Aeroacoustic Scattering Using a Particle Accelerated Computational Fluid Dynamics/Boundary Element Technique
Author:
Affiliation:
1. UNSW Australia, Sydney, New South Wales 2052, Australia
2. Technische Universität München, 85748 Garching bei München, Germany
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J054260
Reference38 articles.
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5. On sound generated aerodynamically I. General theory
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