Aeroacoustic Computation of Cylinder Wake Flow.
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia
2. Kentron International, Hampton, Virginia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.48418
Reference18 articles.
1. On sound generated aerodynamically I. General theory
2. The influence of solid boundaries upon aerodynamic sound
3. Acoustic Radiation from a Stationary Cylinder in a Fluid Stream (Aeolian Tones)
4. Aerodynamic Sound Emission as a Singular Perturbation Problem
5. Contributions to the theory of aerodynamic sound, with application to excess jet noise and the theory of the flute
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