Aeroacoustic Analysis of a Simplified Landing Gear
Author:
Affiliation:
1. NASA Langley Research Center
2. High Technology Corporation
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-3111
Reference9 articles.
1. A Comparison of Ffowcs Williams-Hawkings Solvers for Airframe Noise Applications
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3. Linear Acoustic Formulas for Calculation of Rotating Blade Noise
4. Landing Gear Aerodynamic Noise Prediction Using Unstructured Grids
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