Publications
Conference papers
| Publication | Authors | Year | Type | Venue | Pages | DOI |
|---|---|---|---|---|---|---|
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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. AANTC members: Xin Zhang |
2010 | Conference paper | 16th AIAA/CEAS Aeroacoustics Conference (31st AIAA Aeroacoustics Conference), American Institute of Aeronautics and Astronautics Inc., 2010, article number 2010-3992 | — | 10.2514/6.2010-3992 | |
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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. AANTC members: Xin Zhang |
2009 | Conference paper | 15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference), American Institute of Aeronautics and Astronautics Inc., 2009, article number 2009-3112 | — | 10.2514/6.2009-3112 | |
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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. AANTC members: Xin Zhang |
2009 | Conference paper | 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 | — | 10.2514/6.2009-2216 | |
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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. AANTC members: Xin Zhang |
2009 | Conference paper | Collection of Technical Papers - AIAA Applied Aerodynamics Conference | — | 10.2514/6.2009-3951 | |
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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). AANTC members: Xin Zhang |
2009 | Conference paper | 16th International Congress on Sound and Vibration 2009, ICSV 2009, 2009, p. 2238-2245 | — | — | |
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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. AANTC members: Xin Zhang |
2008 | Conference paper | 14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference), American Institute of Aeronautics and Astronautics Inc., 2008, article number 2008-2817 | — | 10.2514/6.2008-2817 | |
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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. AANTC members: Xin Zhang |
2008 | Conference paper | 14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference), 2008, article number 2008-2877 | — | 10.2514/6.2008-2877 | |
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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. AANTC members: Xin Zhang |
2008 | Conference paper | 14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference), American Institute of Aeronautics and Astronautics Inc., 2008, article number 2008-2961 | — | 10.2514/6.2008-2961 | |
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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. AANTC members: Xin Zhang |
2008 | Conference paper | 14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference), American Institute of Aeronautics and Astronautics Inc., 2008, article number 2008-2964 | — | 10.2514/6.2008-2964 | |
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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. AANTC members: Xin Zhang |
2008 | Conference paper | 14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference), American Institute of Aeronautics and Astronautics Inc., 2008, article number 2008-3044 | — | 10.2514/6.2008-3044 |