, 2010, p. 246-256","order":434,"static_url":"/publications/80/"},{"section":"Publications","title":"Airframe Noise – High Lift Device Noise","url":"/publications/79/","summary":"Zhang, Xin. “Airframe Noise – High Lift Device Noise.” Encyclopedia of Aerospace Engineering / wiley, 2010, p. 3541-3551 (2010). DOI: 10.1002/9780470686652.eae338.","meta":"Book chapter · 2010","search_text":"airframe noise – high lift device noise zhang, xin. “airframe noise – high lift device noise.” encyclopedia of aerospace engineering / wiley, 2010, p. 3541-3551 (2010). doi: 10.1002/9780470686652.eae338. book chapter · 2010 zhang, xin 2010 10.1002/9780470686652.eae338 encyclopedia of aerospace engineering / wiley, 2010, p. 3541-3551","order":435,"static_url":"/publications/79/"},{"section":"Publications","title":"Patched characteristic interface conditions for high-order multiblock aeroacoustic computation","url":"/publications/77/","summary":"Peers, Edward; Zhang, Xin; Kim, Jae Wook. “Patched characteristic interface conditions for high-order multiblock aeroacoustic computation.” AIAA Journal, v. 48, (11), p. 2512-2522 (2010). DOI: 10.2514/1.j050130.","meta":"Journal article · 2010","search_text":"patched characteristic interface conditions for high-order multiblock aeroacoustic computation peers, edward; zhang, xin; kim, jae wook. “patched characteristic interface conditions for high-order multiblock aeroacoustic computation.” aiaa journal, v. 48, (11), p. 2512-2522 (2010). doi: 10.2514/1.j050130. journal article · 2010 peers, edward; zhang, xin; kim, jae wook 2010 10.2514/1.j050130 aiaa journal, v. 48, (11), p. 2512-2522","order":436,"static_url":"/publications/77/"},{"section":"Publications","title":"Broadband flow-induced sound control using plasma actuators","url":"/publications/76/","summary":"Huang, Xun; Zhang, Xin; Li, Yong. “Broadband flow-induced sound control using plasma actuators.” Journal of Sound and Vibration, v. 329, (13), p. 2477-2489 (2010). DOI: 10.1016/j.jsv.2010.01.018.","meta":"Journal article · 2010","search_text":"broadband flow-induced sound control using plasma actuators huang, xun; zhang, xin; li, yong. “broadband flow-induced sound control using plasma actuators.” journal of sound and vibration, v. 329, (13), p. 2477-2489 (2010). doi: 10.1016/j.jsv.2010.01.018. journal article · 2010 huang, xun; zhang, xin; li, yong 2010 10.1016/j.jsv.2010.01.018 journal of sound and vibration, v. 329, (13), p. 2477-2489","order":437,"static_url":"/publications/76/"},{"section":"Publications","title":"Landing gear noise control using perforated fairings","url":"/publications/74/","summary":"Boorsma, K.; Zhang, X.; Molin, N.. “Landing gear noise control using perforated fairings.” Acta Mechanica Sinica/Lixue Xuebao, v. 26, (2), p. 159-174 (2010). DOI: 10.1007/s10409-009-0304-0.","meta":"Journal article · 2010","search_text":"landing gear noise control using perforated fairings boorsma, k.; zhang, x.; molin, n.. “landing gear noise control using perforated fairings.” acta mechanica sinica/lixue xuebao, v. 26, (2), p. 159-174 (2010). doi: 10.1007/s10409-009-0304-0. journal article · 2010 boorsma, k.; zhang, x.; molin, n. 2010 10.1007/s10409-009-0304-0 acta mechanica sinica/lixue xuebao, v. 26, (2), p. 159-174","order":438,"static_url":"/publications/74/"},{"section":"Publications","title":"Identification and attenuation of a tonal-noise source on an aircraft's landing gear","url":"/publications/73/","summary":"Li, Yong; Smith, Malcolm G.; Zhang, Xin. “Identification and attenuation of a tonal-noise source on an aircraft's landing gear.” Journal of Aircraft, v. 47, (3), p. 796-804 (2010). DOI: 10.2514/1.43183.","meta":"Journal article · 2010","search_text":"identification and attenuation of a tonal-noise source on an aircraft's landing gear li, yong; smith, malcolm g.; zhang, xin. “identification and attenuation of a tonal-noise source on an aircraft's landing gear.” journal of aircraft, v. 47, (3), p. 796-804 (2010). doi: 10.2514/1.43183. journal article · 2010 li, yong; smith, malcolm g.; zhang, xin 2010 10.2514/1.43183 journal of aircraft, v. 47, (3), p. 796-804","order":439,"static_url":"/publications/73/"},{"section":"Publications","title":"Plasma actuators for noise control","url":"/publications/72/","summary":"Huang, Xun; Zhang, Xin. “Plasma actuators for noise control.” International Journal of Aeroacoustics, v. 9, p. 679-703 (2010). DOI: 10.1260/1475-472x.9.4-5.679.","meta":"Journal article · 2010","search_text":"plasma actuators for noise control huang, xun; zhang, xin. “plasma actuators for noise control.” international journal of aeroacoustics, v. 9, p. 679-703 (2010). doi: 10.1260/1475-472x.9.4-5.679. journal article · 2010 huang, xun; zhang, xin 2010 10.1260/1475-472x.9.4-5.679 international journal of aeroacoustics, v. 9, p. 679-703","order":440,"static_url":"/publications/72/"},{"section":"Publications","title":"Computational investigation of a race car wing with vortex generators in ground effect","url":"/publications/71/","summary":"Kuya, Yuichi; Takeda, Kenji; Zhang, Xin. “Computational investigation of a race car wing with vortex generators in ground effect.” Journal of Fluids Engineering, Transactions of the ASME, v. 132, (2), p. 211021-211028 (2010). DOI: 10.1115/1.4000741.","meta":"Journal article · 2010","search_text":"computational investigation of a race car wing with vortex generators in ground effect kuya, yuichi; takeda, kenji; zhang, xin. “computational investigation of a race car wing with vortex generators in ground effect.” journal of fluids engineering, transactions of the asme, v. 132, (2), p. 211021-211028 (2010). doi: 10.1115/1.4000741. journal article · 2010 kuya, yuichi; takeda, kenji; zhang, xin 2010 10.1115/1.4000741 journal of fluids engineering, transactions of the asme, v. 132, (2), p. 211021-211028","order":441,"static_url":"/publications/71/"},{"section":"Publications","title":"The use of plasma actuators for bluff body broadband noise control","url":"/publications/70/","summary":"Li, Yong; Zhang, Xin; Huang, Xun. “The use of plasma actuators for bluff body broadband noise control.” Experiments in Fluids, v. 49, (2), p. 367-377 (2010). DOI: 10.1007/s00348-009-0806-3.","meta":"Journal article · 2010","search_text":"the use of plasma actuators for bluff body broadband noise control li, yong; zhang, xin; huang, xun. “the use of plasma actuators for bluff body broadband noise control.” experiments in fluids, v. 49, (2), p. 367-377 (2010). doi: 10.1007/s00348-009-0806-3. journal article · 2010 li, yong; zhang, xin; huang, xun 2010 10.1007/s00348-009-0806-3 experiments in fluids, v. 49, (2), p. 367-377","order":442,"static_url":"/publications/70/"},{"section":"Publications","title":"Patched characteristic interface condition for high-order aeroacoustic computation","url":"/publications/398/","summary":"Peers, Edward; Zhang, Xin; Kim, Jae Wook. “Patched characteristic interface condition for high-order aeroacoustic computation.” 15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference), American Institute of Aeronautics and Astronautics Inc., 2009, article nu…","meta":"Conference paper · 2009","search_text":"patched characteristic interface condition for high-order aeroacoustic computation peers, edward; zhang, xin; kim, jae wook. “patched characteristic interface condition for high-order aeroacoustic computation.” 15th aiaa/ceas aeroacoustics conference (30th aiaa aeroacoustics conference), american institute of aeronautics and astronautics inc., 2009, article number 2009-3112 (2009). doi: 10.2514/6.2009-3112. conference paper · 2009 peers, edward; zhang, xin; kim, jae wook 2009 10.2514/6.2009-3112 15th aiaa/ceas aeroacoustics conference (30th aiaa aeroacoustics conference), american institute of aeronautics and astronautics inc., 2009, article number 2009-3112","order":443,"static_url":"/publications/398/"},{"section":"Publications","title":"Optimal surrogate modelling approaches for combining experimental and computational fluid dynamics data sets","url":"/publications/397/","summary":"Kuya, Yuichi; Takeda, Kenji; Zhang, Xin. “Optimal surrogate modelling approaches for combining experimental and computational fluid dynamics data sets.” 17th AIAA/ASME/AHS Adaptive Structures Conf., 11th AIAA Non-Deterministic Approaches Conf., 10th AIAA Gossamer Spacecraft Foru…","meta":"Conference paper · 2009","search_text":"optimal surrogate modelling approaches for combining experimental and computational fluid dynamics data sets kuya, yuichi; takeda, kenji; zhang, xin. “optimal surrogate modelling approaches for combining experimental and computational fluid dynamics data sets.” 17th aiaa/asme/ahs adaptive structures conf., 11th aiaa non-deterministic approaches conf., 10th aiaa gossamer spacecraft forum, 5th aiaa multidisciplinary design optimization specialist conf., mdo, american institute of aeronautics and astronautics inc., 2009, article number 2009-2216 (2009). doi: 10.2514/6.2009-2216. conference paper · 2009 kuya, yuichi; takeda, kenji; zhang, xin 2009 10.2514/6.2009-2216 17th aiaa/asme/ahs adaptive structures conf., 11th aiaa non-deterministic approaches conf., 10th aiaa gossamer spacecraft forum, 5th aiaa multidisciplinary design optimization specialist conf., mdo, american institute of aeronautics and astronautics inc., 2009, article number 2009-2216","order":444,"static_url":"/publications/397/"},{"section":"Publications","title":"Large-scale source term modeling of vortex generation","url":"/publications/396/","summary":"Booker, Christopher; Zhang, Xin; Chernyshenko, Sergei. “Large-scale source term modeling of vortex generation.” Collection of Technical Papers - AIAA Applied Aerodynamics Conference (2009). DOI: 10.2514/6.2009-3951.","meta":"Conference paper · 2009","search_text":"large-scale source term modeling of vortex generation booker, christopher; zhang, xin; chernyshenko, sergei. “large-scale source term modeling of vortex generation.” collection of technical papers - aiaa applied aerodynamics conference (2009). doi: 10.2514/6.2009-3951. conference paper · 2009 booker, christopher; zhang, xin; chernyshenko, sergei 2009 10.2514/6.2009-3951 collection of technical papers - aiaa applied aerodynamics conference","order":445,"static_url":"/publications/396/"},{"section":"Publications","title":"High-order interface for CFD and CAA simulation","url":"/publications/395/","summary":"Chen, Xiaoxian; Zhang, Xin. “High-order interface for CFD and CAA simulation.” 16th International Congress on Sound and Vibration 2009, ICSV 2009, 2009, p. 2238-2245 (2009).","meta":"Conference paper · 2009","search_text":"high-order interface for cfd and caa simulation chen, xiaoxian; zhang, xin. “high-order interface for cfd and caa simulation.” 16th international congress on sound and vibration 2009, icsv 2009, 2009, p. 2238-2245 (2009). conference paper · 2009 chen, xiaoxian; zhang, xin 2009 16th international congress on sound and vibration 2009, icsv 2009, 2009, p. 2238-2245","order":446,"static_url":"/publications/395/"},{"section":"Publications","title":"Numerical investigation of broadband slat noise attenuation with acoustic liner treatment","url":"/publications/69/","summary":"Ma, Zhaokai; Zhang, Xin. “Numerical investigation of broadband slat noise attenuation with acoustic liner treatment.” AIAA Journal, v. 47, (12), p. 2812-2820 (2009). DOI: 10.2514/1.39883.","meta":"Journal article · 2009","search_text":"numerical investigation of broadband slat noise attenuation with acoustic liner treatment ma, zhaokai; zhang, xin. “numerical investigation of broadband slat noise attenuation with acoustic liner treatment.” aiaa journal, v. 47, (12), p. 2812-2820 (2009). doi: 10.2514/1.39883. journal article · 2009 ma, zhaokai; zhang, xin 2009 10.2514/1.39883 aiaa journal, v. 47, (12), p. 2812-2820","order":447,"static_url":"/publications/69/"},{"section":"Publications","title":"Flow separation control on a race car wing with vortex gnerators in ground effect","url":"/publications/68/","summary":"Kuya, Yuichi; Takeda, Kenji; Zhang, Xin; Beeton, Scott; Pandaleon, Ted. “Flow separation control on a race car wing with vortex gnerators in ground effect.” Journal of Fluids Engineering, Transactions of the ASME, v. 131, (12), p. 1211021-1211028 (2009). DOI: 10.1115/1.4000420.","meta":"Journal article · 2009","search_text":"flow separation control on a race car wing with vortex gnerators in ground effect kuya, yuichi; takeda, kenji; zhang, xin; beeton, scott; pandaleon, ted. “flow separation control on a race car wing with vortex gnerators in ground effect.” journal of fluids engineering, transactions of the asme, v. 131, (12), p. 1211021-1211028 (2009). doi: 10.1115/1.4000420. journal article · 2009 kuya, yuichi; takeda, kenji; zhang, xin; beeton, scott; pandaleon, ted 2009 10.1115/1.4000420 journal of fluids engineering, transactions of the asme, v. 131, (12), p. 1211021-1211028","order":448,"static_url":"/publications/68/"},{"section":"Publications","title":"Flow physics of a race car wing with wortex generators in ground effect","url":"/publications/67/","summary":"Kuya, Yuichi; Takeda, Kenji; Zhang, Xin; Beeton, Scott; Pandaleon, Ted. “Flow physics of a race car wing with wortex generators in ground effect.” Journal of Fluids Engineering, Transactions of the ASME, v. 131, (12), p. 1211031-1211039 (2009). DOI: 10.1115/1.4000423.","meta":"Journal article · 2009","search_text":"flow physics of a race car wing with wortex generators in ground effect kuya, yuichi; takeda, kenji; zhang, xin; beeton, scott; pandaleon, ted. “flow physics of a race car wing with wortex generators in ground effect.” journal of fluids engineering, transactions of the asme, v. 131, (12), p. 1211031-1211039 (2009). doi: 10.1115/1.4000423. journal article · 2009 kuya, yuichi; takeda, kenji; zhang, xin; beeton, scott; pandaleon, ted 2009 10.1115/1.4000423 journal of fluids engineering, transactions of the asme, v. 131, (12), p. 1211031-1211039","order":449,"static_url":"/publications/67/"},{"section":"Publications","title":"The aerodynamic interaction between an inverted wing and a rotating wheel","url":"/publications/66/","summary":"Van Den Berg, M. A.; Zhang, X.. “The aerodynamic interaction between an inverted wing and a rotating wheel.” Journal of Fluids Engineering, Transactions of the ASME, v. 131, (10), p. 1011041-10110413 (2009). DOI: 10.1115/1.3215942.","meta":"Journal article · 2009","search_text":"the aerodynamic interaction between an inverted wing and a rotating wheel van den berg, m. a.; zhang, x.. “the aerodynamic interaction between an inverted wing and a rotating wheel.” journal of fluids engineering, transactions of the asme, v. 131, (10), p. 1011041-10110413 (2009). doi: 10.1115/1.3215942. journal article · 2009 van den berg, m. a.; zhang, x. 2009 10.1115/1.3215942 journal of fluids engineering, transactions of the asme, v. 131, (10), p. 1011041-10110413","order":450,"static_url":"/publications/66/"},{"section":"Publications","title":"Measurements of flow around a flap side edge with porous edge treatment","url":"/publications/65/","summary":"Angland, D.; Zhang, X.; Molin, N.. “Measurements of flow around a flap side edge with porous edge treatment.” AIAA Journal, v. 47, (7), p. 1660-1671 (2009). DOI: 10.2514/1.39311.","meta":"Journal article · 2009","search_text":"measurements of flow around a flap side edge with porous edge treatment angland, d.; zhang, x.; molin, n.. “measurements of flow around a flap side edge with porous edge treatment.” aiaa journal, v. 47, (7), p. 1660-1671 (2009). doi: 10.2514/1.39311. journal article · 2009 angland, d.; zhang, x.; molin, n. 2009 10.2514/1.39311 aiaa journal, v. 47, (7), p. 1660-1671","order":451,"static_url":"/publications/65/"},{"section":"Publications","title":"Bluff body noise control using perforated fairings","url":"/publications/64/","summary":"Boorsma, K.; Zhang, X.; Molin, N.; Chow, L. C.. “Bluff body noise control using perforated fairings.” AIAA Journal, v. 47, (1), p. 33-43 (2009). DOI: 10.2514/1.32766.","meta":"Journal article · 2009","search_text":"bluff body noise control using perforated fairings boorsma, k.; zhang, x.; molin, n.; chow, l. c.. “bluff body noise control using perforated fairings.” aiaa journal, v. 47, (1), p. 33-43 (2009). doi: 10.2514/1.32766. journal article · 2009 boorsma, k.; zhang, x.; molin, n.; chow, l. c. 2009 10.2514/1.32766 aiaa journal, v. 47, (1), p. 33-43","order":452,"static_url":"/publications/64/"},{"section":"Publications","title":"Sound radiation from a bypass duct with bifurcations","url":"/publications/63/","summary":"Chen, Xiaoxian; Huang, Xun; Zhang, Xin. “Sound radiation from a bypass duct with bifurcations.” AIAA Journal, v. 47, (2), p. 429-436 (2009). DOI: 10.2514/1.39710.","meta":"Journal article · 2009","search_text":"sound radiation from a bypass duct with bifurcations chen, xiaoxian; huang, xun; zhang, xin. “sound radiation from a bypass duct with bifurcations.” aiaa journal, v. 47, (2), p. 429-436 (2009). doi: 10.2514/1.39710. journal article · 2009 chen, xiaoxian; huang, xun; zhang, xin 2009 10.2514/1.39710 aiaa journal, v. 47, (2), p. 429-436","order":453,"static_url":"/publications/63/"},{"section":"Publications","title":"The use of a fairing and split plate for bluff body noise control","url":"/publications/403/","summary":"Spiteri, M.; Zhang, X.; Molin, N.; Chow, L. C.. “The use of a fairing and split plate for bluff body noise control.” 14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference), American Institute of Aeronautics and Astronautics Inc., 2008, article number 2008-2…","meta":"Conference paper · 2008","search_text":"the use of a fairing and split plate for bluff body noise control spiteri, m.; zhang, x.; molin, n.; chow, l. c.. “the use of a fairing and split plate for bluff body noise control.” 14th aiaa/ceas aeroacoustics conference (29th aiaa aeroacoustics conference), american institute of aeronautics and astronautics inc., 2008, article number 2008-2817 (2008). doi: 10.2514/6.2008-2817. conference paper · 2008 spiteri, m.; zhang, x.; molin, n.; chow, l. c. 2008 10.2514/6.2008-2817 14th aiaa/ceas aeroacoustics conference (29th aiaa aeroacoustics conference), american institute of aeronautics and astronautics inc., 2008, article number 2008-2817","order":454,"static_url":"/publications/403/"},{"section":"Publications","title":"Sound radiation from a generic bypass duct with bifurcations","url":"/publications/402/","summary":"Chen, Xiaoxian; Huang, Xun; Zhang, Xin. “Sound radiation from a generic bypass duct with bifurcations.” 14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference), 2008, article number 2008-2877 (2008). DOI: 10.2514/6.2008-2877.","meta":"Conference paper · 2008","search_text":"sound radiation from a generic bypass duct with bifurcations chen, xiaoxian; huang, xun; zhang, xin. “sound radiation from a generic bypass duct with bifurcations.” 14th aiaa/ceas aeroacoustics conference (29th aiaa aeroacoustics conference), 2008, article number 2008-2877 (2008). doi: 10.2514/6.2008-2877. conference paper · 2008 chen, xiaoxian; huang, xun; zhang, xin 2008 10.2514/6.2008-2877 14th aiaa/ceas aeroacoustics conference (29th aiaa aeroacoustics conference), 2008, article number 2008-2877","order":455,"static_url":"/publications/402/"},{"section":"Publications","title":"Perforated fairings for landing gear noise control","url":"/publications/401/","summary":"Boorsma, K.; Zhang, X.; Molin, N.. “Perforated fairings for landing gear noise control.” 14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference), American Institute of Aeronautics and Astronautics Inc., 2008, article number 2008-2961 (2008). DOI: 10.2514/6.2…","meta":"Conference paper · 2008","search_text":"perforated fairings for landing gear noise control boorsma, k.; zhang, x.; molin, n.. “perforated fairings for landing gear noise control.” 14th aiaa/ceas aeroacoustics conference (29th aiaa aeroacoustics conference), american institute of aeronautics and astronautics inc., 2008, article number 2008-2961 (2008). doi: 10.2514/6.2008-2961. conference paper · 2008 boorsma, k.; zhang, x.; molin, n. 2008 10.2514/6.2008-2961 14th aiaa/ceas aeroacoustics conference (29th aiaa aeroacoustics conference), american institute of aeronautics and astronautics inc., 2008, article number 2008-2961","order":456,"static_url":"/publications/401/"},{"section":"Publications","title":"Broadband slat noise attenuation with acoustic liner treatment","url":"/publications/400/","summary":"Ma, Zhaokai; Zhang, Xin. “Broadband slat noise attenuation with acoustic liner treatment.” 14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference), American Institute of Aeronautics and Astronautics Inc., 2008, article number 2008-2964 (2008). DOI: 10.2514/6…","meta":"Conference paper · 2008","search_text":"broadband slat noise attenuation with acoustic liner treatment ma, zhaokai; zhang, xin. “broadband slat noise attenuation with acoustic liner treatment.” 14th aiaa/ceas aeroacoustics conference (29th aiaa aeroacoustics conference), american institute of aeronautics and astronautics inc., 2008, article number 2008-2964 (2008). doi: 10.2514/6.2008-2964. conference paper · 2008 ma, zhaokai; zhang, xin 2008 10.2514/6.2008-2964 14th aiaa/ceas aeroacoustics conference (29th aiaa aeroacoustics conference), american institute of aeronautics and astronautics inc., 2008, article number 2008-2964","order":457,"static_url":"/publications/400/"},{"section":"Publications","title":"Bluff body noise and flow control with atmospheric plasma actuators","url":"/publications/399/","summary":"Huang, Xun; Zhang, Xin; Gabriel, Steve. “Bluff body noise and flow control with atmospheric plasma actuators.” 14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference), American Institute of Aeronautics and Astronautics Inc., 2008, article number 2008-3044 (2…","meta":"Conference paper · 2008","search_text":"bluff body noise and flow control with atmospheric plasma actuators huang, xun; zhang, xin; gabriel, steve. “bluff body noise and flow control with atmospheric plasma actuators.” 14th aiaa/ceas aeroacoustics conference (29th aiaa aeroacoustics conference), american institute of aeronautics and astronautics inc., 2008, article number 2008-3044 (2008). doi: 10.2514/6.2008-3044. conference paper · 2008 huang, xun; zhang, xin; gabriel, steve 2008 10.2514/6.2008-3044 14th aiaa/ceas aeroacoustics conference (29th aiaa aeroacoustics conference), american institute of aeronautics and astronautics inc., 2008, article number 2008-3044","order":458,"static_url":"/publications/399/"},{"section":"Publications","title":"Adaptive mesh refinement computation of acoustic radiation from an engine intake","url":"/publications/62/","summary":"Huang, Xun; Zhang, Xin; Richards, Simon Keith. “Adaptive mesh refinement computation of acoustic radiation from an engine intake.” Aerospace Science and Technology, v. 12, (5), p. 418-426 (2008). DOI: 10.1016/j.ast.2007.09.004.","meta":"Journal article · 2008","search_text":"adaptive mesh refinement computation of acoustic radiation from an engine intake huang, xun; zhang, xin; richards, simon keith. “adaptive mesh refinement computation of acoustic radiation from an engine intake.” aerospace science and technology, v. 12, (5), p. 418-426 (2008). doi: 10.1016/j.ast.2007.09.004. journal article · 2008 huang, xun; zhang, xin; richards, simon keith 2008 10.1016/j.ast.2007.09.004 aerospace science and technology, v. 12, (5), p. 418-426","order":459,"static_url":"/publications/62/"},{"section":"Publications","title":"Streamwise and spanwise plasma actuators for flow-induced cavity noise control","url":"/publications/61/","summary":"Huang, Xun; Zhang, Xin. “Streamwise and spanwise plasma actuators for flow-induced cavity noise control.” Physics of Fluids, v. 20, (3), article number 037101 (2008). DOI: 10.1063/1.2890448.","meta":"Journal article · 2008","search_text":"streamwise and spanwise plasma actuators for flow-induced cavity noise control huang, xun; zhang, xin. “streamwise and spanwise plasma actuators for flow-induced cavity noise control.” physics of fluids, v. 20, (3), article number 037101 (2008). doi: 10.1063/1.2890448. journal article · 2008 huang, xun; zhang, xin 2008 10.1063/1.2890448 physics of fluids, v. 20, (3), article number 037101","order":460,"static_url":"/publications/61/"},{"section":"Publications","title":"Efficient computation of spinning modal radiation through an engine bypass duct","url":"/publications/60/","summary":"Huang, Xun; Chen, Xiaoxian; Ma, Zhaokai; Zhang, Xin. “Efficient computation of spinning modal radiation through an engine bypass duct.” AIAA Journal, v. 46, (6), p. 1413-1423 (2008). DOI: 10.2514/1.31136.","meta":"Journal article · 2008","search_text":"efficient computation of spinning modal radiation through an engine bypass duct huang, xun; chen, xiaoxian; ma, zhaokai; zhang, xin. “efficient computation of spinning modal radiation through an engine bypass duct.” aiaa journal, v. 46, (6), p. 1413-1423 (2008). doi: 10.2514/1.31136. journal article · 2008 huang, xun; chen, xiaoxian; ma, zhaokai; zhang, xin 2008 10.2514/1.31136 aiaa journal, v. 46, (6), p. 1413-1423","order":461,"static_url":"/publications/60/"},{"section":"Publications","title":"Variable structure model for flow-induced tonal noise control with plasma actuators","url":"/publications/59/","summary":"Huang, Xun; Chan, Sammie; Zhang, Xin; Gabriel, Steve. “Variable structure model for flow-induced tonal noise control with plasma actuators.” AIAA Journal, v. 46, (1), p. 241-250 (2008). DOI: 10.2514/1.30852.","meta":"Journal article · 2008","search_text":"variable structure model for flow-induced tonal noise control with plasma actuators huang, xun; chan, sammie; zhang, xin; gabriel, steve. “variable structure model for flow-induced tonal noise control with plasma actuators.” aiaa journal, v. 46, (1), p. 241-250 (2008). doi: 10.2514/1.30852. journal article · 2008 huang, xun; chan, sammie; zhang, xin; gabriel, steve 2008 10.2514/1.30852 aiaa journal, v. 46, (1), p. 241-250","order":462,"static_url":"/publications/59/"},{"section":"Publications","title":"Unsteady RANS and detached-eddy simulations of flow around a circular cylinder in ground effect","url":"/publications/58/","summary":"Nishino, T.; Roberts, G. T.; Zhang, X.. “Unsteady RANS and detached-eddy simulations of flow around a circular cylinder in ground effect.” Journal of Fluids and Structures, v. 24, (1), p. 18-33 (2008). DOI: 10.1016/j.jfluidstructs.2007.06.002.","meta":"Journal article · 2008","search_text":"unsteady rans and detached-eddy simulations of flow around a circular cylinder in ground effect nishino, t.; roberts, g. t.; zhang, x.. “unsteady rans and detached-eddy simulations of flow around a circular cylinder in ground effect.” journal of fluids and structures, v. 24, (1), p. 18-33 (2008). doi: 10.1016/j.jfluidstructs.2007.06.002. journal article · 2008 nishino, t.; roberts, g. t.; zhang, x. 2008 10.1016/j.jfluidstructs.2007.06.002 journal of fluids and structures, v. 24, (1), p. 18-33","order":463,"static_url":"/publications/58/"},{"section":"Publications","title":"Variable structure model for flow-induced tonal noise control with plasma actuators","url":"/publications/408/","summary":"Huang, Xun; Chan, Sammie; Zhang, Xin; Gabrielx, Steve. “Variable structure model for flow-induced tonal noise control with plasma actuators.” 13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference), 2007, (2007). DOI: 10.2514/6.2007-3561.","meta":"Conference paper · 2007","search_text":"variable structure model for flow-induced tonal noise control with plasma actuators huang, xun; chan, sammie; zhang, xin; gabrielx, steve. “variable structure model for flow-induced tonal noise control with plasma actuators.” 13th aiaa/ceas aeroacoustics conference (28th aiaa aeroacoustics conference), 2007, (2007). doi: 10.2514/6.2007-3561. conference paper · 2007 huang, xun; chan, sammie; zhang, xin; gabrielx, steve 2007 10.2514/6.2007-3561 13th aiaa/ceas aeroacoustics conference (28th aiaa aeroacoustics conference), 2007,","order":464,"static_url":"/publications/408/"},{"section":"Publications","title":"Perforated fairings for Bluff body noise control","url":"/publications/407/","summary":"Boorsma, K.; Zhang, X.; Molin, N.. “Perforated fairings for Bluff body noise control.” 13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference), American Institute of Aeronautics and Astronautics Inc., 2007, (2007). DOI: 10.2514/6.2007-3462.","meta":"Conference paper · 2007","search_text":"perforated fairings for bluff body noise control boorsma, k.; zhang, x.; molin, n.. “perforated fairings for bluff body noise control.” 13th aiaa/ceas aeroacoustics conference (28th aiaa aeroacoustics conference), american institute of aeronautics and astronautics inc., 2007, (2007). doi: 10.2514/6.2007-3462. conference paper · 2007 boorsma, k.; zhang, x.; molin, n. 2007 10.2514/6.2007-3462 13th aiaa/ceas aeroacoustics conference (28th aiaa aeroacoustics conference), american institute of aeronautics and astronautics inc., 2007,","order":465,"static_url":"/publications/407/"},{"section":"Publications","title":"Noise sources control of an aircraft landing gear","url":"/publications/406/","summary":"Li, Yong; Smith, Malcolm G.; Zhang, Xin; Molin, Nicolas. “Noise sources control of an aircraft landing gear.” 13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference), 2007, (2007). DOI: 10.2514/6.2007-3465.","meta":"Conference paper · 2007","search_text":"noise sources control of an aircraft landing gear li, yong; smith, malcolm g.; zhang, xin; molin, nicolas. “noise sources control of an aircraft landing gear.” 13th aiaa/ceas aeroacoustics conference (28th aiaa aeroacoustics conference), 2007, (2007). doi: 10.2514/6.2007-3465. conference paper · 2007 li, yong; smith, malcolm g.; zhang, xin; molin, nicolas 2007 10.2514/6.2007-3465 13th aiaa/ceas aeroacoustics conference (28th aiaa aeroacoustics conference), 2007,","order":466,"static_url":"/publications/406/"},{"section":"Publications","title":"Measurements of flow around a split flap configuration","url":"/publications/405/","summary":"Angland, D.; Zhang, X.; Molin, N.; Chow, L. C.. “Measurements of flow around a split flap configuration.” Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting, 2007, p. 2657-2674 (2007). DOI: 10.2514/6.2007-225.","meta":"Conference paper · 2007","search_text":"measurements of flow around a split flap configuration angland, d.; zhang, x.; molin, n.; chow, l. c.. “measurements of flow around a split flap configuration.” collection of technical papers - 45th aiaa aerospace sciences meeting, 2007, p. 2657-2674 (2007). doi: 10.2514/6.2007-225. conference paper · 2007 angland, d.; zhang, x.; molin, n.; chow, l. c. 2007 10.2514/6.2007-225 collection of technical papers - 45th aiaa aerospace sciences meeting, 2007, p. 2657-2674","order":467,"static_url":"/publications/405/"},{"section":"Publications","title":"Unsteady simulations of the flow around a short surface-mounted cylinder","url":"/publications/404/","summary":"Pattenden, R. J.; Bressloff, N. W.; Turnock, S. R.; Zhang, X.. “Unsteady simulations of the flow around a short surface-mounted cylinder.” International Journal for Numerical Methods in Fluids, v. 53, (6), p. 895-914 (2007). DOI: 10.1002/fld.1309.","meta":"Journal article · 2007","search_text":"unsteady simulations of the flow around a short surface-mounted cylinder pattenden, r. j.; bressloff, n. w.; turnock, s. r.; zhang, x.. “unsteady simulations of the flow around a short surface-mounted cylinder.” international journal for numerical methods in fluids, v. 53, (6), p. 895-914 (2007). doi: 10.1002/fld.1309. journal article · 2007 pattenden, r. j.; bressloff, n. w.; turnock, s. r.; zhang, x. 2007 10.1002/fld.1309 international journal for numerical methods in fluids, v. 53, (6), p. 895-914","order":468,"static_url":"/publications/404/"},{"section":"Publications","title":"Aerodynamic model of a hill climb racing car","url":"/publications/57/","summary":"Blyth, Paul; Dunning, Paul; Gardiner, Mark; Wood, Christian; Zhang, Xin. “Aerodynamic model of a hill climb racing car.” Bernoulli Aerodynamics International, v. 2, p. 52-61 (2007).","meta":"Journal article · 2007","search_text":"aerodynamic model of a hill climb racing car blyth, paul; dunning, paul; gardiner, mark; wood, christian; zhang, xin. “aerodynamic model of a hill climb racing car.” bernoulli aerodynamics international, v. 2, p. 52-61 (2007). journal article · 2007 blyth, paul; dunning, paul; gardiner, mark; wood, christian; zhang, xin 2007 bernoulli aerodynamics international, v. 2, p. 52-61","order":469,"static_url":"/publications/57/"},{"section":"Publications","title":"Atmospheric plasma actuators for aeroacoustic applications","url":"/publications/56/","summary":"Huang, Xun; Chan, Sammie; Zhang, Xin. “Atmospheric plasma actuators for aeroacoustic applications.” IEEE Transactions on Plasma Science, v. 35, (3), p. 693-695 (2007). DOI: 10.1109/tps.2007.896781.","meta":"Journal article · 2007","search_text":"atmospheric plasma actuators for aeroacoustic applications huang, xun; chan, sammie; zhang, xin. “atmospheric plasma actuators for aeroacoustic applications.” ieee transactions on plasma science, v. 35, (3), p. 693-695 (2007). doi: 10.1109/tps.2007.896781. journal article · 2007 huang, xun; chan, sammie; zhang, xin 2007 10.1109/tps.2007.896781 ieee transactions on plasma science, v. 35, (3), p. 693-695","order":470,"static_url":"/publications/56/"},{"section":"Publications","title":"Computation of Fan Noise Radiation through an Engine Exhaust Geometry with Flow","url":"/publications/54/","summary":"Richards, Simon Keith; Chen, Xiaoxian; Huang, Xun; Zhang, Xin. “Computation of Fan Noise Radiation through an Engine Exhaust Geometry with Flow.” International Journal of Aeroacoustics, v. 6, p. 223-241 (2007). DOI: 10.1260/147547207782419534.","meta":"Journal article · 2007","search_text":"computation of fan noise radiation through an engine exhaust geometry with flow richards, simon keith; chen, xiaoxian; huang, xun; zhang, xin. “computation of fan noise radiation through an engine exhaust geometry with flow.” international journal of aeroacoustics, v. 6, p. 223-241 (2007). doi: 10.1260/147547207782419534. journal article · 2007 richards, simon keith; chen, xiaoxian; huang, xun; zhang, xin 2007 10.1260/147547207782419534 international journal of aeroacoustics, v. 6, p. 223-241","order":471,"static_url":"/publications/54/"},{"section":"Publications","title":"Attenuation of low-speed flow-induced cavity tones using plasma actuators","url":"/publications/53/","summary":"Chan, Sammie; Zhang, Xin; Gabriel, Steve. “Attenuation of low-speed flow-induced cavity tones using plasma actuators.” AIAA Journal, v. 45, (7), p. 1525-1538 (2007). DOI: 10.2514/1.26645.","meta":"Journal article · 2007","search_text":"attenuation of low-speed flow-induced cavity tones using plasma actuators chan, sammie; zhang, xin; gabriel, steve. “attenuation of low-speed flow-induced cavity tones using plasma actuators.” aiaa journal, v. 45, (7), p. 1525-1538 (2007). doi: 10.2514/1.26645. journal article · 2007 chan, sammie; zhang, xin; gabriel, steve 2007 10.2514/1.26645 aiaa journal, v. 45, (7), p. 1525-1538","order":472,"static_url":"/publications/53/"},{"section":"Publications","title":"Vortex shedding from a circular cylinder near a moving ground","url":"/publications/52/","summary":"Nishino, Takafumi; Roberts, Graham T.; Zhang, Xin. “Vortex shedding from a circular cylinder near a moving ground.” Physics of Fluids, v. 19, (2), article number 025103 (2007). DOI: 10.1063/1.2710273.","meta":"Journal article · 2007","search_text":"vortex shedding from a circular cylinder near a moving ground nishino, takafumi; roberts, graham t.; zhang, xin. “vortex shedding from a circular cylinder near a moving ground.” physics of fluids, v. 19, (2), article number 025103 (2007). doi: 10.1063/1.2710273. journal article · 2007 nishino, takafumi; roberts, graham t.; zhang, xin 2007 10.1063/1.2710273 physics of fluids, v. 19, (2), article number 025103","order":473,"static_url":"/publications/52/"},{"section":"Publications","title":"Detached eddy simulation of flow around a circular cylinder in ground effect","url":"/publications/450/","summary":"Nishino, T., Roberts, G. and Zhang, X.. “Detached eddy simulation of flow around a circular cylinder in ground effect.” 17th International Symposium on Transport Phenomena, Toyama, Japan, 4-8 September 2006 (2006).","meta":"Conference paper · 2006","search_text":"detached eddy simulation of flow around a circular cylinder in ground effect nishino, t., roberts, g. and zhang, x.. “detached eddy simulation of flow around a circular cylinder in ground effect.” 17th international symposium on transport phenomena, toyama, japan, 4-8 september 2006 (2006). conference paper · 2006 nishino, t., roberts, g. and zhang, x. 2006 17th international symposium on transport phenomena, toyama, japan, 4-8 september 2006.","order":474,"static_url":"/publications/450/"},{"section":"Publications","title":"Measurements of flow around a flap side-edge with porous edge treatment","url":"/publications/411/","summary":"Angland, D.; Zhang, X.; Chow, L. C.; Molin, N.. “Measurements of flow around a flap side-edge with porous edge treatment.” Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting, American Institute of Aeronautics and Astronautics Inc., 2006, p. 2554-2575 (2006). D…","meta":"Conference paper · 2006","search_text":"measurements of flow around a flap side-edge with porous edge treatment angland, d.; zhang, x.; chow, l. c.; molin, n.. “measurements of flow around a flap side-edge with porous edge treatment.” collection of technical papers - 44th aiaa aerospace sciences meeting, american institute of aeronautics and astronautics inc., 2006, p. 2554-2575 (2006). doi: 10.2514/6.2006-213. conference paper · 2006 angland, d.; zhang, x.; chow, l. c.; molin, n. 2006 10.2514/6.2006-213 collection of technical papers - 44th aiaa aerospace sciences meeting, american institute of aeronautics and astronautics inc., 2006, p. 2554-2575","order":475,"static_url":"/publications/411/"},{"section":"Publications","title":"An experimental study of flow around a circular cylinder with and without end plates in ground effect","url":"/publications/410/","summary":"Nishino, Takafumi; Roberts, Graham T.; Zhang, Xin. “An experimental study of flow around a circular cylinder with and without end plates in ground effect.” Collection of Technical Papers - 36th AIAA Fluid Dynamics Conference, American Institute of Aeronautics and Astronautics In…","meta":"Conference paper · 2006","search_text":"an experimental study of flow around a circular cylinder with and without end plates in ground effect nishino, takafumi; roberts, graham t.; zhang, xin. “an experimental study of flow around a circular cylinder with and without end plates in ground effect.” collection of technical papers - 36th aiaa fluid dynamics conference, american institute of aeronautics and astronautics inc., 2006, p. 1714-1728 (2006). doi: 10.2514/6.2006-3551. conference paper · 2006 nishino, takafumi; roberts, graham t.; zhang, xin 2006 10.2514/6.2006-3551 collection of technical papers - 36th aiaa fluid dynamics conference, american institute of aeronautics and astronautics inc., 2006, p. 1714-1728","order":476,"static_url":"/publications/410/"},{"section":"Publications","title":"Adaptive mesh refinement computation of acoustic radiation from an engine intake","url":"/publications/409/","summary":"Huang, Xun; Zhang, Xin. “Adaptive mesh refinement computation of acoustic radiation from an engine intake.” Collection of Technical Papers - 12th AIAA/CEAS Aeroacoustics Conference, 2006, p. 3813-3825 (2006). DOI: 10.2514/6.2006-2694.","meta":"Conference paper · 2006","search_text":"adaptive mesh refinement computation of acoustic radiation from an engine intake huang, xun; zhang, xin. “adaptive mesh refinement computation of acoustic radiation from an engine intake.” collection of technical papers - 12th aiaa/ceas aeroacoustics conference, 2006, p. 3813-3825 (2006). doi: 10.2514/6.2006-2694. conference paper · 2006 huang, xun; zhang, xin 2006 10.2514/6.2006-2694 collection of technical papers - 12th aiaa/ceas aeroacoustics conference, 2006, p. 3813-3825","order":477,"static_url":"/publications/409/"},{"section":"Publications","title":"Ground effect aerodynamics research of racing cars","url":"/publications/51/","summary":"Zhang, Xin; Toet, Willem. “Ground effect aerodynamics research of racing cars.” AutoTechnology, v. 6, (DEC.), p. 40-43 (2006). DOI: 10.1007/bf03246972.","meta":"Journal article · 2006","search_text":"ground effect aerodynamics research of racing cars zhang, xin; toet, willem. “ground effect aerodynamics research of racing cars.” autotechnology, v. 6, (dec.), p. 40-43 (2006). doi: 10.1007/bf03246972. journal article · 2006 zhang, xin; toet, willem 2006 10.1007/bf03246972 autotechnology, v. 6, (dec.), p. 40-43","order":478,"static_url":"/publications/51/"},{"section":"Publications","title":"Attenuation of Slat Trailing Edge Noise Using Acoustic Liners","url":"/publications/50/","summary":"Ma, Zhaokai; Richards, Simon K.; Smith, Malcolm G.; Zhang, Xin. “Attenuation of Slat Trailing Edge Noise Using Acoustic Liners.” International Journal of Aeroacoustics, v. 5, p. 311-333 (2006). DOI: 10.1260/147547206779379886.","meta":"Journal article · 2006","search_text":"attenuation of slat trailing edge noise using acoustic liners ma, zhaokai; richards, simon k.; smith, malcolm g.; zhang, xin. “attenuation of slat trailing edge noise using acoustic liners.” international journal of aeroacoustics, v. 5, p. 311-333 (2006). doi: 10.1260/147547206779379886. journal article · 2006 ma, zhaokai; richards, simon k.; smith, malcolm g.; zhang, xin 2006 10.1260/147547206779379886 international journal of aeroacoustics, v. 5, p. 311-333","order":479,"static_url":"/publications/50/"},{"section":"Publications","title":"Computational analysis of a inverted double-element airfoil in ground effect","url":"/publications/49/","summary":"Mahon, Stephen; Zhang, Xin. “Computational analysis of a inverted double-element airfoil in ground effect.” Journal of Fluids Engineering, Transactions of the ASME, v. 128, (6), p. 1172-1180 (2006). DOI: 10.1115/1.2353268.","meta":"Journal article · 2006","search_text":"computational analysis of a inverted double-element airfoil in ground effect mahon, stephen; zhang, xin. “computational analysis of a inverted double-element airfoil in ground effect.” journal of fluids engineering, transactions of the asme, v. 128, (6), p. 1172-1180 (2006). doi: 10.1115/1.2353268. journal article · 2006 mahon, stephen; zhang, xin 2006 10.1115/1.2353268 journal of fluids engineering, transactions of the asme, v. 128, (6), p. 1172-1180","order":480,"static_url":"/publications/49/"},{"section":"Publications","title":"A Fourier Pseudospectral Method for Some Computational Aeroacoustics Problems","url":"/publications/48/","summary":"Huang, Xun; Zhang, Xin. “A Fourier Pseudospectral Method for Some Computational Aeroacoustics Problems.” International Journal of Aeroacoustics, v. 5, p. 279-294 (2006). DOI: 10.1260/1475-472x.5.3.279.","meta":"Journal article · 2006","search_text":"a fourier pseudospectral method for some computational aeroacoustics problems huang, xun; zhang, xin. “a fourier pseudospectral method for some computational aeroacoustics problems.” international journal of aeroacoustics, v. 5, p. 279-294 (2006). doi: 10.1260/1475-472x.5.3.279. journal article · 2006 huang, xun; zhang, xin 2006 10.1260/1475-472x.5.3.279 international journal of aeroacoustics, v. 5, p. 279-294","order":481,"static_url":"/publications/48/"},{"section":"Publications","title":"A computational study of the flow around an isolated wheel in contact with the ground","url":"/publications/47/","summary":"McManus, James; Zhang, Xin. “A computational study of the flow around an isolated wheel in contact with the ground.” Journal of Fluids Engineering, Transactions of the ASME, v. 128, (3), p. 520-530 (2006). DOI: 10.1115/1.2175158.","meta":"Journal article · 2006","search_text":"a computational study of the flow around an isolated wheel in contact with the ground mcmanus, james; zhang, xin. “a computational study of the flow around an isolated wheel in contact with the ground.” journal of fluids engineering, transactions of the asme, v. 128, (3), p. 520-530 (2006). doi: 10.1115/1.2175158. journal article · 2006 mcmanus, james; zhang, xin 2006 10.1115/1.2175158 journal of fluids engineering, transactions of the asme, v. 128, (3), p. 520-530","order":482,"static_url":"/publications/47/"},{"section":"Publications","title":"Ground effect aerodynamics of race cars","url":"/publications/46/","summary":"Zhang, Xin; Toet, Willem; Zerihan, Jonathan. “Ground effect aerodynamics of race cars.” Applied Mechanics Reviews, v. 59, (1-6), p. 33-48 (2006). DOI: 10.1115/1.2110263.","meta":"Journal article · 2006","search_text":"ground effect aerodynamics of race cars zhang, xin; toet, willem; zerihan, jonathan. “ground effect aerodynamics of race cars.” applied mechanics reviews, v. 59, (1-6), p. 33-48 (2006). doi: 10.1115/1.2110263. journal article · 2006 zhang, xin; toet, willem; zerihan, jonathan 2006 10.1115/1.2110263 applied mechanics reviews, v. 59, (1-6), p. 33-48","order":483,"static_url":"/publications/46/"},{"section":"Publications","title":"The attenuation of cavity tones using plasma actuators","url":"/publications/416/","summary":"Chan, Sammie; Zhang, Xin; Gabriel, Steve. “The attenuation of cavity tones using plasma actuators.” Collection of Technical Papers - 11th AIAA/CEAS Aeroacoustics Conference, 2005, p. 30-43 (2005). DOI: 10.2514/6.2005-2802.","meta":"Conference paper · 2005","search_text":"the attenuation of cavity tones using plasma actuators chan, sammie; zhang, xin; gabriel, steve. “the attenuation of cavity tones using plasma actuators.” collection of technical papers - 11th aiaa/ceas aeroacoustics conference, 2005, p. 30-43 (2005). doi: 10.2514/6.2005-2802. conference paper · 2005 chan, sammie; zhang, xin; gabriel, steve 2005 10.2514/6.2005-2802 collection of technical papers - 11th aiaa/ceas aeroacoustics conference, 2005, p. 30-43","order":484,"static_url":"/publications/416/"},{"section":"Publications","title":"Slat noise attenuation using acoustic liner","url":"/publications/415/","summary":"Ma, Zhaokai; Smith, Malcolm; Richards, Simon K.; Zhang, Xin. “Slat noise attenuation using acoustic liner.” Collection of Technical Papers - 11th AIAA/CEAS Aeroacoustics Conference, American Institute of Aeronautics and Astronautics Inc., 2005, p. 2634-2647 (2005). DOI: 10.2514/…","meta":"Conference paper · 2005","search_text":"slat noise attenuation using acoustic liner ma, zhaokai; smith, malcolm; richards, simon k.; zhang, xin. “slat noise attenuation using acoustic liner.” collection of technical papers - 11th aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc., 2005, p. 2634-2647 (2005). doi: 10.2514/6.2005-3009. conference paper · 2005 ma, zhaokai; smith, malcolm; richards, simon k.; zhang, xin 2005 10.2514/6.2005-3009 collection of technical papers - 11th aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc., 2005, p. 2634-2647","order":485,"static_url":"/publications/415/"},{"section":"Publications","title":"Parallel computation of 3D acoustic radiation from an engine intake","url":"/publications/414/","summary":"Richards, S. K.; Ghent, X. X.; Zhang, X.. “Parallel computation of 3D acoustic radiation from an engine intake.” Collection of Technical Papers - 11th AIAA/CEAS Aeroacoustics Conference, American Institute of Aeronautics and Astronautics Inc., 2005, p. 1856-1871 (2005). DOI: 10.…","meta":"Conference paper · 2005","search_text":"parallel computation of 3d acoustic radiation from an engine intake richards, s. k.; ghent, x. x.; zhang, x.. “parallel computation of 3d acoustic radiation from an engine intake.” collection of technical papers - 11th aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc., 2005, p. 1856-1871 (2005). doi: 10.2514/6.2005-2947. conference paper · 2005 richards, s. k.; ghent, x. x.; zhang, x. 2005 10.2514/6.2005-2947 collection of technical papers - 11th aiaa/ceas aeroacoustics conference, american institute of aeronautics and astronautics inc., 2005, p. 1856-1871","order":486,"static_url":"/publications/414/"},{"section":"Publications","title":"Adaptive mesh refinement for computational aeroacoustics","url":"/publications/413/","summary":"Huang, Xun; Zhang, Xin. “Adaptive mesh refinement for computational aeroacoustics.” Collection of Technical Papers - 11th AIAA/CEAS Aeroacoustics Conference, 2005, p. 937-950 (2005). DOI: 10.2514/6.2005-2873.","meta":"Conference paper · 2005","search_text":"adaptive mesh refinement for computational aeroacoustics huang, xun; zhang, xin. “adaptive mesh refinement for computational aeroacoustics.” collection of technical papers - 11th aiaa/ceas aeroacoustics conference, 2005, p. 937-950 (2005). doi: 10.2514/6.2005-2873. conference paper · 2005 huang, xun; zhang, xin 2005 10.2514/6.2005-2873 collection of technical papers - 11th aiaa/ceas aeroacoustics conference, 2005, p. 937-950","order":487,"static_url":"/publications/413/"},{"section":"Publications","title":"Aerodynamics of a Half-Cylinder in Ground Effect","url":"/publications/412/","summary":"Zhang, X.; Mahon, S.; Van Den-Berg, M.; Williams, C.. “Aerodynamics of a Half-Cylinder in Ground Effect.” Engineering Turbulence Modelling and Experiments 6 / Elsevier, 2005, p. 461-470 (2005). DOI: 10.1016/b978-008044544-1/50044-3.","meta":"Book chapter · 2005","search_text":"aerodynamics of a half-cylinder in ground effect zhang, x.; mahon, s.; van den-berg, m.; williams, c.. “aerodynamics of a half-cylinder in ground effect.” engineering turbulence modelling and experiments 6 / elsevier, 2005, p. 461-470 (2005). doi: 10.1016/b978-008044544-1/50044-3. book chapter · 2005 zhang, x.; mahon, s.; van den-berg, m.; williams, c. 2005 10.1016/b978-008044544-1/50044-3 engineering turbulence modelling and experiments 6 / elsevier, 2005, p. 461-470","order":488,"static_url":"/publications/412/"},{"section":"Publications","title":"Measurements of the flow over a low-aspect-ratio cylinder mounted on a ground plane","url":"/publications/45/","summary":"Pattenden, R. J.; Turnock, S. R.; Zhang, X.. “Measurements of the flow over a low-aspect-ratio cylinder mounted on a ground plane.” Experiments in Fluids, v. 39, (1), p. 10-21 (2005). DOI: 10.1007/s00348-005-0949-9.","meta":"Journal article · 2005","search_text":"measurements of the flow over a low-aspect-ratio cylinder mounted on a ground plane pattenden, r. j.; turnock, s. r.; zhang, x.. “measurements of the flow over a low-aspect-ratio cylinder mounted on a ground plane.” experiments in fluids, v. 39, (1), p. 10-21 (2005). doi: 10.1007/s00348-005-0949-9. journal article · 2005 pattenden, r. j.; turnock, s. r.; zhang, x. 2005 10.1007/s00348-005-0949-9 experiments in fluids, v. 39, (1), p. 10-21","order":489,"static_url":"/publications/45/"},{"section":"Publications","title":"Acoustic radiation from a semi-infinite duct with a subsonic jet","url":"/publications/44/","summary":"Chen, X.X.; Morfey, C.L.; Zhang, Xin. “Acoustic radiation from a semi-infinite duct with a subsonic jet.” International Journal of Aeroacoustics, v. 4, p. 169-184 (2005). DOI: 10.1260/1475472053730075.","meta":"Journal article · 2005","search_text":"acoustic radiation from a semi-infinite duct with a subsonic jet chen, x.x.; morfey, c.l.; zhang, xin. “acoustic radiation from a semi-infinite duct with a subsonic jet.” international journal of aeroacoustics, v. 4, p. 169-184 (2005). doi: 10.1260/1475472053730075. journal article · 2005 chen, x.x.; morfey, c.l.; zhang, xin 2005 10.1260/1475472053730075 international journal of aeroacoustics, v. 4, p. 169-184","order":490,"static_url":"/publications/44/"},{"section":"Publications","title":"Computational analysis of pressure and wake characteristics of an aerofoil in ground effect","url":"/publications/43/","summary":"Mahon, Stephen; Zhang, Xin. “Computational analysis of pressure and wake characteristics of an aerofoil in ground effect.” Journal of Fluids Engineering, Transactions of the ASME, v. 127, (2), p. 290-298 (2005). DOI: 10.1115/1.1891152.","meta":"Journal article · 2005","search_text":"computational analysis of pressure and wake characteristics of an aerofoil in ground effect mahon, stephen; zhang, xin. “computational analysis of pressure and wake characteristics of an aerofoil in ground effect.” journal of fluids engineering, transactions of the asme, v. 127, (2), p. 290-298 (2005). doi: 10.1115/1.1891152. journal article · 2005 mahon, stephen; zhang, xin 2005 10.1115/1.1891152 journal of fluids engineering, transactions of the asme, v. 127, (2), p. 290-298","order":491,"static_url":"/publications/43/"},{"section":"Publications","title":"Vortical structures over rectangular cavities at low speed","url":"/publications/42/","summary":"Ashcroft, Graham; Zhang, Xin. “Vortical structures over rectangular cavities at low speed.” Physics of Fluids, v. 17, (1), p. 015104-015104, article number 015104 (2005). DOI: 10.1063/1.1833412.","meta":"Journal article · 2005","search_text":"vortical structures over rectangular cavities at low speed ashcroft, graham; zhang, xin. “vortical structures over rectangular cavities at low speed.” physics of fluids, v. 17, (1), p. 015104-015104, article number 015104 (2005). doi: 10.1063/1.1833412. journal article · 2005 ashcroft, graham; zhang, xin 2005 10.1063/1.1833412 physics of fluids, v. 17, (1), p. 015104-015104, article number 015104","order":492,"static_url":"/publications/42/"},{"section":"Publications","title":"The evolution of edge vortices underneath a diffuser equipped bluff body","url":"/publications/451/","summary":"Mahon, S. Gage, C. and Zhang, X.. “The evolution of edge vortices underneath a diffuser equipped bluff body.” 12th International Symposium on Applications of Laser Techniques to Fluid Mechanics, pp. 1-10, 12-15 July 2004 (2004).","meta":"Conference paper · 2004","search_text":"the evolution of edge vortices underneath a diffuser equipped bluff body mahon, s. gage, c. and zhang, x.. “the evolution of edge vortices underneath a diffuser equipped bluff body.” 12th international symposium on applications of laser techniques to fluid mechanics, pp. 1-10, 12-15 july 2004 (2004). conference paper · 2004 mahon, s. gage, c. and zhang, x. 2004 12th international symposium on applications of laser techniques to fluid mechanics, pp. 1-10, 12-15 july 2004.","order":493,"static_url":"/publications/451/"},{"section":"Publications","title":"Numerical investigation of subsonic 2D/3D cavity flows","url":"/publications/422/","summary":"Bissessur, P.; Chen, X. X.; Zhang, X.. “Numerical investigation of subsonic 2D/3D cavity flows.” Paper presented at 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, United States, p. 1673-1685 (2004). DOI: 10.2514/6.2004-683.","meta":"Conference paper · 2004","search_text":"numerical investigation of subsonic 2d/3d cavity flows bissessur, p.; chen, x. x.; zhang, x.. “numerical investigation of subsonic 2d/3d cavity flows.” paper presented at 42nd aiaa aerospace sciences meeting and exhibit, reno, nv, united states, p. 1673-1685 (2004). doi: 10.2514/6.2004-683. conference paper · 2004 bissessur, p.; chen, x. x.; zhang, x. 2004 10.2514/6.2004-683 paper presented at 42nd aiaa aerospace sciences meeting and exhibit, reno, nv, united states, p. 1673-1685","order":494,"static_url":"/publications/422/"},{"section":"Publications","title":"Edge vortices of a double element wing in ground effect","url":"/publications/421/","summary":"Zhang, Xin; Zerihan, Jonathan. “Edge vortices of a double element wing in ground effect.” Paper presented at 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, United States, p. 9935-9949 (2004). DOI: 10.2514/6.2004-1240.","meta":"Conference paper · 2004","search_text":"edge vortices of a double element wing in ground effect zhang, xin; zerihan, jonathan. “edge vortices of a double element wing in ground effect.” paper presented at 42nd aiaa aerospace sciences meeting and exhibit, reno, nv, united states, p. 9935-9949 (2004). doi: 10.2514/6.2004-1240. conference paper · 2004 zhang, xin; zerihan, jonathan 2004 10.2514/6.2004-1240 paper presented at 42nd aiaa aerospace sciences meeting and exhibit, reno, nv, united states, p. 9935-9949","order":495,"static_url":"/publications/421/"},{"section":"Publications","title":"Computation of mode radiation from a generic aeroengine intake","url":"/publications/420/","summary":"Richards, Simon K.; Chen, Xiaoxian; Zhang, Xin. “Computation of mode radiation from a generic aeroengine intake.” Paper presented at European Congress on Computational Methods in Applied Sciences and Engineering, ECCOMAS 2004, Jyvaskyla, Finland (2004).","meta":"Conference paper · 2004","search_text":"computation of mode radiation from a generic aeroengine intake richards, simon k.; chen, xiaoxian; zhang, xin. “computation of mode radiation from a generic aeroengine intake.” paper presented at european congress on computational methods in applied sciences and engineering, eccomas 2004, jyvaskyla, finland (2004). conference paper · 2004 richards, simon k.; chen, xiaoxian; zhang, xin 2004 paper presented at european congress on computational methods in applied sciences and engineering, eccomas 2004, jyvaskyla, finland","order":496,"static_url":"/publications/420/"},{"section":"Publications","title":"Acoustic radiation computation from an engine inlet with aerodynamic flow field","url":"/publications/419/","summary":"Richards, S. K.; Zhang, X.; Chen, X. X.. “Acoustic radiation computation from an engine inlet with aerodynamic flow field.” Paper presented at 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, United States, p. 9527-9538 (2004). DOI: 10.2514/6.2004-848.","meta":"Conference paper · 2004","search_text":"acoustic radiation computation from an engine inlet with aerodynamic flow field richards, s. k.; zhang, x.; chen, x. x.. “acoustic radiation computation from an engine inlet with aerodynamic flow field.” paper presented at 42nd aiaa aerospace sciences meeting and exhibit, reno, nv, united states, p. 9527-9538 (2004). doi: 10.2514/6.2004-848. conference paper · 2004 richards, s. k.; zhang, x.; chen, x. x. 2004 10.2514/6.2004-848 paper presented at 42nd aiaa aerospace sciences meeting and exhibit, reno, nv, united states, p. 9527-9538","order":497,"static_url":"/publications/419/"},{"section":"Publications","title":"The evaluation of non-reflecting boundary conditions for duct acoustic computation","url":"/publications/418/","summary":"Richards, S. K.; Zhang, X.; Chen, X. X.; Nelson, P. A.. “The evaluation of non-reflecting boundary conditions for duct acoustic computation.” Journal of Sound and Vibration, v. 270, (3), p. 539-557 (2004). DOI: 10.1016/j.jsv.2003.09.042.","meta":"Journal article · 2004","search_text":"the evaluation of non-reflecting boundary conditions for duct acoustic computation richards, s. k.; zhang, x.; chen, x. x.; nelson, p. a.. “the evaluation of non-reflecting boundary conditions for duct acoustic computation.” journal of sound and vibration, v. 270, (3), p. 539-557 (2004). doi: 10.1016/j.jsv.2003.09.042. journal article · 2004 richards, s. k.; zhang, x.; chen, x. x.; nelson, p. a. 2004 10.1016/j.jsv.2003.09.042 journal of sound and vibration, v. 270, (3), p. 539-557","order":498,"static_url":"/publications/418/"},{"section":"Publications","title":"Journal of Sound and Vibration: Preface","url":"/publications/417/","summary":"Lai, C. H.; Nelson, P. A.; Zhang, X.. “Journal of Sound and Vibration: Preface.” Journal of Sound and Vibration, v. 270, (3), p. 481 (2004). DOI: 10.1016/j.jsv.2003.09.044.","meta":"Journal article · 2004","search_text":"journal of sound and vibration: preface lai, c. h.; nelson, p. a.; zhang, x.. “journal of sound and vibration: preface.” journal of sound and vibration, v. 270, (3), p. 481 (2004). doi: 10.1016/j.jsv.2003.09.044. journal article · 2004 lai, c. h.; nelson, p. a.; zhang, x. 2004 10.1016/j.jsv.2003.09.044 journal of sound and vibration, v. 270, (3), p. 481","order":499,"static_url":"/publications/417/"},{"section":"Publications","title":"Computation of spinning modal radiation from an unflanged duct","url":"/publications/41/","summary":"Zhang, X.; Chen, X. X.; Morfey, C. L.; Nelson, P. A.. “Computation of spinning modal radiation from an unflanged duct.” AIAA Journal, v. 42, (9), p. 1795-1801 (2004). DOI: 10.2514/1.890.","meta":"Journal article · 2004","search_text":"computation of spinning modal radiation from an unflanged duct zhang, x.; chen, x. x.; morfey, c. l.; nelson, p. a.. “computation of spinning modal radiation from an unflanged duct.” aiaa journal, v. 42, (9), p. 1795-1801 (2004). doi: 10.2514/1.890. journal article · 2004 zhang, x.; chen, x. x.; morfey, c. l.; nelson, p. a. 2004 10.2514/1.890 aiaa journal, v. 42, (9), p. 1795-1801","order":500,"static_url":"/publications/41/"},{"section":"Publications","title":"Edge vortices of a double-element wing in ground effect","url":"/publications/40/","summary":"Zhang, Xin; Zerihan, Jonathan. “Edge vortices of a double-element wing in ground effect.” Journal of Aircraft, v. 41, (5), p. 1127-1137 (2004). DOI: 10.2514/1.1380.","meta":"Journal article · 2004","search_text":"edge vortices of a double-element wing in ground effect zhang, xin; zerihan, jonathan. “edge vortices of a double-element wing in ground effect.” journal of aircraft, v. 41, (5), p. 1127-1137 (2004). doi: 10.2514/1.1380. journal article · 2004 zhang, xin; zerihan, jonathan 2004 10.2514/1.1380 journal of aircraft, v. 41, (5), p. 1127-1137","order":501,"static_url":"/publications/40/"},{"section":"Publications","title":"Vortices behind a bluff body with an upswept aft section in ground effect","url":"/publications/39/","summary":"Zhang, X.; Senior, A.; Ruhrmann, A.. “Vortices behind a bluff body with an upswept aft section in ground effect.” International Journal of Heat and Fluid Flow, v. 25, (1), p. 1-9 (2004). DOI: 10.1016/j.ijheatfluidflow.2003.11.002.","meta":"Journal article · 2004","search_text":"vortices behind a bluff body with an upswept aft section in ground effect zhang, x.; senior, a.; ruhrmann, a.. “vortices behind a bluff body with an upswept aft section in ground effect.” international journal of heat and fluid flow, v. 25, (1), p. 1-9 (2004). doi: 10.1016/j.ijheatfluidflow.2003.11.002. journal article · 2004 zhang, x.; senior, a.; ruhrmann, a. 2004 10.1016/j.ijheatfluidflow.2003.11.002 international journal of heat and fluid flow, v. 25, (1), p. 1-9","order":502,"static_url":"/publications/39/"},{"section":"Publications","title":"Time accurate numerical study of turbulent supersonic jets","url":"/publications/38/","summary":"Rona, A.; Zhang, X.. “Time accurate numerical study of turbulent supersonic jets.” Journal of Sound and Vibration, v. 270, (1-2), p. 297-321 (2004). DOI: 10.1016/s0022-460x(03)00537-6.","meta":"Journal article · 2004","search_text":"time accurate numerical study of turbulent supersonic jets rona, a.; zhang, x.. “time accurate numerical study of turbulent supersonic jets.” journal of sound and vibration, v. 270, (1-2), p. 297-321 (2004). doi: 10.1016/s0022-460x(03)00537-6. journal article · 2004 rona, a.; zhang, x. 2004 10.1016/s0022-460x(03)00537-6 journal of sound and vibration, v. 270, (1-2), p. 297-321","order":503,"static_url":"/publications/38/"},{"section":"Publications","title":"Computational aeroacoustic simulations of leading-edge slat flow","url":"/publications/37/","summary":"Takeda, K.; Zhang, X.; Nelson, P. A.. “Computational aeroacoustic simulations of leading-edge slat flow.” Journal of Sound and Vibration, v. 270, (3), p. 559-572 (2004). DOI: 10.1016/j.jsv.2003.09.046.","meta":"Journal article · 2004","search_text":"computational aeroacoustic simulations of leading-edge slat flow takeda, k.; zhang, x.; nelson, p. a.. “computational aeroacoustic simulations of leading-edge slat flow.” journal of sound and vibration, v. 270, (3), p. 559-572 (2004). doi: 10.1016/j.jsv.2003.09.046. journal article · 2004 takeda, k.; zhang, x.; nelson, p. a. 2004 10.1016/j.jsv.2003.09.046 journal of sound and vibration, v. 270, (3), p. 559-572","order":504,"static_url":"/publications/37/"},{"section":"Publications","title":"The evaluation of a buffer zone as an inflow/outflow boundary condition for computational aeroacoustic applications","url":"/publications/36/","summary":"Nelson, P.A.; Richards, S.; Zhang, Xin. “The evaluation of a buffer zone as an inflow/outflow boundary condition for computational aeroacoustic applications.” Journal of Sound and Vibration, v. 270, p. 539-557 (2004).","meta":"Journal article · 2004","search_text":"the evaluation of a buffer zone as an inflow/outflow boundary condition for computational aeroacoustic applications nelson, p.a.; richards, s.; zhang, xin. “the evaluation of a buffer zone as an inflow/outflow boundary condition for computational aeroacoustic applications.” journal of sound and vibration, v. 270, p. 539-557 (2004). journal article · 2004 nelson, p.a.; richards, s.; zhang, xin 2004 journal of sound and vibration, v. 270, p. 539-557","order":505,"static_url":"/publications/36/"},{"section":"Publications","title":"A numerical method for computation of sound radiation from an unflanged duct","url":"/publications/35/","summary":"Chen, X. X.; Zhang, X.; Morfey, C. L.; Nelson, P. A.. “A numerical method for computation of sound radiation from an unflanged duct.” Journal of Sound and Vibration, v. 270, (3), p. 573-586 (2004). DOI: 10.1016/j.jsv.2003.09.055.","meta":"Journal article · 2004","search_text":"a numerical method for computation of sound radiation from an unflanged duct chen, x. x.; zhang, x.; morfey, c. l.; nelson, p. a.. “a numerical method for computation of sound radiation from an unflanged duct.” journal of sound and vibration, v. 270, (3), p. 573-586 (2004). doi: 10.1016/j.jsv.2003.09.055. journal article · 2004 chen, x. x.; zhang, x.; morfey, c. l.; nelson, p. a. 2004 10.1016/j.jsv.2003.09.055 journal of sound and vibration, v. 270, (3), p. 573-586","order":506,"static_url":"/publications/35/"},{"section":"Publications","title":"Linearized Euler simulations of leading-edge slat flow","url":"/publications/424/","summary":"Takeda, K.; Zhang, X.; Nelson, P. A.. “Linearized Euler simulations of leading-edge slat flow.” 41st Aerospace Sciences Meeting and Exhibit, American Institute of Aeronautics and Astronautics Inc., 2003, (2003). DOI: 10.2514/6.2003-364.","meta":"Conference paper · 2003","search_text":"linearized euler simulations of leading-edge slat flow takeda, k.; zhang, x.; nelson, p. a.. “linearized euler simulations of leading-edge slat flow.” 41st aerospace sciences meeting and exhibit, american institute of aeronautics and astronautics inc., 2003, (2003). doi: 10.2514/6.2003-364. conference paper · 2003 takeda, k.; zhang, x.; nelson, p. a. 2003 10.2514/6.2003-364 41st aerospace sciences meeting and exhibit, american institute of aeronautics and astronautics inc., 2003,","order":507,"static_url":"/publications/424/"},{"section":"Publications","title":"Computation of fan noise radiation through a realistic engine exhaust geometry with flow","url":"/publications/423/","summary":"Zhang, X.; Chen, X. X.; Morfey, C. L.; Tester, B. J.. “Computation of fan noise radiation through a realistic engine exhaust geometry with flow.” 9th AIAA/CEAS Aeroacoustics Conference and Exhibit, 2003, (2003). DOI: 10.2514/6.2003-3267.","meta":"Conference paper · 2003","search_text":"computation of fan noise radiation through a realistic engine exhaust geometry with flow zhang, x.; chen, x. x.; morfey, c. l.; tester, b. j.. “computation of fan noise radiation through a realistic engine exhaust geometry with flow.” 9th aiaa/ceas aeroacoustics conference and exhibit, 2003, (2003). doi: 10.2514/6.2003-3267. conference paper · 2003 zhang, x.; chen, x. x.; morfey, c. l.; tester, b. j. 2003 10.2514/6.2003-3267 9th aiaa/ceas aeroacoustics conference and exhibit, 2003,","order":508,"static_url":"/publications/423/"},{"section":"Publications","title":"The evolution of co-rotating vortices in a canonical boundary layer with inclined jets","url":"/publications/34/","summary":"Zhang, Xin. “The evolution of co-rotating vortices in a canonical boundary layer with inclined jets.” Physics of Fluids, v. 15, (12), p. 3693-3702 (2003). DOI: 10.1063/1.1624609.","meta":"Journal article · 2003","search_text":"the evolution of co-rotating vortices in a canonical boundary layer with inclined jets zhang, xin. “the evolution of co-rotating vortices in a canonical boundary layer with inclined jets.” physics of fluids, v. 15, (12), p. 3693-3702 (2003). doi: 10.1063/1.1624609. journal article · 2003 zhang, xin 2003 10.1063/1.1624609 physics of fluids, v. 15, (12), p. 3693-3702","order":509,"static_url":"/publications/34/"},{"section":"Publications","title":"Off-surface aerodynamic measurements of a wing in ground effect","url":"/publications/33/","summary":"Zhang, Xin; Zerihan, Jonathan. “Off-surface aerodynamic measurements of a wing in ground effect.” Journal of Aircraft, v. 40, (4), p. 716-725 (2003). DOI: 10.2514/2.3150.","meta":"Journal article · 2003","search_text":"off-surface aerodynamic measurements of a wing in ground effect zhang, xin; zerihan, jonathan. “off-surface aerodynamic measurements of a wing in ground effect.” journal of aircraft, v. 40, (4), p. 716-725 (2003). doi: 10.2514/2.3150. journal article · 2003 zhang, xin; zerihan, jonathan 2003 10.2514/2.3150 journal of aircraft, v. 40, (4), p. 716-725","order":510,"static_url":"/publications/33/"},{"section":"Publications","title":"Influence of diffuser angle on a bluff body in ground effect","url":"/publications/32/","summary":"Ruhrmann, Andreas; Zhang, Xin. “Influence of diffuser angle on a bluff body in ground effect.” Journal of Fluids Engineering, Transactions of the ASME, v. 125, (2), p. 332-338 (2003). DOI: 10.1115/1.1537252.","meta":"Journal article · 2003","search_text":"influence of diffuser angle on a bluff body in ground effect ruhrmann, andreas; zhang, xin. “influence of diffuser angle on a bluff body in ground effect.” journal of fluids engineering, transactions of the asme, v. 125, (2), p. 332-338 (2003). doi: 10.1115/1.1537252. journal article · 2003 ruhrmann, andreas; zhang, xin 2003 10.1115/1.1537252 journal of fluids engineering, transactions of the asme, v. 125, (2), p. 332-338","order":511,"static_url":"/publications/32/"},{"section":"Publications","title":"A numerical investigation of the noise radiated by a turbulent flow over a cavity","url":"/publications/31/","summary":"Ashcroft, G. B.; Takeda, K.; Zhang, X.. “A numerical investigation of the noise radiated by a turbulent flow over a cavity.” Journal of Sound and Vibration, v. 265, (1), p. 43-60 (2003). DOI: 10.1016/s0022-460x(02)01439-6.","meta":"Journal article · 2003","search_text":"a numerical investigation of the noise radiated by a turbulent flow over a cavity ashcroft, g. b.; takeda, k.; zhang, x.. “a numerical investigation of the noise radiated by a turbulent flow over a cavity.” journal of sound and vibration, v. 265, (1), p. 43-60 (2003). doi: 10.1016/s0022-460x(02)01439-6. journal article · 2003 ashcroft, g. b.; takeda, k.; zhang, x. 2003 10.1016/s0022-460x(02)01439-6 journal of sound and vibration, v. 265, (1), p. 43-60","order":512,"static_url":"/publications/31/"},{"section":"Publications","title":"Aerodynamics of a double-element wing in ground effect","url":"/publications/30/","summary":"Zhang, Xin; Zerihan, Jonathan. “Aerodynamics of a double-element wing in ground effect.” AIAA Journal, v. 41, (6), p. 1007-1016 (2003). DOI: 10.2514/2.2057.","meta":"Journal article · 2003","search_text":"aerodynamics of a double-element wing in ground effect zhang, xin; zerihan, jonathan. “aerodynamics of a double-element wing in ground effect.” aiaa journal, v. 41, (6), p. 1007-1016 (2003). doi: 10.2514/2.2057. journal article · 2003 zhang, xin; zerihan, jonathan 2003 10.2514/2.2057 aiaa journal, v. 41, (6), p. 1007-1016","order":513,"static_url":"/publications/30/"},{"section":"Publications","title":"Optimized prefactored compact schemes","url":"/publications/29/","summary":"Ashcroft, Graham; Zhang, Xin. “Optimized prefactored compact schemes.” Journal of Computational Physics, v. 190, (2), p. 459-477 (2003). DOI: 10.1016/s0021-9991(03)00293-6.","meta":"Journal article · 2003","search_text":"optimized prefactored compact schemes ashcroft, graham; zhang, xin. “optimized prefactored compact schemes.” journal of computational physics, v. 190, (2), p. 459-477 (2003). doi: 10.1016/s0021-9991(03)00293-6. journal article · 2003 ashcroft, graham; zhang, xin 2003 10.1016/s0021-9991(03)00293-6 journal of computational physics, v. 190, (2), p. 459-477","order":514,"static_url":"/publications/29/"},{"section":"Publications","title":"Tip vortices generated by a wing in ground effect","url":"/publications/453/","summary":"Zhang, X., Zerihan, J., Ruhrmann A. and Deviese, M.. “Tip vortices generated by a wing in ground effect.” The 11th International Symposium on Applications of Laser Techniques to Fluid Mechanics, Lisbon, Portugal, 8-10 July 2002 (2002).","meta":"Conference paper · 2002","search_text":"tip vortices generated by a wing in ground effect zhang, x., zerihan, j., ruhrmann a. and deviese, m.. “tip vortices generated by a wing in ground effect.” the 11th international symposium on applications of laser techniques to fluid mechanics, lisbon, portugal, 8-10 july 2002 (2002). conference paper · 2002 zhang, x., zerihan, j., ruhrmann a. and deviese, m. 2002 the 11th international symposium on applications of laser techniques to fluid mechanics, lisbon, portugal, 8-10 july 2002.","order":515,"static_url":"/publications/453/"},{"section":"Publications","title":"A numerical method for noise radiation from an unflanged duct","url":"/publications/452/","summary":"Chen, X., Zhang, X., Morfey, C.L. and Nelson, P.A.. “A numerical method for noise radiation from an unflanged duct.” IMA Conference on Computational Aeroacoustics, Greenwich, UK, 9-11 April 2002 (2002).","meta":"Conference paper · 2002","search_text":"a numerical method for noise radiation from an unflanged duct chen, x., zhang, x., morfey, c.l. and nelson, p.a.. “a numerical method for noise radiation from an unflanged duct.” ima conference on computational aeroacoustics, greenwich, uk, 9-11 april 2002 (2002). conference paper · 2002 chen, x., zhang, x., morfey, c.l. and nelson, p.a. 2002 ima conference on computational aeroacoustics, greenwich, uk, 9-11 april 2002.","order":516,"static_url":"/publications/452/"},{"section":"Publications","title":"Unsteady aerodynamics and aeroacoustics of a high-lift device configuration","url":"/publications/426/","summary":"Takeda, K.; Zhang, X.; Nelson, P. A.. “Unsteady aerodynamics and aeroacoustics of a high-lift device configuration.” Paper presented at 40th AIAA Aerospace Sciences Meeting and Exhibit 2002, Reno, NV, United States (2002). DOI: 10.2514/6.2002-570.","meta":"Conference paper · 2002","search_text":"unsteady aerodynamics and aeroacoustics of a high-lift device configuration takeda, k.; zhang, x.; nelson, p. a.. “unsteady aerodynamics and aeroacoustics of a high-lift device configuration.” paper presented at 40th aiaa aerospace sciences meeting and exhibit 2002, reno, nv, united states (2002). doi: 10.2514/6.2002-570. conference paper · 2002 takeda, k.; zhang, x.; nelson, p. a. 2002 10.2514/6.2002-570 paper presented at 40th aiaa aerospace sciences meeting and exhibit 2002, reno, nv, united states","order":517,"static_url":"/publications/426/"},{"section":"Publications","title":"Aerodynamics of a double element wing in ground effect","url":"/publications/425/","summary":"Zhang, Xin; Zerihan, Jonathan. “Aerodynamics of a double element wing in ground effect.” Paper presented at 40th AIAA Aerospace Sciences Meeting and Exhibit 2002, Reno, NV, United States (2002). DOI: 10.2514/6.2002-834.","meta":"Conference paper · 2002","search_text":"aerodynamics of a double element wing in ground effect zhang, xin; zerihan, jonathan. “aerodynamics of a double element wing in ground effect.” paper presented at 40th aiaa aerospace sciences meeting and exhibit 2002, reno, nv, united states (2002). doi: 10.2514/6.2002-834. conference paper · 2002 zhang, xin; zerihan, jonathan 2002 10.2514/6.2002-834 paper presented at 40th aiaa aerospace sciences meeting and exhibit 2002, reno, nv, united states","order":518,"static_url":"/publications/425/"},{"section":"Publications","title":"Unsteady aerodynamics of slat cove flow in a high-lift device configuration","url":"/publications/431/","summary":"Takeda, K.; Ashcroft, G. B.; Zhang, X.; Nelson, P. A.. “Unsteady aerodynamics of slat cove flow in a high-lift device configuration.” Paper presented at 39th Aerospace Sciences Meeting and Exhibit 2001, Reno, NV, United States (2001). DOI: 10.2514/6.2001-706.","meta":"Conference paper · 2001","search_text":"unsteady aerodynamics of slat cove flow in a high-lift device configuration takeda, k.; ashcroft, g. b.; zhang, x.; nelson, p. a.. “unsteady aerodynamics of slat cove flow in a high-lift device configuration.” paper presented at 39th aerospace sciences meeting and exhibit 2001, reno, nv, united states (2001). doi: 10.2514/6.2001-706. conference paper · 2001 takeda, k.; ashcroft, g. b.; zhang, x.; nelson, p. a. 2001 10.2514/6.2001-706 paper presented at 39th aerospace sciences meeting and exhibit 2001, reno, nv, united states","order":519,"static_url":"/publications/431/"},{"section":"Publications","title":"Unsteady aerodynamics of flap cove flow in a high-lift device configuration","url":"/publications/430/","summary":"Takeda, K.; Ashcroft, G. B.; Zhang, X.; Nelson, P. A.. “Unsteady aerodynamics of flap cove flow in a high-lift device configuration.” Paper presented at 39th Aerospace Sciences Meeting and Exhibit 2001, Reno, NV, United States (2001). DOI: 10.2514/6.2001-707.","meta":"Conference paper · 2001","search_text":"unsteady aerodynamics of flap cove flow in a high-lift device configuration takeda, k.; ashcroft, g. b.; zhang, x.; nelson, p. a.. “unsteady aerodynamics of flap cove flow in a high-lift device configuration.” paper presented at 39th aerospace sciences meeting and exhibit 2001, reno, nv, united states (2001). doi: 10.2514/6.2001-707. conference paper · 2001 takeda, k.; ashcroft, g. b.; zhang, x.; nelson, p. a. 2001 10.2514/6.2001-707 paper presented at 39th aerospace sciences meeting and exhibit 2001, reno, nv, united states","order":520,"static_url":"/publications/430/"},{"section":"Publications","title":"A single element wing in ground effect; comparisons of experiments and computation","url":"/publications/429/","summary":"Zerihan, Jonathan; Zhang, Xin. “A single element wing in ground effect; comparisons of experiments and computation.” Paper presented at 39th Aerospace Sciences Meeting and Exhibit 2001, Reno, NV, United States (2001). DOI: 10.2514/6.2001-423.","meta":"Conference paper · 2001","search_text":"a single element wing in ground effect; comparisons of experiments and computation zerihan, jonathan; zhang, xin. “a single element wing in ground effect; comparisons of experiments and computation.” paper presented at 39th aerospace sciences meeting and exhibit 2001, reno, nv, united states (2001). doi: 10.2514/6.2001-423. conference paper · 2001 zerihan, jonathan; zhang, xin 2001 10.2514/6.2001-423 paper presented at 39th aerospace sciences meeting and exhibit 2001, reno, nv, united states","order":521,"static_url":"/publications/429/"},{"section":"Publications","title":"A computational investigation of the noise radiated by flow-induced cavity oscillations","url":"/publications/428/","summary":"Ashcroft, Graham; Zhang, Xin. “A computational investigation of the noise radiated by flow-induced cavity oscillations.” Paper presented at 39th Aerospace Sciences Meeting and Exhibit 2001, Reno, NV, United States (2001). DOI: 10.2514/6.2001-512.","meta":"Conference paper · 2001","search_text":"a computational investigation of the noise radiated by flow-induced cavity oscillations ashcroft, graham; zhang, xin. “a computational investigation of the noise radiated by flow-induced cavity oscillations.” paper presented at 39th aerospace sciences meeting and exhibit 2001, reno, nv, united states (2001). doi: 10.2514/6.2001-512. conference paper · 2001 ashcroft, graham; zhang, xin 2001 10.2514/6.2001-512 paper presented at 39th aerospace sciences meeting and exhibit 2001, reno, nv, united states","order":522,"static_url":"/publications/428/"},{"section":"Publications","title":"Aerodynamics of Gurney flaps on a wing in ground effect","url":"/publications/427/","summary":"Zerihan, Jonathan; Zhang, Xin. “Aerodynamics of Gurney flaps on a wing in ground effect.” AIAA Journal, v. 39, (5), p. 772-780 (2001). DOI: 10.2514/2.1396.","meta":"Journal article · 2001","search_text":"aerodynamics of gurney flaps on a wing in ground effect zerihan, jonathan; zhang, xin. “aerodynamics of gurney flaps on a wing in ground effect.” aiaa journal, v. 39, (5), p. 772-780 (2001). doi: 10.2514/2.1396. journal article · 2001 zerihan, jonathan; zhang, xin 2001 10.2514/2.1396 aiaa journal, v. 39, (5), p. 772-780","order":523,"static_url":"/publications/427/"},{"section":"Publications","title":"Aerodynamics of gurney flaps on a wing in ground effect","url":"/publications/28/","summary":"Zhang, X. & Zerihan, J., \"Aerodynamics of Gurney flaps on a wing in ground effect,\" AIAA Journal, Vol. 39, No. 5, May 2001, pp. 772-780.","meta":"Journal article · 2001","search_text":"aerodynamics of gurney flaps on a wing in ground effect zhang, x. & zerihan, j., \"aerodynamics of gurney flaps on a wing in ground effect,\" aiaa journal, vol. 39, no. 5, may 2001, pp. 772-780. journal article · 2001 jonathan zerihan; xin zhang 2001 10.2514/3.14801 aiaa journal 39 772-780","order":524,"static_url":"/publications/28/"},{"section":"Publications","title":"The force and pressure of a diffuser-equipped bluff body in ground effect","url":"/publications/27/","summary":"Senior, Andrea E.; Zhang, Xin. “The force and pressure of a diffuser-equipped bluff body in ground effect.” Journal of Fluids Engineering, Transactions of the ASME, v. 123, (1), p. 105-111 (2001). DOI: 10.1115/1.1340637.","meta":"Journal article · 2001","search_text":"the force and pressure of a diffuser-equipped bluff body in ground effect senior, andrea e.; zhang, xin. “the force and pressure of a diffuser-equipped bluff body in ground effect.” journal of fluids engineering, transactions of the asme, v. 123, (1), p. 105-111 (2001). doi: 10.1115/1.1340637. journal article · 2001 senior, andrea e.; zhang, xin 2001 10.1115/1.1340637 journal of fluids engineering, transactions of the asme, v. 123, (1), p. 105-111","order":525,"static_url":"/publications/27/"},{"section":"Publications","title":"Some aspects of the aerodynamics of gurney flaps on a double-element wing","url":"/publications/26/","summary":"Jeffrey, David; Zhang, Xin; Hurst, David W.. “Some aspects of the aerodynamics of gurney flaps on a double-element wing.” Journal of Fluids Engineering, Transactions of the ASME, v. 123, (1), p. 99-104 (2001). DOI: 10.1115/1.1334376.","meta":"Journal article · 2001","search_text":"some aspects of the aerodynamics of gurney flaps on a double-element wing jeffrey, david; zhang, xin; hurst, david w.. “some aspects of the aerodynamics of gurney flaps on a double-element wing.” journal of fluids engineering, transactions of the asme, v. 123, (1), p. 99-104 (2001). doi: 10.1115/1.1334376. journal article · 2001 jeffrey, david; zhang, xin; hurst, david w. 2001 10.1115/1.1334376 journal of fluids engineering, transactions of the asme, v. 123, (1), p. 99-104","order":526,"static_url":"/publications/26/"},{"section":"Publications","title":"A computational investigation of the far-field noise radiated by the unsteady flow over a cavity","url":"/publications/456/","summary":"Ashcroft, G. and Zhang, X.. “A computational investigation of the far-field noise radiated by the unsteady flow over a cavity.” The 3rd MIRA international conference on vehicle aerodynamics, Rugby, U.K, 18-19 October 2000 (2000).","meta":"Conference paper · 2000","search_text":"a computational investigation of the far-field noise radiated by the unsteady flow over a cavity ashcroft, g. and zhang, x.. “a computational investigation of the far-field noise radiated by the unsteady flow over a cavity.” the 3rd mira international conference on vehicle aerodynamics, rugby, u.k, 18-19 october 2000 (2000). conference paper · 2000 ashcroft, g. and zhang, x. 2000 the 3rd mira international conference on vehicle aerodynamics, rugby, u.k, 18-19 october 2000.","order":527,"static_url":"/publications/456/"},{"section":"Publications","title":"Unsteady turbulent wake behind a single-element wing in ground effect","url":"/publications/455/","summary":"Zhang, X. and Zerihan, J.. “Unsteady turbulent wake behind a single-element wing in ground effect.” The 10th International Symposium on Applications of Laser Techniques to Fluid Mechanics, Lisbon, Portugal, 10-13 July 2000 (2000).","meta":"Conference paper · 2000","search_text":"unsteady turbulent wake behind a single-element wing in ground effect zhang, x. and zerihan, j.. “unsteady turbulent wake behind a single-element wing in ground effect.” the 10th international symposium on applications of laser techniques to fluid mechanics, lisbon, portugal, 10-13 july 2000 (2000). conference paper · 2000 zhang, x. and zerihan, j. 2000 the 10th international symposium on applications of laser techniques to fluid mechanics, lisbon, portugal, 10-13 july 2000.","order":528,"static_url":"/publications/455/"},{"section":"Publications","title":"Computational modelling of the aeroacoustics of a door cavity flow oscillation","url":"/publications/454/","summary":"Ashcroft, G., Takeda, K. and Zhang, X.. “Computational modelling of the aeroacoustics of a door cavity flow oscillation.” The 7th International Congress on Sound and Vibration, Garmisch-Partenkirchen, 4-7 July 2000 (2000).","meta":"Conference paper · 2000","search_text":"computational modelling of the aeroacoustics of a door cavity flow oscillation ashcroft, g., takeda, k. and zhang, x.. “computational modelling of the aeroacoustics of a door cavity flow oscillation.” the 7th international congress on sound and vibration, garmisch-partenkirchen, 4-7 july 2000 (2000). conference paper · 2000 ashcroft, g., takeda, k. and zhang, x. 2000 the 7th international congress on sound and vibration, garmisch-partenkirchen, 4-7 july 2000.","order":529,"static_url":"/publications/454/"},{"section":"Publications","title":"Force enhancement of gurney flaps on a wing in ground effect","url":"/publications/433/","summary":"Zerihan, Jonathan; Zhang, Xin. “Force enhancement of gurney flaps on a wing in ground effect.” Paper presented at Fluids 2000 Conference and Exhibit, Denver, CO, United States (2000). DOI: 10.2514/6.2000-2241.","meta":"Conference paper · 2000","search_text":"force enhancement of gurney flaps on a wing in ground effect zerihan, jonathan; zhang, xin. “force enhancement of gurney flaps on a wing in ground effect.” paper presented at fluids 2000 conference and exhibit, denver, co, united states (2000). doi: 10.2514/6.2000-2241. conference paper · 2000 zerihan, jonathan; zhang, xin 2000 10.2514/6.2000-2241 paper presented at fluids 2000 conference and exhibit, denver, co, united states","order":530,"static_url":"/publications/433/"},{"section":"Publications","title":"An experimental study of a diffuser in ground effect","url":"/publications/432/","summary":"Senior, Andrea; Zhang, Xin. “An experimental study of a diffuser in ground effect.” Paper presented at 38th Aerospace Sciences Meeting and Exhibit 2000, Reno, NV, United States (2000). DOI: 10.2514/6.2000-118.","meta":"Conference paper · 2000","search_text":"an experimental study of a diffuser in ground effect senior, andrea; zhang, xin. “an experimental study of a diffuser in ground effect.” paper presented at 38th aerospace sciences meeting and exhibit 2000, reno, nv, united states (2000). doi: 10.2514/6.2000-118. conference paper · 2000 senior, andrea; zhang, xin 2000 10.2514/6.2000-118 paper presented at 38th aerospace sciences meeting and exhibit 2000, reno, nv, united states","order":531,"static_url":"/publications/432/"},{"section":"Publications","title":"Aerodynamics of a single element wing in ground effect","url":"/publications/25/","summary":"Zerihan, Jonathan; Zhang, Xin. “Aerodynamics of a single element wing in ground effect.” Journal of Aircraft, v. 37, (6), p. 1058-1064 (2000). DOI: 10.2514/2.2711.","meta":"Journal article · 2000","search_text":"aerodynamics of a single element wing in ground effect zerihan, jonathan; zhang, xin. “aerodynamics of a single element wing in ground effect.” journal of aircraft, v. 37, (6), p. 1058-1064 (2000). doi: 10.2514/2.2711. journal article · 2000 zerihan, jonathan; zhang, xin 2000 10.2514/2.2711 journal of aircraft, v. 37, (6), p. 1058-1064","order":532,"static_url":"/publications/25/"},{"section":"Publications","title":"Turbulence measurements of an inclined rectangular jet embedded in a turbulent boundary layer","url":"/publications/24/","summary":"Zhang, Xin. “Turbulence measurements of an inclined rectangular jet embedded in a turbulent boundary layer.” International Journal of Heat and Fluid Flow, v. 21, (3), p. 291-296 (2000). DOI: 10.1016/s0142-727x(00)00012-6.","meta":"Journal article · 2000","search_text":"turbulence measurements of an inclined rectangular jet embedded in a turbulent boundary layer zhang, xin. “turbulence measurements of an inclined rectangular jet embedded in a turbulent boundary layer.” international journal of heat and fluid flow, v. 21, (3), p. 291-296 (2000). doi: 10.1016/s0142-727x(00)00012-6. journal article · 2000 zhang, xin 2000 10.1016/s0142-727x(00)00012-6 international journal of heat and fluid flow, v. 21, (3), p. 291-296","order":533,"static_url":"/publications/24/"},{"section":"Publications","title":"An inclined rectangular jet in a turbulent boundary layer-vortex flow","url":"/publications/23/","summary":"Zhang, X.. “An inclined rectangular jet in a turbulent boundary layer-vortex flow.” Experiments in Fluids, v. 28, (4), p. 344-354 (2000). DOI: 10.1007/s003480050393.","meta":"Journal article · 2000","search_text":"an inclined rectangular jet in a turbulent boundary layer-vortex flow zhang, x.. “an inclined rectangular jet in a turbulent boundary layer-vortex flow.” experiments in fluids, v. 28, (4), p. 344-354 (2000). doi: 10.1007/s003480050393. journal article · 2000 zhang, x. 2000 10.1007/s003480050393 experiments in fluids, v. 28, (4), p. 344-354","order":534,"static_url":"/publications/23/"},{"section":"Publications","title":"Aerodynamics of Gurney flaps on a single-element high-lift wing","url":"/publications/22/","summary":"Jeffrey, David; Zhang, Xin; Hurst, David W.. “Aerodynamics of Gurney flaps on a single-element high-lift wing.” Journal of Aircraft, v. 37, (2), p. 295-301 (2000). DOI: 10.2514/2.2593.","meta":"Journal article · 2000","search_text":"aerodynamics of gurney flaps on a single-element high-lift wing jeffrey, david; zhang, xin; hurst, david w.. “aerodynamics of gurney flaps on a single-element high-lift wing.” journal of aircraft, v. 37, (2), p. 295-301 (2000). doi: 10.2514/2.2593. journal article · 2000 jeffrey, david; zhang, xin; hurst, david w. 2000 10.2514/2.2593 journal of aircraft, v. 37, (2), p. 295-301","order":535,"static_url":"/publications/22/"},{"section":"Publications","title":"Computations of self-sustained oscillatory flow in an automobile door cavity","url":"/publications/458/","summary":"Ashcroft, G.B., Takeda, K, and Zhang, X. “Computations of self-sustained oscillatory flow in an automobile door cavity.” Third Computational Aeroacoustics (CAA) Workshop on Benckmark Problems, Cleveland, U.S.A., 8-10 November 1999 (1999).","meta":"Conference paper · 1999","search_text":"computations of self-sustained oscillatory flow in an automobile door cavity ashcroft, g.b., takeda, k, and zhang, x. “computations of self-sustained oscillatory flow in an automobile door cavity.” third computational aeroacoustics (caa) workshop on benckmark problems, cleveland, u.s.a., 8-10 november 1999 (1999). conference paper · 1999 ashcroft, g.b., takeda, k, and zhang, x 1999 third computational aeroacoustics (caa) workshop on benckmark problems, cleveland, u.s.a., 8-10 november 1999.","order":536,"static_url":"/publications/458/"},{"section":"Publications","title":"Jet screech source model by CFD and acoustic analogy","url":"/publications/457/","summary":"Zhang, X. and Rona, A.. “Jet screech source model by CFD and acoustic analogy.” Proceedings of 3rd ASME/JSME Joint Fluids Engineering Conference, FEDSM99-7239, San Francisco, U.S.A., July 18-22 1999 (1999).","meta":"Conference paper · 1999","search_text":"jet screech source model by cfd and acoustic analogy zhang, x. and rona, a.. “jet screech source model by cfd and acoustic analogy.” proceedings of 3rd asme/jsme joint fluids engineering conference, fedsm99-7239, san francisco, u.s.a., july 18-22 1999 (1999). conference paper · 1999 zhang, x. and rona, a. 1999 proceedings of 3rd asme/jsme joint fluids engineering conference, fedsm99-7239, san francisco, u.s.a., july 18-22 1999.","order":537,"static_url":"/publications/457/"},{"section":"Publications","title":"Measurements of contra-rotating vortices in a turbulent boundary layer","url":"/publications/434/","summary":"Zhang, X.; Rona, A.. “Measurements of contra-rotating vortices in a turbulent boundary layer.” Paper presented at 37th Aerospace Sciences Meeting and Exhibit, 1999, Reno, United States (1999). DOI: 10.2514/6.1999-555.","meta":"Conference paper · 1999","search_text":"measurements of contra-rotating vortices in a turbulent boundary layer zhang, x.; rona, a.. “measurements of contra-rotating vortices in a turbulent boundary layer.” paper presented at 37th aerospace sciences meeting and exhibit, 1999, reno, united states (1999). doi: 10.2514/6.1999-555. conference paper · 1999 zhang, x.; rona, a. 1999 10.2514/6.1999-555 paper presented at 37th aerospace sciences meeting and exhibit, 1999, reno, united states","order":538,"static_url":"/publications/434/"},{"section":"Publications","title":"Counter-rotating vortices embedded in a turbulent boundary layer with inclined jets","url":"/publications/21/","summary":"Zhang, X.. “Counter-rotating vortices embedded in a turbulent boundary layer with inclined jets.” AIAA Journal, v. 37, (10), p. 1277-1284 (1999). DOI: 10.2514/2.596.","meta":"Journal article · 1999","search_text":"counter-rotating vortices embedded in a turbulent boundary layer with inclined jets zhang, x.. “counter-rotating vortices embedded in a turbulent boundary layer with inclined jets.” aiaa journal, v. 37, (10), p. 1277-1284 (1999). doi: 10.2514/2.596. journal article · 1999 zhang, x. 1999 10.2514/2.596 aiaa journal, v. 37, (10), p. 1277-1284","order":539,"static_url":"/publications/21/"},{"section":"Publications","title":"Attenuation of cavity flow oscillation through leading edge flow control","url":"/publications/20/","summary":"Zhang, X.; Chen, X. X.; Rona, A.; Edwards, J. A.. “Attenuation of cavity flow oscillation through leading edge flow control.” Journal of Sound and Vibration, v. 221, (1), p. 23-47 (1999). DOI: 10.1006/jsvi.1998.2012.","meta":"Journal article · 1999","search_text":"attenuation of cavity flow oscillation through leading edge flow control zhang, x.; chen, x. x.; rona, a.; edwards, j. a.. “attenuation of cavity flow oscillation through leading edge flow control.” journal of sound and vibration, v. 221, (1), p. 23-47 (1999). doi: 10.1006/jsvi.1998.2012. journal article · 1999 zhang, x.; chen, x. x.; rona, a.; edwards, j. a. 1999 10.1006/jsvi.1998.2012 journal of sound and vibration, v. 221, (1), p. 23-47","order":540,"static_url":"/publications/20/"},{"section":"Publications","title":"Pressure over a dual-cavity cascade at supersonic speeds","url":"/publications/19/","summary":"Zhang, X.; Edwards, J. A.. “Pressure over a dual-cavity cascade at supersonic speeds.” Aeronautical Journal, v. 103, (1019), p. 45-53, article number 2378 (1999). DOI: 10.1017/s000192400006509x.","meta":"Journal article · 1999","search_text":"pressure over a dual-cavity cascade at supersonic speeds zhang, x.; edwards, j. a.. “pressure over a dual-cavity cascade at supersonic speeds.” aeronautical journal, v. 103, (1019), p. 45-53, article number 2378 (1999). doi: 10.1017/s000192400006509x. journal article · 1999 zhang, x.; edwards, j. a. 1999 10.1017/s000192400006509x aeronautical journal, v. 103, (1019), p. 45-53, article number 2378","order":541,"static_url":"/publications/19/"},{"section":"Publications","title":"Some aspects of the time-averaged and unsteady aerodynamics of Gurney flaps","url":"/publications/460/","summary":"Jeffrey, D.R., Zhang, X. and Hurst, D.W.. “Some aspects of the time-averaged and unsteady aerodynamics of Gurney flaps.” The 1st MIRA international conference on vehicle aerodynamics, Birmingham, U.K., October 1998 (1998).","meta":"Conference paper · 1998","search_text":"some aspects of the time-averaged and unsteady aerodynamics of gurney flaps jeffrey, d.r., zhang, x. and hurst, d.w.. “some aspects of the time-averaged and unsteady aerodynamics of gurney flaps.” the 1st mira international conference on vehicle aerodynamics, birmingham, u.k., october 1998 (1998). conference paper · 1998 jeffrey, d.r., zhang, x. and hurst, d.w. 1998 the 1st mira international conference on vehicle aerodynamics, birmingham, u.k., october 1998.","order":542,"static_url":"/publications/460/"},{"section":"Publications","title":"Streamwise vortex production by an array of inclined jets","url":"/publications/459/","summary":"Zhang, X. and Rona, A.. “Streamwise vortex production by an array of inclined jets.” The 9th International Symposium on Applications of Laser Techniques to Fluid Mechanics, Lisbon, Portugal, July 13-16 1998 (1998).","meta":"Conference paper · 1998","search_text":"streamwise vortex production by an array of inclined jets zhang, x. and rona, a.. “streamwise vortex production by an array of inclined jets.” the 9th international symposium on applications of laser techniques to fluid mechanics, lisbon, portugal, july 13-16 1998 (1998). conference paper · 1998 zhang, x. and rona, a. 1998 the 9th international symposium on applications of laser techniques to fluid mechanics, lisbon, portugal, july 13-16 1998.","order":543,"static_url":"/publications/459/"},{"section":"Publications","title":"Control of cavity flow oscillation through leading edge flow modification","url":"/publications/435/","summary":"Ronat, A.; Ghent, X. X.; Zhang, X.; Edwards, J. A.. “Control of cavity flow oscillation through leading edge flow modification.” Paper presented at 36th AIAA Aerospace Sciences Meeting and Exhibit, 1998, Reno, United States (1998). DOI: 10.2514/6.1998-672.","meta":"Conference paper · 1998","search_text":"control of cavity flow oscillation through leading edge flow modification ronat, a.; ghent, x. x.; zhang, x.; edwards, j. a.. “control of cavity flow oscillation through leading edge flow modification.” paper presented at 36th aiaa aerospace sciences meeting and exhibit, 1998, reno, united states (1998). doi: 10.2514/6.1998-672. conference paper · 1998 ronat, a.; ghent, x. x.; zhang, x.; edwards, j. a. 1998 10.2514/6.1998-672 paper presented at 36th aiaa aerospace sciences meeting and exhibit, 1998, reno, united states","order":544,"static_url":"/publications/435/"},{"section":"Publications","title":"Turbulence measurements of a longitudinal vortex generated by an inclined jet in a turbulent boundary layer","url":"/publications/18/","summary":"Zhang, X.. “Turbulence measurements of a longitudinal vortex generated by an inclined jet in a turbulent boundary layer.” Journal of Fluids Engineering, Transactions of the ASME, v. 120, (4), p. 765-771 (1998). DOI: 10.1115/1.2820736.","meta":"Journal article · 1998","search_text":"turbulence measurements of a longitudinal vortex generated by an inclined jet in a turbulent boundary layer zhang, x.. “turbulence measurements of a longitudinal vortex generated by an inclined jet in a turbulent boundary layer.” journal of fluids engineering, transactions of the asme, v. 120, (4), p. 765-771 (1998). doi: 10.1115/1.2820736. journal article · 1998 zhang, x. 1998 10.1115/1.2820736 journal of fluids engineering, transactions of the asme, v. 120, (4), p. 765-771","order":545,"static_url":"/publications/18/"},{"section":"Publications","title":"The effect of trailing edge geometry on cavity flow oscillation driven by a supersonic shear layer","url":"/publications/17/","summary":"Zhang, X.; Rona, A.; Edwards, J. A.. “The effect of trailing edge geometry on cavity flow oscillation driven by a supersonic shear layer.” Aeronautical Journal, v. 102, (1013), p. 129-135 (1998). DOI: 10.1017/s0001924000065416.","meta":"Journal article · 1998","search_text":"the effect of trailing edge geometry on cavity flow oscillation driven by a supersonic shear layer zhang, x.; rona, a.; edwards, j. a.. “the effect of trailing edge geometry on cavity flow oscillation driven by a supersonic shear layer.” aeronautical journal, v. 102, (1013), p. 129-135 (1998). doi: 10.1017/s0001924000065416. journal article · 1998 zhang, x.; rona, a.; edwards, j. a. 1998 10.1017/s0001924000065416 aeronautical journal, v. 102, (1013), p. 129-135","order":546,"static_url":"/publications/17/"},{"section":"Publications","title":"An observation of pressure waves around a shallow cavity","url":"/publications/16/","summary":"Zhang, X.; Rona, A.; Edwards, J. A.. “An observation of pressure waves around a shallow cavity.” Journal of Sound and Vibration, v. 214, (4), p. 771-778 (1998). DOI: 10.1006/jsvi.1998.1635.","meta":"Journal article · 1998","search_text":"an observation of pressure waves around a shallow cavity zhang, x.; rona, a.; edwards, j. a.. “an observation of pressure waves around a shallow cavity.” journal of sound and vibration, v. 214, (4), p. 771-778 (1998). doi: 10.1006/jsvi.1998.1635. journal article · 1998 zhang, x.; rona, a.; edwards, j. a. 1998 10.1006/jsvi.1998.1635 journal of sound and vibration, v. 214, (4), p. 771-778","order":547,"static_url":"/publications/16/"},{"section":"Publications","title":"Streamwise vortex production by inclined jets and design guidelines","url":"/publications/462/","summary":"Zhang, X.. “Streamwise vortex production by inclined jets and design guidelines.” The 3rd Pacific International Conference on Aerospace Science and Technology, China, September 1997 (1997).","meta":"Conference paper · 1997","search_text":"streamwise vortex production by inclined jets and design guidelines zhang, x.. “streamwise vortex production by inclined jets and design guidelines.” the 3rd pacific international conference on aerospace science and technology, china, september 1997 (1997). conference paper · 1997 zhang, x. 1997 the 3rd pacific international conference on aerospace science and technology, china, september 1997.","order":548,"static_url":"/publications/462/"},{"section":"Publications","title":"A numerical study of fully and over-expanded Mach 2 jets","url":"/publications/461/","summary":"Zhang, X. and Rona, A.. “A numerical study of fully and over-expanded Mach 2 jets.” The 10th International Conference on Numerical Methods for Laminar and Turbulent Flow, Swansea, U.K., 28 July-1 August 1997 (1997).","meta":"Conference paper · 1997","search_text":"a numerical study of fully and over-expanded mach 2 jets zhang, x. and rona, a.. “a numerical study of fully and over-expanded mach 2 jets.” the 10th international conference on numerical methods for laminar and turbulent flow, swansea, u.k., 28 july-1 august 1997 (1997). conference paper · 1997 zhang, x. and rona, a. 1997 the 10th international conference on numerical methods for laminar and turbulent flow, swansea, u.k., 28 july-1 august 1997.","order":549,"static_url":"/publications/461/"},{"section":"Publications","title":"Turbulence measurements of a longitudinal vortex in a turbulent boundary layer","url":"/publications/436/","summary":"Zhang, X.; Collina, M. W.. “Turbulence measurements of a longitudinal vortex in a turbulent boundary layer.” Paper presented at 35th Aerospace Sciences Meeting and Exhibit, 1997, Reno, United States (1997). DOI: 10.2514/6.1997-654.","meta":"Conference paper · 1997","search_text":"turbulence measurements of a longitudinal vortex in a turbulent boundary layer zhang, x.; collina, m. w.. “turbulence measurements of a longitudinal vortex in a turbulent boundary layer.” paper presented at 35th aerospace sciences meeting and exhibit, 1997, reno, united states (1997). doi: 10.2514/6.1997-654. conference paper · 1997 zhang, x.; collina, m. w. 1997 10.2514/6.1997-654 paper presented at 35th aerospace sciences meeting and exhibit, 1997, reno, united states","order":550,"static_url":"/publications/436/"},{"section":"Publications","title":"Nearfield evolution of a longitudinal vortex generated by an inclined jet in a turbulent boundary layer","url":"/publications/15/","summary":"Zhang, X.; Collins, M. W.. “Nearfield evolution of a longitudinal vortex generated by an inclined jet in a turbulent boundary layer.” Journal of Fluids Engineering, Transactions of the ASME, v. 119, (4), p. 934-939 (1997). DOI: 10.1115/1.2819520.","meta":"Journal article · 1997","search_text":"nearfield evolution of a longitudinal vortex generated by an inclined jet in a turbulent boundary layer zhang, x.; collins, m. w.. “nearfield evolution of a longitudinal vortex generated by an inclined jet in a turbulent boundary layer.” journal of fluids engineering, transactions of the asme, v. 119, (4), p. 934-939 (1997). doi: 10.1115/1.2819520. journal article · 1997 zhang, x.; collins, m. w. 1997 10.1115/1.2819520 journal of fluids engineering, transactions of the asme, v. 119, (4), p. 934-939","order":551,"static_url":"/publications/15/"},{"section":"Publications","title":"Measurements of a longitudinal vortex generated by a rectangular jet in a turbulent boundary layer","url":"/publications/14/","summary":"Zhang, Xin; Collins, Michael W.. “Measurements of a longitudinal vortex generated by a rectangular jet in a turbulent boundary layer.” Physics of Fluids, v. 9, (6), p. 1665-1673 (1997). DOI: 10.1063/1.869286.","meta":"Journal article · 1997","search_text":"measurements of a longitudinal vortex generated by a rectangular jet in a turbulent boundary layer zhang, xin; collins, michael w.. “measurements of a longitudinal vortex generated by a rectangular jet in a turbulent boundary layer.” physics of fluids, v. 9, (6), p. 1665-1673 (1997). doi: 10.1063/1.869286. journal article · 1997 zhang, xin; collins, michael w. 1997 10.1063/1.869286 physics of fluids, v. 9, (6), p. 1665-1673","order":552,"static_url":"/publications/14/"},{"section":"Publications","title":"Progress in Computational Aeroacoustics in Predicting the Noise Radiated from Turbulent Flows","url":"/publications/13/","summary":"Aldo, Rona; Geoffrey, M. Lilley; Zhang, Xin. “Progress in Computational Aeroacoustics in Predicting the Noise Radiated from Turbulent Flows.” International Journal of Acoustics and Vibrations, v. 2, p. 45933 (1997). DOI: 10.20855/ijav.1997.2.106.","meta":"Journal article · 1997","search_text":"progress in computational aeroacoustics in predicting the noise radiated from turbulent flows aldo, rona; geoffrey, m. lilley; zhang, xin. “progress in computational aeroacoustics in predicting the noise radiated from turbulent flows.” international journal of acoustics and vibrations, v. 2, p. 45933 (1997). doi: 10.20855/ijav.1997.2.106. journal article · 1997 aldo, rona; geoffrey, m. lilley; zhang, xin 1997 10.20855/ijav.1997.2.106 international journal of acoustics and vibrations, v. 2, p. 45933","order":553,"static_url":"/publications/13/"},{"section":"Publications","title":"Flow structure analysis around an oscillating circular cylinder at low KC number: A numerical study","url":"/publications/12/","summary":"Zhang, Hui Liu; Zhang, Xin. “Flow structure analysis around an oscillating circular cylinder at low KC number: A numerical study.” Computers and Fluids, v. 26, (1), p. 83-106 (1997). DOI: 10.1016/s0045-7930(96)00031-x.","meta":"Journal article · 1997","search_text":"flow structure analysis around an oscillating circular cylinder at low kc number: a numerical study zhang, hui liu; zhang, xin. “flow structure analysis around an oscillating circular cylinder at low kc number: a numerical study.” computers and fluids, v. 26, (1), p. 83-106 (1997). doi: 10.1016/s0045-7930(96)00031-x. journal article · 1997 zhang, hui liu; zhang, xin 1997 10.1016/s0045-7930(96)00031-x computers and fluids, v. 26, (1), p. 83-106","order":554,"static_url":"/publications/12/"},{"section":"Publications","title":"A wind-tunnel investigation of aerofoil fitted with Gurney flaps","url":"/publications/466/","summary":"Jeffrey, D.R., Zhang, X. and Hurst, D.W.. “A wind-tunnel investigation of aerofoil fitted with Gurney flaps.” MIRA international conference on vehicle aerodynamics, Birmingham, U.K., 15-16 September 1996 (1996).","meta":"Conference paper · 1996","search_text":"a wind-tunnel investigation of aerofoil fitted with gurney flaps jeffrey, d.r., zhang, x. and hurst, d.w.. “a wind-tunnel investigation of aerofoil fitted with gurney flaps.” mira international conference on vehicle aerodynamics, birmingham, u.k., 15-16 september 1996 (1996). conference paper · 1996 jeffrey, d.r., zhang, x. and hurst, d.w. 1996 mira international conference on vehicle aerodynamics, birmingham, u.k., 15-16 september 1996.","order":555,"static_url":"/publications/466/"},{"section":"Publications","title":"An LDA study of longitudinal vortices embedded in a turbulent boundary layer","url":"/publications/465/","summary":"Zhang, H.L. and Zhang, X.. “An LDA study of longitudinal vortices embedded in a turbulent boundary layer.” The 8th International Symposium on Applications of Laser Techniques to Fluid Mechanics, Lisbon, Portugal, 8-11 July 1996 (1996).","meta":"Conference paper · 1996","search_text":"an lda study of longitudinal vortices embedded in a turbulent boundary layer zhang, h.l. and zhang, x.. “an lda study of longitudinal vortices embedded in a turbulent boundary layer.” the 8th international symposium on applications of laser techniques to fluid mechanics, lisbon, portugal, 8-11 july 1996 (1996). conference paper · 1996 zhang, h.l. and zhang, x. 1996 the 8th international symposium on applications of laser techniques to fluid mechanics, lisbon, portugal, 8-11 july 1996.","order":556,"static_url":"/publications/465/"},{"section":"Publications","title":"Computational study of small vane flow and heat transfer in a turbulent boundary layer","url":"/publications/464/","summary":"Zhang, H.L., Zhang, X., and Collins, W.W.. “Computational study of small vane flow and heat transfer in a turbulent boundary layer.” The 9th International Symposium on Transport Phenomena in Thermal-Fluids Engineering, Singapore, 25-28 June 1996 (1996).","meta":"Conference paper · 1996","search_text":"computational study of small vane flow and heat transfer in a turbulent boundary layer zhang, h.l., zhang, x., and collins, w.w.. “computational study of small vane flow and heat transfer in a turbulent boundary layer.” the 9th international symposium on transport phenomena in thermal-fluids engineering, singapore, 25-28 june 1996 (1996). conference paper · 1996 zhang, h.l., zhang, x., and collins, w.w. 1996 the 9th international symposium on transport phenomena in thermal-fluids engineering, singapore, 25-28 june 1996.","order":557,"static_url":"/publications/464/"},{"section":"Publications","title":"Pressure drag induced by a supersonic flow over cavities","url":"/publications/463/","summary":"Zhang, X.. “Pressure drag induced by a supersonic flow over cavities.” 76th AGARD Fluid Dynamics Panel Symposium, Ankara, Turkey, 24-27 April 1995. (also: AGARD Conference Proceedings 570, Aerodynamics of Store Intergration and Separation, pp. (19)1-9, February 1996 (1996).","meta":"Conference paper · 1996","search_text":"pressure drag induced by a supersonic flow over cavities zhang, x.. “pressure drag induced by a supersonic flow over cavities.” 76th agard fluid dynamics panel symposium, ankara, turkey, 24-27 april 1995. (also: agard conference proceedings 570, aerodynamics of store intergration and separation, pp. (19)1-9, february 1996 (1996). conference paper · 1996 zhang, x. 1996 76th agard fluid dynamics panel symposium, ankara, turkey, 24-27 april 1995. (also: agard conference proceedings 570, aerodynamics of store intergration and separation, pp. (19)1-9, february 1996.","order":558,"static_url":"/publications/463/"},{"section":"Publications","title":"Some aspects of streamwise vortex production using air jets","url":"/publications/437/","summary":"Zhang, Xin; Zhang, Hui Liu; Collins, M. W.. “Some aspects of streamwise vortex production using air jets.” Paper presented at 34th Aerospace Sciences Meeting and Exhibit, 1996, Reno, United States (1996). DOI: 10.2514/6.1996-209.","meta":"Conference paper · 1996","search_text":"some aspects of streamwise vortex production using air jets zhang, xin; zhang, hui liu; collins, m. w.. “some aspects of streamwise vortex production using air jets.” paper presented at 34th aerospace sciences meeting and exhibit, 1996, reno, united states (1996). doi: 10.2514/6.1996-209. conference paper · 1996 zhang, xin; zhang, hui liu; collins, m. w. 1996 10.2514/6.1996-209 paper presented at 34th aerospace sciences meeting and exhibit, 1996, reno, united states","order":559,"static_url":"/publications/437/"},{"section":"Publications","title":"Analysis of unsteady supersonic cavity flow employing an adaptive meshing algorithm","url":"/publications/11/","summary":"Zhang, Xin; Edwards, John A.. “Analysis of unsteady supersonic cavity flow employing an adaptive meshing algorithm.” Computers and Fluids, v. 25, (4), p. 373-393 (1996). DOI: 10.1016/0045-7930(95)00045-3.","meta":"Journal article · 1996","search_text":"analysis of unsteady supersonic cavity flow employing an adaptive meshing algorithm zhang, xin; edwards, john a.. “analysis of unsteady supersonic cavity flow employing an adaptive meshing algorithm.” computers and fluids, v. 25, (4), p. 373-393 (1996). doi: 10.1016/0045-7930(95)00045-3. journal article · 1996 zhang, xin; edwards, john a. 1996 10.1016/0045-7930(95)00045-3 computers and fluids, v. 25, (4), p. 373-393","order":560,"static_url":"/publications/11/"},{"section":"Publications","title":"Far-field noise radiation from an unsteady supersonic cavity flow","url":"/publications/469/","summary":"Zhang, X., Rona, A. and Lilley, G. M.. “Far-field noise radiation from an unsteady supersonic cavity flow.” AIAA Paper 95-040, Proceedings of the 16th AIAA Aeroacoustic Conference, pp. 285-292, 12-15 June 1995 (1995).","meta":"Conference paper · 1995","search_text":"far-field noise radiation from an unsteady supersonic cavity flow zhang, x., rona, a. and lilley, g. m.. “far-field noise radiation from an unsteady supersonic cavity flow.” aiaa paper 95-040, proceedings of the 16th aiaa aeroacoustic conference, pp. 285-292, 12-15 june 1995 (1995). conference paper · 1995 zhang, x., rona, a. and lilley, g. m. 1995 aiaa paper 95-040, proceedings of the 16th aiaa aeroacoustic conference, pp. 285-292, 12-15 june 1995.","order":561,"static_url":"/publications/469/"},{"section":"Publications","title":"Developing flow in a curved rectangular duct-numerical prediction using algebraic Reynolds stress turbulence model","url":"/publications/468/","summary":"Zhang, H.L. and Zhang, X.. “Developing flow in a curved rectangular duct-numerical prediction using algebraic Reynolds stress turbulence model.” 4th ERCOFTAC/AHR workshop on refined flow modelling, Karlsruhe, Germany, April 1995 (1995).","meta":"Conference paper · 1995","search_text":"developing flow in a curved rectangular duct-numerical prediction using algebraic reynolds stress turbulence model zhang, h.l. and zhang, x.. “developing flow in a curved rectangular duct-numerical prediction using algebraic reynolds stress turbulence model.” 4th ercoftac/ahr workshop on refined flow modelling, karlsruhe, germany, april 1995 (1995). conference paper · 1995 zhang, h.l. and zhang, x. 1995 4th ercoftac/ahr workshop on refined flow modelling, karlsruhe, germany, april 1995.","order":562,"static_url":"/publications/468/"},{"section":"Publications","title":"A computational analysis of shear layer induced flow oscillation and acoustic radiation","url":"/publications/467/","summary":"Zhang, X. and Rona, A.. “A computational analysis of shear layer induced flow oscillation and acoustic radiation.” Proceedings of 1st Asian CFD Conference, Vol. 2, pp. 677-682, Hong Kong, January 1995 (1995).","meta":"Conference paper · 1995","search_text":"a computational analysis of shear layer induced flow oscillation and acoustic radiation zhang, x. and rona, a.. “a computational analysis of shear layer induced flow oscillation and acoustic radiation.” proceedings of 1st asian cfd conference, vol. 2, pp. 677-682, hong kong, january 1995 (1995). conference paper · 1995 zhang, x. and rona, a. 1995 proceedings of 1st asian cfd conference, vol. 2, pp. 677-682, hong kong, january 1995.","order":563,"static_url":"/publications/467/"},{"section":"Publications","title":"Unsteady flow over a two-dimensional cascade of cavities at supersonic speeds","url":"/publications/438/","summary":"Zhang, X.. “Unsteady flow over a two-dimensional cascade of cavities at supersonic speeds.” Paper presented at Fluid Dynamics Conference, 1995, San Diego, United States, p. 1-10 (1995). DOI: 10.2514/6.1995-2162.","meta":"Conference paper · 1995","search_text":"unsteady flow over a two-dimensional cascade of cavities at supersonic speeds zhang, x.. “unsteady flow over a two-dimensional cascade of cavities at supersonic speeds.” paper presented at fluid dynamics conference, 1995, san diego, united states, p. 1-10 (1995). doi: 10.2514/6.1995-2162. conference paper · 1995 zhang, x. 1995 10.2514/6.1995-2162 paper presented at fluid dynamics conference, 1995, san diego, united states, p. 1-10","order":564,"static_url":"/publications/438/"},{"section":"Publications","title":"Co- and contrarotating streamwise vortices in a turbulent boundary layer","url":"/publications/10/","summary":"Zhang, Xin. “Co- and contrarotating streamwise vortices in a turbulent boundary layer.” Journal of Aircraft, v. 32, (5), p. 1095-1101 (1995). DOI: 10.2514/3.46841.","meta":"Journal article · 1995","search_text":"co- and contrarotating streamwise vortices in a turbulent boundary layer zhang, xin. “co- and contrarotating streamwise vortices in a turbulent boundary layer.” journal of aircraft, v. 32, (5), p. 1095-1101 (1995). doi: 10.2514/3.46841. journal article · 1995 zhang, xin 1995 10.2514/3.46841 journal of aircraft, v. 32, (5), p. 1095-1101","order":565,"static_url":"/publications/10/"},{"section":"Publications","title":"Compressible cavity flow oscillation due to shear layer instabilities and pressure feedback","url":"/publications/9/","summary":"Zhang, Xin. “Compressible cavity flow oscillation due to shear layer instabilities and pressure feedback.” AIAA Journal, v. 33, (8), p. 1404-1411 (1995). DOI: 10.2514/3.12845.","meta":"Journal article · 1995","search_text":"compressible cavity flow oscillation due to shear layer instabilities and pressure feedback zhang, xin. “compressible cavity flow oscillation due to shear layer instabilities and pressure feedback.” aiaa journal, v. 33, (8), p. 1404-1411 (1995). doi: 10.2514/3.12845. journal article · 1995 zhang, xin 1995 10.2514/3.12845 aiaa journal, v. 33, (8), p. 1404-1411","order":566,"static_url":"/publications/9/"},{"section":"Publications","title":"Experimental and numerical analysis of convective heat transfer in turbulent channel flow with square and circular columns","url":"/publications/8/","summary":"Zhang, Xin; Stasiek, Jan; Collins, Michael W.. “Experimental and numerical analysis of convective heat transfer in turbulent channel flow with square and circular columns.” Experimental Thermal and Fluid Science, v. 10, (2), p. 229-237 (1995). DOI: 10.1016/0894-1777(94)00089-q.","meta":"Journal article · 1995","search_text":"experimental and numerical analysis of convective heat transfer in turbulent channel flow with square and circular columns zhang, xin; stasiek, jan; collins, michael w.. “experimental and numerical analysis of convective heat transfer in turbulent channel flow with square and circular columns.” experimental thermal and fluid science, v. 10, (2), p. 229-237 (1995). doi: 10.1016/0894-1777(94)00089-q. journal article · 1995 zhang, xin; stasiek, jan; collins, michael w. 1995 10.1016/0894-1777(94)00089-q experimental thermal and fluid science, v. 10, (2), p. 229-237","order":567,"static_url":"/publications/8/"},{"section":"Publications","title":"A computational analysis of supersonic jet and instability wave interaction","url":"/publications/471/","summary":"Zhang, X. and Edwards, J.A.. “A computational analysis of supersonic jet and instability wave interaction.” AIAA Paper 94-2194, 25th AIAA Fluid Dynamics Conference, Colorado Springs, Colorado, U.S.A., 20-23 June 1994 (1994).","meta":"Conference paper · 1994","search_text":"a computational analysis of supersonic jet and instability wave interaction zhang, x. and edwards, j.a.. “a computational analysis of supersonic jet and instability wave interaction.” aiaa paper 94-2194, 25th aiaa fluid dynamics conference, colorado springs, colorado, u.s.a., 20-23 june 1994 (1994). conference paper · 1994 zhang, x. and edwards, j.a. 1994 aiaa paper 94-2194, 25th aiaa fluid dynamics conference, colorado springs, colorado, u.s.a., 20-23 june 1994.","order":568,"static_url":"/publications/471/"},{"section":"Publications","title":"Control of shear layer driven flow oscillation and heat transfer over groove-type geometry","url":"/publications/470/","summary":"Zhang, X.. “Control of shear layer driven flow oscillation and heat transfer over groove-type geometry.” Experimental and Predictive Methods for Energy Applications-IFEC1, pp. 162-167, London, U.K., April 1994 (1994).","meta":"Conference paper · 1994","search_text":"control of shear layer driven flow oscillation and heat transfer over groove-type geometry zhang, x.. “control of shear layer driven flow oscillation and heat transfer over groove-type geometry.” experimental and predictive methods for energy applications-ifec1, pp. 162-167, london, u.k., april 1994 (1994). conference paper · 1994 zhang, x. 1994 experimental and predictive methods for energy applications-ifec1, pp. 162-167, london, u.k., april 1994.","order":569,"static_url":"/publications/470/"},{"section":"Publications","title":"An experimental and computational investigation of ground effect lift loss for single jet impingement","url":"/publications/7/","summary":"Ing, Dan N.; Zhang, Xin. “An experimental and computational investigation of ground effect lift loss for single jet impingement.” Aeronautical Journal, v. 98, p. 127-136 (1994). DOI: 10.1017/s0001924000049976.","meta":"Journal article · 1994","search_text":"an experimental and computational investigation of ground effect lift loss for single jet impingement ing, dan n.; zhang, xin. “an experimental and computational investigation of ground effect lift loss for single jet impingement.” aeronautical journal, v. 98, p. 127-136 (1994). doi: 10.1017/s0001924000049976. journal article · 1994 ing, dan n.; zhang, xin 1994 10.1017/s0001924000049976 aeronautical journal, v. 98, p. 127-136","order":570,"static_url":"/publications/7/"},{"section":"Publications","title":"Computational analysis of a single jet impingement ground effect lift loss","url":"/publications/5/","summary":"Zhang, Xin; Ing, Dan N.. “Computational analysis of a single jet impingement ground effect lift loss.” Journal of Aircraft, v. 31, (2), p. 256-262 (1994). DOI: 10.2514/3.46482.","meta":"Journal article · 1994","search_text":"computational analysis of a single jet impingement ground effect lift loss zhang, xin; ing, dan n.. “computational analysis of a single jet impingement ground effect lift loss.” journal of aircraft, v. 31, (2), p. 256-262 (1994). doi: 10.2514/3.46482. journal article · 1994 zhang, xin; ing, dan n. 1994 10.2514/3.46482 journal of aircraft, v. 31, (2), p. 256-262","order":571,"static_url":"/publications/5/"},{"section":"Publications","title":"Streamwise vortex production in a turbulent flow through wall jets","url":"/publications/475/","summary":"Zhang, X. “Streamwise vortex production in a turbulent flow through wall jets.” Numerical Methods in Laminar and Turbulent Flow, Vol. VIII, Part 1, Edited by C. Taylor, Pineridge Press, Swansea, U.K., pp.875-886, 18-23 July 1993 (1993).","meta":"Conference paper · 1993","search_text":"streamwise vortex production in a turbulent flow through wall jets zhang, x. “streamwise vortex production in a turbulent flow through wall jets.” numerical methods in laminar and turbulent flow, vol. viii, part 1, edited by c. taylor, pineridge press, swansea, u.k., pp.875-886, 18-23 july 1993 (1993). conference paper · 1993 zhang, x 1993 numerical methods in laminar and turbulent flow, vol. viii, part 1, edited by c. taylor, pineridge press, swansea, u.k., pp.875-886, 18-23 july 1993.","order":572,"static_url":"/publications/475/"},{"section":"Publications","title":"Transient features of a supersonic jet in cross flow","url":"/publications/474/","summary":"Zhang, X, Hurst, D. W. and Lilley, G. M.. “Transient features of a supersonic jet in cross flow.” 72nd AGARD Fluid Dynamics Panel Symposium, Winchester, U.K., April 1993. (also: AGARD Conference Proceedings 570, Computational and Experimental Assessment of Jets in Cross Flow, pp…","meta":"Conference paper · 1993","search_text":"transient features of a supersonic jet in cross flow zhang, x, hurst, d. w. and lilley, g. m.. “transient features of a supersonic jet in cross flow.” 72nd agard fluid dynamics panel symposium, winchester, u.k., april 1993. (also: agard conference proceedings 570, computational and experimental assessment of jets in cross flow, pp. (3)1-16, november 1993.) (1993). conference paper · 1993 zhang, x, hurst, d. w. and lilley, g. m. 1993 72nd agard fluid dynamics panel symposium, winchester, u.k., april 1993. (also: agard conference proceedings 570, computational and experimental assessment of jets in cross flow, pp. (3)1-16, november 1993.)","order":573,"static_url":"/publications/474/"},{"section":"Publications","title":"Holographic interferometry and liquid crystals for quantitative convection","url":"/publications/473/","summary":"Collins, M. W., Collins, A. L., Stasiek, J. and Zhang, X.. “Holographic interferometry and liquid crystals for quantitative convection.” Proceedings of 1st International Thermal Energy Congress, Vol. 1, pp. 15-26, Marrakesh, Morocco, 6-10 June 6-10 1993 (1993).","meta":"Conference paper · 1993","search_text":"holographic interferometry and liquid crystals for quantitative convection collins, m. w., collins, a. l., stasiek, j. and zhang, x.. “holographic interferometry and liquid crystals for quantitative convection.” proceedings of 1st international thermal energy congress, vol. 1, pp. 15-26, marrakesh, morocco, 6-10 june 6-10 1993 (1993). conference paper · 1993 collins, m. w., collins, a. l., stasiek, j. and zhang, x. 1993 proceedings of 1st international thermal energy congress, vol. 1, pp. 15-26, marrakesh, morocco, 6-10 june 6-10 1993.","order":574,"static_url":"/publications/473/"},{"section":"Publications","title":"A study of single jet impingement ground effect lift loss","url":"/publications/472/","summary":"Zhang, X. and Ing, D.. “A study of single jet impingement ground effect lift loss.” AIAA Paper 93-0869, AIAA 31st Aerospace Sciences Meeting and Exhibit, Reno, Nevada, U.S.A., January 1993 (1993). DOI: 10.2514/6.1993-869.","meta":"Conference paper · 1993","search_text":"a study of single jet impingement ground effect lift loss zhang, x. and ing, d.. “a study of single jet impingement ground effect lift loss.” aiaa paper 93-0869, aiaa 31st aerospace sciences meeting and exhibit, reno, nevada, u.s.a., january 1993 (1993). doi: 10.2514/6.1993-869. conference paper · 1993 zhang, x. and ing, d. 1993 10.2514/6.1993-869 aiaa paper 93-0869, aiaa 31st aerospace sciences meeting and exhibit, reno, nevada, u.s.a., january 1993.","order":575,"static_url":"/publications/472/"},{"section":"Publications","title":"Computational analysis of co- and contra-rotating streamwise vortices in a turbulent boundary layer","url":"/publications/440/","summary":"Zhang, Xin. “Computational analysis of co- and contra-rotating streamwise vortices in a turbulent boundary layer.” Paper presented at AIAA 23rd Fluid Dynamics, Plasmadynamics, and Lasers Conference, 1993, Orlando, United States (1993). DOI: 10.2514/6.1993-3035.","meta":"Conference paper · 1993","search_text":"computational analysis of co- and contra-rotating streamwise vortices in a turbulent boundary layer zhang, xin. “computational analysis of co- and contra-rotating streamwise vortices in a turbulent boundary layer.” paper presented at aiaa 23rd fluid dynamics, plasmadynamics, and lasers conference, 1993, orlando, united states (1993). doi: 10.2514/6.1993-3035. conference paper · 1993 zhang, xin 1993 10.2514/6.1993-3035 paper presented at aiaa 23rd fluid dynamics, plasmadynamics, and lasers conference, 1993, orlando, united states","order":576,"static_url":"/publications/440/"},{"section":"Publications","title":"An experimental and numerical study of single jet impingement ground-effect lift loss","url":"/publications/439/","summary":"Ing, D. N.; Zhang, X.. “An experimental and numerical study of single jet impingement ground-effect lift loss.” Paper presented at International Powered Lift Conference, 1993, Santa Clara, United States, p. 293-303 (1993). DOI: 10.2514/6.1993-4887.","meta":"Conference paper · 1993","search_text":"an experimental and numerical study of single jet impingement ground-effect lift loss ing, d. n.; zhang, x.. “an experimental and numerical study of single jet impingement ground-effect lift loss.” paper presented at international powered lift conference, 1993, santa clara, united states, p. 293-303 (1993). doi: 10.2514/6.1993-4887. conference paper · 1993 ing, d. n.; zhang, x. 1993 10.2514/6.1993-4887 paper presented at international powered lift conference, 1993, santa clara, united states, p. 293-303","order":577,"static_url":"/publications/439/"},{"section":"Publications","title":"Flow and heat transfer in a turbulent boundary layer through skewed and pitched jets","url":"/publications/4/","summary":"Zhang, Xin; Collins, Michael W.. “Flow and heat transfer in a turbulent boundary layer through skewed and pitched jets.” AIAA Journal, v. 31, (9), p. 1590-1599 (1993). DOI: 10.2514/3.11819.","meta":"Journal article · 1993","search_text":"flow and heat transfer in a turbulent boundary layer through skewed and pitched jets zhang, xin; collins, michael w.. “flow and heat transfer in a turbulent boundary layer through skewed and pitched jets.” aiaa journal, v. 31, (9), p. 1590-1599 (1993). doi: 10.2514/3.11819. journal article · 1993 zhang, xin; collins, michael w. 1993 10.2514/3.11819 aiaa journal, v. 31, (9), p. 1590-1599","order":578,"static_url":"/publications/4/"},{"section":"Publications","title":"Novel applications of holographic interferometry and liquid crystal thermography in low speed wind tunnel","url":"/publications/477/","summary":"Zhang, X., Stasiek, J. and Collins, M. W.. “Novel applications of holographic interferometry and liquid crystal thermography in low speed wind tunnel.” Wind Tunnels and Wind Tunnel Test Techniques, The Royal Aeronautical Society, Southampton, U.K., pp. (38)1-11, September 1992 (…","meta":"Conference paper · 1992","search_text":"novel applications of holographic interferometry and liquid crystal thermography in low speed wind tunnel zhang, x., stasiek, j. and collins, m. w.. “novel applications of holographic interferometry and liquid crystal thermography in low speed wind tunnel.” wind tunnels and wind tunnel test techniques, the royal aeronautical society, southampton, u.k., pp. (38)1-11, september 1992 (1992). conference paper · 1992 zhang, x., stasiek, j. and collins, m. w. 1992 wind tunnels and wind tunnel test techniques, the royal aeronautical society, southampton, u.k., pp. (38)1-11, september 1992.","order":579,"static_url":"/publications/477/"},{"section":"Publications","title":"Surface heat transfer investigation using thermochromic liquid crystal, Part II: application to complex geometries and comparison with computational predictions","url":"/publications/476/","summary":"Stasiek J., Zhang, X, Henry F. and Collins, M. W.. “Surface heat transfer investigation using thermochromic liquid crystal, Part II: application to complex geometries and comparison with computational predictions.” Proceedings of Optical Methods and Data Processing in Heat and F…","meta":"Conference paper · 1992","search_text":"surface heat transfer investigation using thermochromic liquid crystal, part ii: application to complex geometries and comparison with computational predictions stasiek j., zhang, x, henry f. and collins, m. w.. “surface heat transfer investigation using thermochromic liquid crystal, part ii: application to complex geometries and comparison with computational predictions.” proceedings of optical methods and data processing in heat and fluid flow, imeche, london, u.k, pp. 137-140, april 1992 (1992). conference paper · 1992 stasiek j., zhang, x, henry f. and collins, m. w. 1992 proceedings of optical methods and data processing in heat and fluid flow, imeche, london, u.k, pp. 137-140, april 1992.","order":580,"static_url":"/publications/476/"},{"section":"Publications","title":"Experimental investigation of supersonic flow over two cavities in tandem","url":"/publications/3/","summary":"Zhang, Xin; Edwards, John A.. “Experimental investigation of supersonic flow over two cavities in tandem.” AIAA Journal, v. 30, (5), p. 1182-1190 (1992). DOI: 10.2514/3.11049.","meta":"Journal article · 1992","search_text":"experimental investigation of supersonic flow over two cavities in tandem zhang, xin; edwards, john a.. “experimental investigation of supersonic flow over two cavities in tandem.” aiaa journal, v. 30, (5), p. 1182-1190 (1992). doi: 10.2514/3.11049. journal article · 1992 zhang, xin; edwards, john a. 1992 10.2514/3.11049 aiaa journal, v. 30, (5), p. 1182-1190","order":581,"static_url":"/publications/3/"},{"section":"Publications","title":"A laser Doppler anemometry study of a supersonic jet in a low speed cross-flow","url":"/publications/478/","summary":"Zhang, X. and Hurst. D. W.. “A laser Doppler anemometry study of a supersonic jet in a low speed cross-flow.” Proceedings of the 4th International Conference on Laser Anemometry, Advance and Applications, Vol. 2, pp. 403-411, Cleveland, Ohio, U.S.A., August 1991 (1991).","meta":"Conference paper · 1991","search_text":"a laser doppler anemometry study of a supersonic jet in a low speed cross-flow zhang, x. and hurst. d. w.. “a laser doppler anemometry study of a supersonic jet in a low speed cross-flow.” proceedings of the 4th international conference on laser anemometry, advance and applications, vol. 2, pp. 403-411, cleveland, ohio, u.s.a., august 1991 (1991). conference paper · 1991 zhang, x. and hurst. d. w. 1991 proceedings of the 4th international conference on laser anemometry, advance and applications, vol. 2, pp. 403-411, cleveland, ohio, u.s.a., august 1991.","order":582,"static_url":"/publications/478/"},{"section":"Publications","title":"Surface flow on a flat plate induced by a supersonic jet exhausting normally into a low speed crossflow","url":"/publications/442/","summary":"Zhang, Xin; Hurst, David W.. “Surface flow on a flat plate induced by a supersonic jet exhausting normally into a low speed crossflow.” Paper presented at Flight Simulation Technologies Conference and Exhibit, 1990, Dayton, United States, p. 168-177 (1990). DOI: 10.2514/6.1990-3…","meta":"Conference paper · 1990","search_text":"surface flow on a flat plate induced by a supersonic jet exhausting normally into a low speed crossflow zhang, xin; hurst, david w.. “surface flow on a flat plate induced by a supersonic jet exhausting normally into a low speed crossflow.” paper presented at flight simulation technologies conference and exhibit, 1990, dayton, united states, p. 168-177 (1990). doi: 10.2514/6.1990-3011. conference paper · 1990 zhang, xin; hurst, david w. 1990 10.2514/6.1990-3011 paper presented at flight simulation technologies conference and exhibit, 1990, dayton, united states, p. 168-177","order":583,"static_url":"/publications/442/"},{"section":"Publications","title":"An experimental investigation of supersonic flow over two cavities in tandem","url":"/publications/441/","summary":"Zhang, Xin; Edwards, John A.. “An experimental investigation of supersonic flow over two cavities in tandem.” Paper presented at Flight Simulation Technologies Conference and Exhibit, 1990, Dayton, United States, p. 622-631 (1990). DOI: 10.2514/6.1990-3087.","meta":"Conference paper · 1990","search_text":"an experimental investigation of supersonic flow over two cavities in tandem zhang, xin; edwards, john a.. “an experimental investigation of supersonic flow over two cavities in tandem.” paper presented at flight simulation technologies conference and exhibit, 1990, dayton, united states, p. 622-631 (1990). doi: 10.2514/6.1990-3087. conference paper · 1990 zhang, xin; edwards, john a. 1990 10.2514/6.1990-3087 paper presented at flight simulation technologies conference and exhibit, 1990, dayton, united states, p. 622-631","order":584,"static_url":"/publications/441/"},{"section":"Publications","title":"An investigation of supersonic oscillatory cavity flows driven by thick shear layers","url":"/publications/2/","summary":"X. Zhang; J. A. Edwards. “An investigation of supersonic oscillatory cavity flows driven by thick shear layers.” (1990). DOI: 10.1017/S0001924000023319.","meta":"Journal article · 1990","search_text":"an investigation of supersonic oscillatory cavity flows driven by thick shear layers x. zhang; j. a. edwards. “an investigation of supersonic oscillatory cavity flows driven by thick shear layers.” (1990). doi: 10.1017/s0001924000023319. journal article · 1990 x. zhang; j. a. edwards 1990 10.1017/s0001924000023319","order":585,"static_url":"/publications/2/"},{"section":"Publications","title":"Computational analysis of unsteady supersonic cavity flows driven by thick shear layers","url":"/publications/1/","summary":"Zhang, X.; Edwards, J. A.. “Computational analysis of unsteady supersonic cavity flows driven by thick shear layers.” Aeronautical Journal, v. 92, (919), p. 365-374 (1988). DOI: 10.1017/s0001924000016456.","meta":"Journal article · 1988","search_text":"computational analysis of unsteady supersonic cavity flows driven by thick shear layers zhang, x.; edwards, j. a.. “computational analysis of unsteady supersonic cavity flows driven by thick shear layers.” aeronautical journal, v. 92, (919), p. 365-374 (1988). doi: 10.1017/s0001924000016456. journal article · 1988 zhang, x.; edwards, j. a. 1988 10.1017/s0001924000016456 aeronautical journal, v. 92, (919), p. 365-374","order":586,"static_url":"/publications/1/"},{"section":"Publications","title":"Experiments and computations on a cavity driven by a thick shear layer at Mach 3.5","url":"/publications/479/","summary":"Zhang, X. and Edwards, J. A.. “Experiments and computations on a cavity driven by a thick shear layer at Mach 3.5.” EuroMech 225, The Aerodynamics of Spacecraft, 12-16 July 1987 (1987).","meta":"Conference paper · 1987","search_text":"experiments and computations on a cavity driven by a thick shear layer at mach 3.5 zhang, x. and edwards, j. a.. “experiments and computations on a cavity driven by a thick shear layer at mach 3.5.” euromech 225, the aerodynamics of spacecraft, 12-16 july 1987 (1987). conference paper · 1987 zhang, x. and edwards, j. a. 1987 euromech 225, the aerodynamics of spacecraft, 12-16 july 1987.","order":587,"static_url":"/publications/479/"},{"section":"Publications","title":"Some aspects of supersonic flow over a cavity cascade","url":"/publications/480/","summary":"Edwards, J. A.; Zhang, Xin. “Some aspects of supersonic flow over a cavity cascade.” AIAA Atmospheric Flight Mechanics Conference, Williamsburg, Virginia, 18-20 August 1986, p. 56-61; AIAA Paper 86-2025 (1986). DOI: 10.2514/6.1986-2025.","meta":"Conference paper · 1986","search_text":"some aspects of supersonic flow over a cavity cascade edwards, j. a.; zhang, xin. “some aspects of supersonic flow over a cavity cascade.” aiaa atmospheric flight mechanics conference, williamsburg, virginia, 18-20 august 1986, p. 56-61; aiaa paper 86-2025 (1986). doi: 10.2514/6.1986-2025. conference paper · 1986 edwards, j. a.; zhang, xin 1986 10.2514/6.1986-2025 aiaa atmospheric flight mechanics conference, williamsburg, virginia, 18-20 august 1986, p. 56-61; aiaa paper 86-2025","order":588,"static_url":"/publications/480/"},{"section":"News","title":"AANTC conducts outdoor noise measurements of DJI T100 across multiple flight conditions","url":"/post/40/","summary":"The team led by Professor Xin Zhang at the Aerodynamics, Acoustics and Noise Control Technology Centre (AANTC) of the Hong Kong University of Science and Technology, together with Professor Chuntai Zheng's research group at Shenzhen Technology University, conducted outdoor noise…","meta":"25 September 2026","search_text":"aantc conducts outdoor noise measurements of dji t100 across multiple flight conditions the team led by professor xin zhang at the aerodynamics, acoustics and noise control technology centre (aantc) of the hong kong university of science and technology, together with professor chuntai zheng's research group at shenzhen technology university, conducted outdoor noise measurements of a dji t100 drone at the bay area zhilian test facility in pingshan district, shenzhen, on 16–17 september 2026. the team collected acoustic data under different loading and flight conditions to study how loading and flight operation affect drone noise. in recent years, professor xin zhang's team has conducted multiple environmental noise measurement campaigns involving civil low-altitude aircraft, including drones and electric vertical take-off and landing (evtol) aircraft, at locations in mainland china and hong kong. the present measurements form part of both a research project on environmental noise in the low-altitude economy supported by hong kong's environment and conservation fund and hong kong's low-altitude economy regulatory sandbox project. they aim to provide an experimental basis for aircraft noise characterisation, sound propagation modelling and evidence-based technical recommendations, and to inform the development of noise standards for low-altitude aircraft. measuring noise across loading and flight conditions the measurements examined drone noise under different loading and operating conditions in an outdoor environment. the acoustic recordings will support subsequent analysis of how changes in aircraft operation affect noise emissions. the team deployed a ground microphone array to record sound during the flight tests. the acoustic measurements will support analysis of drone noise characteristics and provide an experimental basis for subsequent environmental noise assessment. measurements at different masses and flight conditions will also support analysis of how loading and operation affect noise. informing low-altitude noise assessment and management the dji t100 campaign is part of the team's environmental noise measurement programme for low-altitude aircraft. the programme has already included tests of drones and electric vertical take-off and landing (evtol) aircraft at multiple locations in mainland china and hong kong, and will continue to expand to additional aircraft types and operating conditions. the present campaign adds measured data across different loading and flight conditions and demonstrates the team's capability to conduct outdoor noise measurements of drones in the 150 kg class. building on these measurements, the team will analyse the acoustic recordings to characterise drone noise and support noise assessments of operating scenarios relevant to hong kong's low-altitude economy regulatory sandbox. comparisons across loading and flight conditions will support studies of individual aircraft noise emissions and acoustic impacts along flight routes and around take-off and landing sites, informing technical regulatory recommendations. the team also actively participates in research and the development of environmental noise standards for low-altitude aircraft. the measurement data and research findings will provide experimental evidence and technical support for the development of future noise measurement procedures, assessment methods and management standards. 25 september 2026 drone projects dji t100 in flight above the ground microphone array during outdoor noise measurements. the bay area zhilian test base in pingshan district, shenzhen. ground microphone array deployed for the dji t100 outdoor noise measurements. dji t100 during flight testing at the pingshan test facility in shenzhen.","order":589,"static_url":"/post/40/"},{"section":"News","title":"Congratulations to Dr. ZHANG Zhicheng on earning his PhD","url":"/post/39/","summary":"AANTC congratulates Dr. ZHANG Zhicheng on completing his doctoral studies and earning his PhD. His dissertation, “Towards aeroacoustic modelling for multi-rotor drones”, brings together experimental, theoretical and numerical approaches to drone noise. Research highlights His re…","meta":"31 August 2026","search_text":"congratulations to dr. zhang zhicheng on earning his phd aantc congratulates dr. zhang zhicheng on completing his doctoral studies and earning his phd. his dissertation, “towards aeroacoustic modelling for multi-rotor drones”, brings together experimental, theoretical and numerical approaches to drone noise. research highlights his research includes noise measurements of multi-rotor drones in an anechoic chamber, the development of a rotor noise propagation model based on linearised theory, and an efficient numerical method for low-mach-number aeroacoustic simulations. these contributions support the group's research into drone noise measurement and prediction. we thank dr. zhang for his contributions to the group and wish him continued success as he pursues postdoctoral research with us. related publications z. zhang, y. xiao, z. peng, p. zhou, and x. zhang, “on weak compressibility effects in low-mach-number aeroacoustic simulations of small-scale rotors,” phys. fluids, vol. 38, no. 7, art. no. 078119, 2026. z. zhang, z. peng, b. chen, p. zhou, and x. zhang, “experimental evaluation of a frequency-domain acoustic model for drone rotor noise prediction in non-axial flows,” aerosp. sci. technol., vol. 176, art. no. 112737, 2026. z. zhang, z. peng, x. li, w. chen, p. zhou, and x. zhang, “a computational aeroacoustic study of a drone rotor in forward flight with flapping motion,” in icsv31, incheon, 2025. z. zhang, j. he, x. li, y. li, p. zhou, x. zhang, and x. huang, “enhancing broadband noise prediction of a hovering rotor with an empirical wall-pressure spectrum model,” in icsv30, amsterdam, 2024. z. zhang, y. li, é. spieser, p. zhou, and x. zhang, “an improved artificial compressibility method for aeroacoustics at low mach numbers,” in internoise23, chiba, 2023. r. cao, z. zhang, z. peng, z. ma, w. chen, p. zhou, and x. zhang, “anechoic noise characterization of sub-7kg multi-rotor drones: configuration effects and spl scaling models,” in forum acusticum euronoise 2025, málaga, 2025. j. he, z. zhang, q. liu, and p. zhou, “prediction of the acoustic particle velocity in aerodynamic flows and its applications to the boundary element method,” in internoise24, nantes, 2024. 31 august 2026 aeroacoustics numerical visualisation of multirotor wake structures in a low-mach-number aeroacoustic simulation.","order":590,"static_url":"/post/39/"},{"section":"News","title":"Congratulations to Dr. BAO Hongsen on earning his PhD","url":"/post/38/","summary":"AANTC congratulates Dr. BAO Hongsen on completing his doctoral degree requirements and earning his PhD. His dissertation is entitled “On the Gaussian beam tracing method for high-frequency sound wave propagation in inhomogeneous flows”. His research addresses the accurate and ef…","meta":"31 August 2026","search_text":"congratulations to dr. bao hongsen on earning his phd aantc congratulates dr. bao hongsen on completing his doctoral degree requirements and earning his phd. his dissertation is entitled “on the gaussian beam tracing method for high-frequency sound wave propagation in inhomogeneous flows”. his research addresses the accurate and efficient prediction of sound propagation in urban environments, where wind fields and building boundaries produce complex acoustic phenomena. he developed a gaussian beam tracing (gbt) method for high-frequency sound propagation in inhomogeneous flows, balancing computational cost and numerical accuracy. the formulation was validated against benchmark cases of varying complexity and integrated into a low-altitude aircraft noise mapping simulation platform. we thank dr. bao for his contributions to the group and wish him every success in his postdoctoral research. related publications h. bao, q. tan, p. zhou, w. chen, x. zhang, and s. zhong, “on the gaussian beam tracing method for long-distance sound wave propagation in non-uniform mean flows,” proceedings of the royal society a: mathematical, physical and engineering sciences, vol. 481, no. 2307, 2025. h. bao, j. he, z. zhang, and x. zhang, “sound transmission of drones in urban wind conditions,” in quiet drones, 2026. h. bao, p. zhou, and x. zhang, “on the high-order gaussian beam series method for acoustic lateral wave propagation in stratified flows,” in 32nd international congress on sound and vibration, 2026. h. bao, q. tan, j. he, p. zhou, w. chen, and x. zhang, “the air vehicle flyover noise assessment in urban areas with complex urban wind conditions,” in 31st international congress on sound and vibration, 2025. h. bao, p. zhou, w. chen, x. zhang, and s. zhong, “an improved gaussian beam tracing method for the long-distance sound wave propagation in nonuniform mean flows,” in 30th international congress on sound and vibration, 2024. 31 august 2026 aeroacoustics case study- noise mappings of tko in hong kong","order":591,"static_url":"/post/38/"},{"section":"News","title":"Congratulations to Dr. LI Xiangru on earning his PhD","url":"/post/37/","summary":"AANTC congratulates Dr. LI Xiangru on completing his doctoral research and earning his PhD. His dissertation is entitled “Advancing cycling performance through integrated aerodynamic engineering and human-centered optimization”. His research develops an integrated, multiscale fr…","meta":"31 August 2026","search_text":"congratulations to dr. li xiangru on earning his phd aantc congratulates dr. li xiangru on completing his doctoral research and earning his phd. his dissertation is entitled “advancing cycling performance through integrated aerodynamic engineering and human-centered optimization”. his research develops an integrated, multiscale framework for improving cycling performance through the aerodynamic optimisation of textiles, cycling skinsuits, rider posture and helmet design. it shows that effective interventions must balance drag reduction with each rider's physiological demands, thermal comfort and practical operating conditions. research highlight beyond low drag: integrating aerodynamics and emg for smarter cycling postures conventional cycling-performance research often considers aerodynamic drag and physiological demands separately, while the upper-body muscular effort required to sustain an aerodynamic posture receives much less attention. this study integrates wind-tunnel aerodynamic measurements with surface electromyography (emg) to quantify drag and upper-body muscle activity across different cycling postures and handlebar positions. pareto optimization was then used to identify postures that best balance aerodynamic efficiency and muscular demand. the results show that more aerodynamic postures reduce drag but generally require greater upper-body muscle activation, providing a quantitative basis for posture selection, athlete training and aerodynamic bike fitting. this work was published in international journal of sports physiology and performance in 2026 and presented at icsports 2025 in spain, where it received the best student paper award. we thank dr. li for his contributions to sports aerodynamics research and wish him every success in his future work and personal life. related publications x. li, p. zhou, and x. zhang, “optimizing cycling postures: upper limb muscle effort and aerodynamic performance,” international journal of sports physiology and performance, advance online publication, 2026. doi: 10.1123/ijspp.2025-0344. x. li, j. mao, and p. zhou, “aerodynamic and acoustic evaluation of a cylinder covered by stretched grooved fabric,” aiaa journal, vol. 63, no. 5, pp. 2097–2104, 2025. doi: 10.2514/1.j065006. x. li, p. zhou, and x. zhang, “balance of upper limb muscle activation and aerodynamics for cycling posture optimization,” in proceedings of the 13th international conference on sport science research and technology support-icsports, scitepress, 2025, pp. 50–56. doi: 10.5220/0013677000003988. x. li, j. mao, and p. zhou, “aerodynamic and acoustic evaluation of a cylinder covered by stretched grooved fabric near critical reynolds numbers,” in proceedings of inter-noise and noise-con congress and conference, institute of noise control engineering, 2024, pp. 5724–5733. doi: 10.3397/in_2024_3638. 31 august 2026 sports aerodynamics emg devices on a cyclist during wind-tunnel testing. surface emg electrodes measuring upper-limb muscle activation. pareto optimization of upper-limb muscle activation and aerodynamic drag across cycling postures.","order":592,"static_url":"/post/37/"},{"section":"News","title":"Prof. Zhou Peng was invited to attend the signing ceremony between bossini.X and the HK cycling team","url":"/post/36/","summary":"Prof. Zhou Peng from AANTC participated in the signing ceremony between bossini.X and the Hong Kong Cycling Team, which took place on April 18th at the Jockey Club Lecture Theatre in the Olympic Building. During the event, Professor Zhou introduced the team's newly designed next…","meta":"19 April 2024","search_text":"prof. zhou peng was invited to attend the signing ceremony between bossini.x and the hk cycling team prof. zhou peng from aantc participated in the signing ceremony between bossini.x and the hong kong cycling team, which took place on april 18th at the jockey club lecture theatre in the olympic building. during the event, professor zhou introduced the team's newly designed next-generation high-performance racing jerseys for the hong kong team. the collaboration between aantc and bossini.x leveraged the research strength of the team in aerodynamics and cycling apparel development, combined with bossini.x's expertise in sports apparel manufacturing, to comprehensively optimize the cycling jerseys. using 3d scanning technology, computational fluid dynamics simulations, and advanced wind tunnel testing, the team conducted multiple rounds of design optimization, focusing on factors such as fabric distribution and stretch ratios of the jerseys. the optimized cycling jerseys can reduce drag by up to 3% at racing speeds, giving the hong kong team a technological advantage in future competitions. 19 april 2024 sports aerodynamics","order":593,"static_url":"/post/36/"},{"section":"News","title":"The Chinese national cycling team athletes and coaches visited AANTC for communication and testing","url":"/post/35/","summary":"Recently, the athletes and coaching staff of the Chinese national cycling team visited AANTC for communication and testing purposes. AANTC, through innovative cycling apparel design, posture optimization technology, and advanced full-scale sports wind tunnel testing, along with …","meta":"19 April 2024","search_text":"the chinese national cycling team athletes and coaches visited aantc for communication and testing recently, the athletes and coaching staff of the chinese national cycling team visited aantc for communication and testing purposes. aantc, through innovative cycling apparel design, posture optimization technology, and advanced full-scale sports wind tunnel testing, along with high-precision sensors, will provide scientific recommendations for the national cycling team athletes. 19 april 2024 sports aerodynamics cyclist in the wind tunnel. prof. zhang xin and dr. li ning. aantc with the chinese national cycling team.","order":594,"static_url":"/post/35/"},{"section":"News","title":"Dr. LI Ning of Viva China Holdings Limited's visit to the Aerodynamics and Acoustics Facility","url":"/post/34/","summary":"Mr. LI Ning of Viva China Holdings Limited visited the Aerodynamics and Acoustics Facility (AAF) on the 22nd of March 2023, where some of MAE’s recent efforts using aerospace science and technologies for aero sports engineering of cycling and windsurfing are made. Prof. ZHOU Pen…","meta":"27 March 2023","search_text":"dr. li ning of viva china holdings limited's visit to the aerodynamics and acoustics facility mr. li ning of viva china holdings limited visited the aerodynamics and acoustics facility (aaf) on the 22nd of march 2023, where some of mae’s recent efforts using aerospace science and technologies for aero sports engineering of cycling and windsurfing are made. prof. zhou peng leads a team of mae students and researchers on developing aerodynamic testing, evaluating and simulation methods and tools for sports performance enhancement. the team works closely with hong kong and mainland partners. the mae team’s effort also extends to outreach activities with local high school students and teachers on stem education. 27 march 2023 sports aerodynamics","order":595,"static_url":"/post/34/"},{"section":"News","title":"HKUST and HKSI Establish Joint Center for Sports Science and Technology to Strengthen Collaboration","url":"/post/33/","summary":"The Hong Kong University of Science and Technology (HKUST) and the Hong Kong Sports Institute (HKSI) celebrated today the inauguration of the HKUST – HKSI Joint Center for Sports Science and Technology (Center). The Center will explore the integration of research and technology …","meta":"10 March 2023","search_text":"hkust and hksi establish joint center for sports science and technology to strengthen collaboration the hong kong university of science and technology (hkust) and the hong kong sports institute (hksi) celebrated today the inauguration of the hkust – hksi joint center for sports science and technology (center). the center will explore the integration of research and technology into sports, promote innovation in sports science and optimize elite athletes’ performance in international competitions. the establishment of the center was built upon a strong foundation of partnership between the parties dated back to 2018, where hkust started collaborating with the hksi to develop state-of-the-art wind tunnel testing capabilities for the development and optimization of low-drag cycling suits and gears for the hong kong cycling team, which had improved training efficiency and contributed to their performances at the tokyo 2020 olympic games. with the launch of the center, hkust’s researchers will further strengthen collaboration with hksi’s sports scientists and engineers as well as coaches on the development of new technologies, sensors, test protocols and analysis tools for sports aerodynamics, advanced training equipment and race simulations. this is aimed to optimize the sports equipment, postures and strategies of elite athletes and achieve critical marginal gains in areas including cycling, triathlon and windsurfing. over 30 representatives from hkust and hksi held the center’s first work meeting after the signing ceremony. hkust faculty presented their latest research findings in the fields of sports aerodynamics, sensors and sports performance monitoring, design and characterization of sports equipment of materials, life science engagement in sports. the two parties have also exchanged on the development, engagement of student athletes as well as internship opportunities for students. 10 march 2023 sports aerodynamics","order":596,"static_url":"/post/33/"},{"section":"News","title":"世盃比賽版足球 傳射更準有數計","url":"/post/32/","summary":"【明報專訊】今屆世界盃採用全新設計的足球Al Rihla，內藏的高靈敏度感應器為多個問題球如Ｃ朗的「上帝之髮」入球、日本翼鋒三笘薰底線助攻未有出界等，提供有力助證。雖然市面上買到的比賽版足球（$1199）未有這塊感應器，但與普通版（$259）相比，售價仍貴3倍有多，踢起來真的有什麼不同嗎？香港科技大學太古航天工程學教授兼空氣動力學和聲學實驗中心主任張欣及其團隊，將兩個足球放入低速風洞大比併，看看到底有什麼分別？ 在談足球設計之前，張欣先解釋影響足球飛行軌迹的一大因素——空氣動力學（aerodynamics），即物體在空氣中運動時所產生的各種阻力、側向力…","meta":"6 December 2022","search_text":"世盃比賽版足球 傳射更準有數計 【明報專訊】今屆世界盃採用全新設計的足球al rihla，內藏的高靈敏度感應器為多個問題球如ｃ朗的「上帝之髮」入球、日本翼鋒三笘薰底線助攻未有出界等，提供有力助證。雖然市面上買到的比賽版足球（$1199）未有這塊感應器，但與普通版（$259）相比，售價仍貴3倍有多，踢起來真的有什麼不同嗎？香港科技大學太古航天工程學教授兼空氣動力學和聲學實驗中心主任張欣及其團隊，將兩個足球放入低速風洞大比併，看看到底有什麼分別？ 在談足球設計之前，張欣先解釋影響足球飛行軌迹的一大因素——空氣動力學（aerodynamics），即物體在空氣中運動時所產生的各種阻力、側向力等。「雖然足球的射傳準確度與運動員的技術有最大關係，但當足球離腳後，影響它飛行軌迹的最重要因素便是空氣動力學。足球在空中飛行主要受兩方面影響，一個是重力，另一個是空氣流動所產生的力，皆影響足球的軌迹。」 他認為要解釋足球的空中運動，可以運用多種原理。首先是伯努利原理（bernoulli's principle），「簡單來說，它說明了當空氣的流動速度愈快，壓力便愈小。因此如果空氣流經足球左右或上下兩邊的速度不一，它的飛行軌迹便會偏向流速快的一邊，而非直線飛行」。 張欣又解釋，空氣流過足球時，並不會完全貼着足球表面，而是在一定的位置後分離，「我們通常稱為流動分離，它會在足球後方形成一個壓力很低的區域，這是足球所受空氣阻力的一個主要來源。低壓區的大小，視乎當時空氣在足球表面流動的狀態是屬於層流（laminar flow）還是湍流（turbulent flow）」。在速度比較低的時候，空氣流動較有規則，分為一層一層，之間不會互相干擾，因而稱為層流；相反速度較高，或者存在表面擾動時，空氣流動就會變成較混亂及捲動的狀態，稱為湍流。「空氣動力學中有一個重要參數『雷諾數』（reynolds number），可用於解釋當球體速度超過某一個臨界值，球表面的流動狀况會發生明顯改變，從有序的層流變成無序的湍流。相應的，流動分離點會往後移動，造成球後方的分離區域減少，阻力亦會隨之下降。」 要分析兩個版本世界盃足球在空氣動力學上的差別，張欣建議在科大空氣動力學和聲學實驗中心的低速風洞實驗室做測試，以量度在不同速度下足球的空氣動力學性能，「在風洞實驗中，我們可以在足球的表面黏貼一些纖維來觀察，氣流速度比較低的時候，可看出這些纖維擺動的方向比較一致，代表空氣流動處於層流狀態；當速度升高，纖維的擺動就變得雜亂無章，代表正受到湍流影響」。 足球周圍空氣流動狀態還可以通過煙流測試來顯示。風速較低時，空氣流動幾乎在足球的中央位置便開始分離；當風速增加，煙流在經過足球的中間點後仍會貼着球面移動，並在稍後位置才分離。先後測試過比賽版及普通版世界盃足球後，科大機械及航空航天工程學系研究助理教授周朋認為，「雖然我們看到比賽版足球的表面有很多結構，包括有較少的縫合坑紋及壓印紋理，但實際上，比賽版足球的空氣阻力與普通版在很多情况下分別不算明顯。」比賽版足球的球速不會與普通版足球有明顯差別。 不過他補充，比賽版足球的設計並非無用，實試中發現在大多數速度下，比賽版足球受到的隨機側向力都較普通版小，因此飛行路線不易改變。另一方面，在流動狀態發生改變的臨界速度區間內，比賽版足球的阻力變化都較普通版平緩。這些特點讓球員在長傳或遠射時，更準確控制傳球及射門位置。 6 december 2022 sports aerodynamics","order":597,"static_url":"/post/32/"},{"section":"News","title":"AANTC PhD student Kwan Pui Mok won the 7th HKASMSS Student Conference Award for Best Presentation","url":"/post/31/","summary":"The 7th Hong Kong Society of Sports Medicine and Science Student Academic Conference and Asian Sports Medicine Association symposium was held at Hong Kong Science and Technology Park from December 4th to 5th. Prof. Xin Zhang delivered a presentation entitled \"Advances in Aero-ba…","meta":"6 December 2021","search_text":"aantc phd student kwan pui mok won the 7th hkasmss student conference award for best presentation the 7th hong kong society of sports medicine and science student academic conference and asian sports medicine association symposium was held at hong kong science and technology park from december 4th to 5th. prof. xin zhang delivered a presentation entitled \"advances in aero-based performance sports engineering research\". as a panel member, dr. zhou peng did the bridging the gap between developers and end users: discussion on \"the obstacles and opportunities\". aantc doctoral student tom kwan pui mok presented an academic report entitled \"computational fluid dynamic simulation for track cycling strategies development\". aantc used computational fluid dynamics to discuss the aerodynamic characteristics in the process of overtaking by single vehicle, which provided a basis for the formulation of overtaking strategy by single vehicle. the presentation was awarded the 1st prize of oral presentation -- sports innovations and sports technology. congratulations, tom! 6 december 2021 sports aerodynamics","order":598,"static_url":"/post/31/"},{"section":"News","title":"AANTC’s project won the \"Tianhe Star\" Outstanding Application Award in 2021","url":"/post/30/","summary":"At the national Supercomputing Guangzhou Center 2021 Supercomputing Innovation and Application Conference held on December 3, the \"Tianhe Star\" Outstanding Application Award was selected after layers of selection. The purpose of the award is to promote the integration and innova…","meta":"6 December 2021","search_text":"aantc’s project won the \"tianhe star\" outstanding application award in 2021 at the national supercomputing guangzhou center 2021 supercomputing innovation and application conference held on december 3, the \"tianhe star\" outstanding application award was selected after layers of selection. the purpose of the award is to promote the integration and innovation of supercomputing and new technologies, and encourage users to explore and make full use of supercomputing resources to carry out research projects with scientific, economic, social and livelihood value. in 2021, the center for research in aerodynamics, acoustics and noise control technologies (aantc) won the award for its research project \"numerical simulation and drag reduction optimization design for single-vehicle aerodynamics\". over the past few years, the research team has applied advanced technologies from aviation and formula 1 racing to competitive sports using advanced computational fluid dynamics methods. special, through cooperation with olympic team, recover the real model of elite athletes, at the same time, combined with advanced sports wind tunnel test measurement, the size of wind speed, cycling posture, cycling equipment, bicycle parts, motion and so on factors to evaluate the overall size of the wind resistance and optimization, to help athletes improve performance effectively, enhance the social influence. in addition, numerical calculation also provides the flow field distribution of different body parts, which helps to optimize the design of cycling clothing. in addition, the team examined the effect of wake characteristics on aerodynamics during overtaking between competitors, providing a basis for the development of effective race measurements. for now, the research team will continue to work with professional sports teams to study the aerodynamics of high-performance sports such as cycling and windsurfing (windsurfing). the results of the research will help coaches and athletes improve their training as well as carry out basic scientific research. 6 december 2021 sports aerodynamics cfd simulation.","order":599,"static_url":"/post/30/"},{"section":"News","title":"Bluff body research reveals the mechanics of surface pattern on drag reduction and sound attenuation","url":"/post/29/","summary":"In cycling sports, the aerodynamic skinsuit plays a significant role as reductions of the aerodynamic drag would improve athlete's performance. Recently, the research team explored the design principles of the aerodynamic skinsuit. By conducting cylinder wind tunnel tests within…","meta":"15 November 2021","search_text":"bluff body research reveals the mechanics of surface pattern on drag reduction and sound attenuation in cycling sports, the aerodynamic skinsuit plays a significant role as reductions of the aerodynamic drag would improve athlete's performance. recently, the research team explored the design principles of the aerodynamic skinsuit. by conducting cylinder wind tunnel tests within the range of cycling speed based reynolds numbers, the research team found the sports fabric with longitudinal grooves can achieve a drag reduction over 50% and a maximum noise attenuation over 15db. the research team also linked such variations to the near-field flow measurements in different flow regimes, revealing the fluid mechanics behind them. this research enables the design of the best aerodynamic skinsuit, helping athletes to improve their performance. the work is published in the reputed fluid dynamics journal physics of fluids. https://doi.org/10.1063/5.0070959 15 november 2021 sports aerodynamics","order":600,"static_url":"/post/29/"},{"section":"News","title":"Windsurfing analysis breaks down propulsion mechanics of sailboards","url":"/post/28/","summary":"Windsurfers often pump their sails back and forth to gain speed, but it can also cause slowing if done incorrectly. The complicated physics of the action was tackled by our group. Recently, the research group examined the propulsive dynamics of sail pumping on sailboards and est…","meta":"12 October 2021","search_text":"windsurfing analysis breaks down propulsion mechanics of sailboards windsurfers often pump their sails back and forth to gain speed, but it can also cause slowing if done incorrectly. the complicated physics of the action was tackled by our group. recently, the research group examined the propulsive dynamics of sail pumping on sailboards and established two quantities that measure the propulsive performance of pumping sails. the work is published on the reputed fluid dynamics journal physics of fluids, and was selected as featured on cover. the aip scilight reported the progress https://aip.scitation.org/doi/10.1063/10.0006710. 12 october 2021 sports aerodynamics windsurfing simulation by aantc.","order":601,"static_url":"/post/28/"},{"section":"News","title":"行政长官祝贺李慧诗勇夺东京奥运铜牌","url":"/post/27/","summary":"AANTC团队为香港单车队精英选手李慧诗进行多轮风洞试验，对骑行姿态、器材、服装进行空气动力学优化，助力李慧诗在二○二○年东京奥运会女子场地单车争先赛中夺得铜牌，行政长官林郑月娥致以热烈祝贺。林郑月娥说：「李慧诗是首名分别于两届奥运会夺得奖牌的香港运动员，她的实力和决心经得起时间考验，成绩斐然，创造香港体坛传奇，全港市民都对她取得的成就感到欣喜。近年香港单车馆为香港单车运动员提供顶级的比赛和训练场地，单车队亦积极和本地大学合作，运用科研成果提升运动员表现。李慧诗和单车队的成功，为体育发展的方向和提升精英运动员培训带来启示，我们一定会更重视这些方面的资源…","meta":"8 August 2021","search_text":"行政长官祝贺李慧诗勇夺东京奥运铜牌 aantc团队为香港单车队精英选手李慧诗进行多轮风洞试验，对骑行姿态、器材、服装进行空气动力学优化，助力李慧诗在二○二○年东京奥运会女子场地单车争先赛中夺得铜牌，行政长官林郑月娥致以热烈祝贺。林郑月娥说：「李慧诗是首名分别于两届奥运会夺得奖牌的香港运动员，她的实力和决心经得起时间考验，成绩斐然，创造香港体坛传奇，全港市民都对她取得的成就感到欣喜。近年香港单车馆为香港单车运动员提供顶级的比赛和训练场地，单车队亦积极和本地大学合作，运用科研成果提升运动员表现。李慧诗和单车队的成功，为体育发展的方向和提升精英运动员培训带来启示，我们一定会更重视这些方面的资源配合。」李慧诗是香港首位女子单车比赛世界冠军，她自二○○四年成为全职运动员，多次出赛为香港扬威国际体坛，包括于二○一○年、二○一四年及二○一八年亚洲运动会在多项赛事取得金牌，以及分别在二○一三年及二○一九年在世界锦标赛夺冠。 8 august 2021 sports aerodynamics 香港单车运动员李慧诗在二○二○年东京奥运会女子场地单车争先赛中为香港夺得铜牌！ 李慧詩在aantc风洞实验室进行训练。 李慧詩在aantc风洞实验室进行训练。","order":602,"static_url":"/post/27/"},{"section":"News","title":"CE congratulates Lee Wai-sze on winning bronze medal at Tokyo Olympics","url":"/post/26/","summary":"AANTC team conducted a multi-round wind tunnel test for Hong Kong cycling athlete Lee Wai-sze, to optimize the riding posture, equipment, and clothing to help her win the bronze medal in the women's track cycling race at the Tokyo Olympic Games in 2020. The Chief Executive, Mrs …","meta":"8 August 2021","search_text":"ce congratulates lee wai-sze on winning bronze medal at tokyo olympics aantc team conducted a multi-round wind tunnel test for hong kong cycling athlete lee wai-sze, to optimize the riding posture, equipment, and clothing to help her win the bronze medal in the women's track cycling race at the tokyo olympic games in 2020. the chief executive, mrs carrie lam, extended her greatest congratulations to her. \"lee wai-sze is the first hong kong athlete who has won medals at two olympic games. she has demonstrated that her competence and determination have passed the test of time, and she has become a hong kong legend with her brilliant results. all hong kong people are overjoyed at her achievements. \"the hong kong velodrome has provided hong kong cycling athletes with a top-notch competition and training venue in recent years. the cycling team has also collaborated with a local university to leverage scientific research achievements to enhance the performance of athletes. the success of lee wai-sze and the cycling team has provided insights into the direction of sports development and training of elite athletes. we will attach more importance to the allocation of resources in these areas,\" mrs lam said. lee wai-sze is the first hong kong world champion in women's cycling competitions. as a full-time athlete since 2004, she has brought hong kong honour in the international sporting arena with outstanding results, including gold medals in various competitions of the asian games in 2010, 2014 and 2018 as well as gold medals at the world championships in 2013 and 2019. 8 august 2021 sports aerodynamics lee wai-sze won a bronze medal in the women's sprint even in the tokyo 2020 olympic games for hk lee wai-sze is training in aantc wind tunnel lee wai-sze is training in aantc wind tunnel","order":603,"static_url":"/post/26/"},{"section":"News","title":"Sarah Lee's wind tunnel test before Tokyo Olympics","url":"/post/25/","summary":"Our Performance Sports Engineering team has been collaborating with Hong Kong Sports Institute to improve the aerodynamic performance of their elite cyclists. Recently, we have done wind tunnel tests for Sarah Lee, one of the top track cyclists in Hong Kong, to prepare for Tokyo…","meta":"27 April 2021","search_text":"sarah lee's wind tunnel test before tokyo olympics our performance sports engineering team has been collaborating with hong kong sports institute to improve the aerodynamic performance of their elite cyclists. recently, we have done wind tunnel tests for sarah lee, one of the top track cyclists in hong kong, to prepare for tokyo olympics. the research activities are greatly supported by mr. adam kwok, executive director of shkp, through his generous donation. 27 april 2021 sports aerodynamics","order":604,"static_url":"/post/25/"},{"section":"News","title":"Ray-tracing of drone noise","url":"/post/20/","summary":"The in-house ENVironmental Acoustic Ray-tracing Code (EnvARC) at the AANTC generates acoustic maps using generalized acoustic sources, generic terrain and building models with user-defined impedances, and resolves the effects of atmospheric sound absorption and refraction. The i…","meta":"25 February 2020","search_text":"ray-tracing of drone noise the in-house environmental acoustic ray-tracing code (envarc) at the aantc generates acoustic maps using generalized acoustic sources, generic terrain and building models with user-defined impedances, and resolves the effects of atmospheric sound absorption and refraction. the inputs consist of the noise source and environmental scenario models as well as the observer positions. the output is the noise exposure map for noise evaluation and abatement. 25 february 2020 drone projects","order":605,"static_url":"/post/20/"},{"section":"News","title":"Variation of the spanwise vorticity on a pitching airfoil","url":"/post/19/","summary":"The instantaneous flow pattern on a pitching airfoil is acquired by a high-speed PIV system, which can achieve the highest sampling rate of 1633Hz. This figure gives the development of the vorticity near the trailing edge during the half pitching cycle.","meta":"25 February 2020","search_text":"variation of the spanwise vorticity on a pitching airfoil the instantaneous flow pattern on a pitching airfoil is acquired by a high-speed piv system, which can achieve the highest sampling rate of 1633hz. this figure gives the development of the vorticity near the trailing edge during the half pitching cycle. 25 february 2020 aeroacoustics","order":606,"static_url":"/post/19/"},{"section":"News","title":"Garment design using advanced CFD techniques","url":"/post/18/","summary":"The studies on the garment are being conducted in the PSE group to provide the most efficient drag reduction design for athletes based on cutting-edge CFD simulations. The flow field varies among different riders due to various figures and body postures. High-resolution CFD simu…","meta":"25 February 2020","search_text":"garment design using advanced cfd techniques the studies on the garment are being conducted in the pse group to provide the most efficient drag reduction design for athletes based on cutting-edge cfd simulations. the flow field varies among different riders due to various figures and body postures. high-resolution cfd simulations can help visualize the wall shear stress from which we can locate the exact position where separation or reattachment occurs. for each flow region, the ad-hoc design can then be applied accordingly. 25 february 2020 sports aerodynamics","order":607,"static_url":"/post/18/"},{"section":"News","title":"Students of AANTC attending AIAA conference in Delft","url":"/post/17/","summary":"PhD students of AANTC attended and presented at 25th AIAA/CEAS Aeroacoustics Conference in Delft, Netherlands. Students presented their own works and shared their research results with scholars all over the world.","meta":"25 February 2020","search_text":"students of aantc attending aiaa conference in delft phd students of aantc attended and presented at 25th aiaa/ceas aeroacoustics conference in delft, netherlands. students presented their own works and shared their research results with scholars all over the world. 25 february 2020 general","order":608,"static_url":"/post/17/"},{"section":"News","title":"Collaboration with HKSI on bicycle aerodynamic research","url":"/post/16/","summary":"PSE team is collaborating with HKSI to help enhance elite cyclists' performance aiming at the Tokyo 2020 Olympics. The collaboration received a donation from Mr Adam KWOK, Executive Director of SHKP. Head cycling coach Mr SHEN Jinkang and the world champion LEE Wai-sze are also …","meta":"25 February 2020","search_text":"collaboration with hksi on bicycle aerodynamic research pse team is collaborating with hksi to help enhance elite cyclists' performance aiming at the tokyo 2020 olympics. the collaboration received a donation from mr adam kwok, executive director of shkp. head cycling coach mr shen jinkang and the world champion lee wai-sze are also highly involved in the program and will provide professional advice on performance improvement. 25 february 2020 sports aerodynamics","order":609,"static_url":"/post/16/"},{"section":"News","title":"Chairman and president of AVIC visited AANTC","url":"/post/15/","summary":"The chairman and president of AVIC visited AANTC in the company of Prof. Xin Zhang and Prof. Wei Shyy. Students from AANTC gave demonstrations of their latest research works, and the academic output from the centre was highly spoken of. The cooperation between AVIC and HKUST sta…","meta":"25 February 2020","search_text":"chairman and president of avic visited aantc the chairman and president of avic visited aantc in the company of prof. xin zhang and prof. wei shyy. students from aantc gave demonstrations of their latest research works, and the academic output from the centre was highly spoken of. the cooperation between avic and hkust starts from 2012 and remarkable success has been achieved especially in aerodynamic and acoustic researches. 25 february 2020 general","order":610,"static_url":"/post/15/"},{"section":"News","title":"Swire Trust visits School of Aeronautical Engineering","url":"/post/14/","summary":"Swire Trust Group visited the School of Aeronautical Engineering with Prof. Zhang for the latest advancement in noise prediction and reduction research from AANTC (01/2018).","meta":"25 February 2020","search_text":"swire trust visits school of aeronautical engineering swire trust group visited the school of aeronautical engineering with prof. zhang for the latest advancement in noise prediction and reduction research from aantc (01/2018). 25 february 2020 general","order":611,"static_url":"/post/14/"},{"section":"News","title":"HKUST Executive Vice-President and Provost visits AANTC","url":"/post/13/","summary":"Professor Wei Shyy, the Executive Vice-President and Provost of HKUST visited the AANTC laboratory accompanied by Prof Xin Zhang and Prof Xun Huang (11/2017). Professor Shyy visited the acoustic and aeroacoustic laboratories. AANTC PhD students briefed Prof. Shyy about their res…","meta":"25 February 2020","search_text":"hkust executive vice-president and provost visits aantc professor wei shyy, the executive vice-president and provost of hkust visited the aantc laboratory accompanied by prof xin zhang and prof xun huang (11/2017). professor shyy visited the acoustic and aeroacoustic laboratories. aantc phd students briefed prof. shyy about their research. 25 february 2020 general","order":612,"static_url":"/post/13/"},{"section":"Opportunities","title":"Research Assistant Expressions of Interest in Aeroacoustics and Low-Noise Design","url":"/career/32/","summary":"AANTC at HKUST welcomes expressions of interest from prospective research assistants who would like to contribute to aeroacoustics and low-noise design for low-altitude aircraft. Future work may involve experimental facilities, numerical tools and artificial intelligence methods…","meta":"Research Assistant","search_text":"research assistant expressions of interest in aeroacoustics and low-noise design aantc at hkust welcomes expressions of interest from prospective research assistants who would like to contribute to aeroacoustics and low-noise design for low-altitude aircraft. future work may involve experimental facilities, numerical tools and artificial intelligence methods developed with the research team. possible contributions include: - building and testing aerodynamic and acoustic experimental systems, including wind-tunnel rigs, sensors and measurement workflows. - supporting aircraft structural design, additive manufacturing, flight-control systems and studies linking flight dynamics with noise emissions. - using wind tunnels, 3d printing facilities and flight simulators where relevant to experimental or design work. - developing noise maps, visualisation tools and data pipelines for low-altitude aircraft and urban environments. - preparing and analysing simulation and measurement data for physics-grounded aeroacoustic world models, with validation against experiments. the team has an established base in aerodynamic and acoustic experiments, noise prediction and engineering software, supported by specialist test facilities and collaborations with industry partners. research assistant work may also lead to further postgraduate study, subject to the relevant admission process. research assistant applicants with a bachelor's or master's degree in aerospace engineering, mechanical engineering, computer science, electrical engineering or a related discipline are welcome to express interest. - experience with cad, structural analysis, cfd, python, c++, matlab or scientific visualisation tools such as opengl or vtk is useful. - practical skills in experimental methods, 3d printing, sensors, embedded systems, flight control or data analysis are an advantage. - ability to write technical reports and communicate in english is expected. mandarin communication skills are an advantage. - experience in engineering design competitions is welcome. applicants need not have experience in every listed area. please send your cv and a brief description of your technical interests to professor peng zhou at pengzhou@ust.hk. this is an expression of interest; availability and appointment details will be discussed with suitable applicants. research assistant","order":613,"static_url":"/career/32/"},{"section":"Opportunities","title":"PhD and Research Staff Opportunities in Aeroacoustics and Low-Noise Design","url":"/career/30/","summary":"AANTC at HKUST invites applications for PhD study and research staff roles in aeroacoustics and low-noise design. The research connects physical understanding of aerodynamic noise with experiments, simulation and artificial intelligence for low-altitude aircraft and the low-alti…","meta":"","search_text":"phd and research staff opportunities in aeroacoustics and low-noise design aantc at hkust invites applications for phd study and research staff roles in aeroacoustics and low-noise design. the research connects physical understanding of aerodynamic noise with experiments, simulation and artificial intelligence for low-altitude aircraft and the low-altitude economy. research directions include: - aerodynamic and aeroacoustic experiments, computation and theory for rotors, aircraft, airframes and engines. - measurement, prediction and assessment of low-altitude aircraft noise and its propagation in urban environments. - low-noise aircraft design, noise-aware flight dynamics and control, and route planning, including how manoeuvres and rotor operating states affect acoustic emissions. - development of physics-grounded world models that combine aeroacoustic measurements and simulations to predict how aircraft, operating conditions and environments affect noise. these models will be evaluated against experimental data and used to explore low-noise design choices. - physics-informed machine learning and artificial intelligence methods for aerodynamic and aeroacoustic modelling. - aerodynamic design of sports equipment and related sports-engineering research. the team builds on established work in aeroacoustics, noise prediction and low-altitude flight. its wind tunnels, acoustic measurement platforms and computational tools support research from physical mechanisms to engineering design. established collaborations with aerospace industry partners connect this work to practical low-noise design. applicants may come from aerospace or mechanical engineering, aeroacoustics, applied mathematics, computer science, artificial intelligence or related disciplines. - phd applicants should be prepared to develop an original research question and work across physical modelling, computation and experimental validation. - research staff applicants should have experience in independent research or engineering development relevant to aeroacoustics, low-noise design, simulation, experiments or data-driven modelling. - experience with cfd, acoustic measurement, scientific computing, machine learning or low-altitude aircraft is an advantage. specific experience in every area is not required. - applicants should be able to communicate research results clearly in english. please send your cv and a brief statement of your research interests to professor peng zhou at pengzhou@ust.hk. indicate whether you are applying for phd study or a research staff role.","order":614,"static_url":"/career/30/"},{"section":"Opportunities","title":"PhD Position in Sports Aerodynamics for Spring or Fall 2027","url":"/career/29/","summary":"One PhD position is available in Sports Aerodynamics at AANTC, HKUST, for entry in Spring or Fall 2027. The research will develop aerodynamic test methods and mechatronic experimental systems for athletes and sports equipment. Research areas include: - Design, fabrication, assem…","meta":"Student","search_text":"phd position in sports aerodynamics for spring or fall 2027 one phd position is available in sports aerodynamics at aantc, hkust, for entry in spring or fall 2027. the research will develop aerodynamic test methods and mechatronic experimental systems for athletes and sports equipment. research areas include: - design, fabrication, assembly, and commissioning of sports aerodynamic test rigs. - wind-tunnel testing and aerodynamic experiments for athletes and sports equipment. - automated flow measurement using robotic systems, including sensor-guided positioning and closed-loop control. - investigate embodied ai methods that connect visual and sensor perception with robotic actions in wind-tunnel experiments, validated through repeatable aerodynamic measurements. - three-dimensional scanning and geometry reconstruction for aerodynamic analysis. - computational fluid dynamics for sports aerodynamics. - embedded sensing, system integration, and motion control for experimental platforms. student - background in mechatronics engineering, aerospace engineering, robotics engineering, automation, or a related discipline, with experience in mechatronic system development. - solid foundation in aerodynamics and fluid mechanics. experience in wind-tunnel testing, aerodynamic experiments, or related research is preferred. - solid background in mechanical design and engineering drawing, with practical experience in the design, fabrication, assembly, and testing of mechanical products or experimental systems. - proficiency in solidworks, creo, ug/nx, or other three-dimensional cad software, with experience in surface modelling. ability to use ansys, adams, or related tools for structural strength and stiffness evaluation, as well as kinematic and dynamic simulation and validation. - experience with stm32 or other mcu-based embedded systems, embedded c/c++, rs485 or can, and system debugging. - practical experience in motion control of stepper motors and robotic joint motors, including motor selection, drive systems, and motion control. - experience in developing complete mechatronic systems or complex experimental platforms is preferred. - experience in robotic perception, computer vision, sensor fusion, or learning-based control is an advantage; prior embodied ai experience is welcome but not required. please send your cv to professor peng zhou at pengzhou@ust.hk. spring or fall 2027 student","order":615,"static_url":"/career/29/"}]
