Landing gear aerodynamic noise prediction using unstructured grids

Author:

Souliez F.1,Long L.,Morris P.,Sharma A.

Affiliation:

1. Pennsylvania State Univ., University Park

Publisher

American Institute of Aeronautics and Astronautics

Reference22 articles.

1. Computational aeroacoustic analysis of slat trailing-edge flow

2. Sound Radiation from Aircraft Wheel-WelVLanding-Gear Configurations

3. 5Dobrzynski, W. M. and Buchholz, H. "Full-Scale Noise Testing on Airbus Landing Gears in the German Dutch Wind Tunnel", AIAA-97-1597.

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1. Acoustics and Surface Pressure Measurements from Tandem Cylinder Configurations;20th AIAA/CEAS Aeroacoustics Conference;2014-06-13

2. Numerical Investigation of a Realistic Nose Landing Gear;20th AIAA/CEAS Aeroacoustics Conference;2014-06-13

3. Airframe Noise Prediction with Installed Landing Gear for a Complete Aircraft;15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference);2009-05-11

4. RETRACTED: A component-based model for aircraft landing gear noise prediction;Journal of Sound and Vibration;2008-05

5. Introduction. Computational aerodynamics;Philosophical Transactions of the Royal Society A: Mathematical, Physical and Engineering Sciences;2007-05-22

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