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Aeroacoustics
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 acr....
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An experimental and computational investigation was carried out to determine the aerodynamics and aeroacoustics of a flap side-edge.....
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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 maximu....
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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 ....
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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 influen....
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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 c....
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