Computation of quadrupole noise using acoustic analogy
Author:
Affiliation:
1. Stanford University, Stanford, California 94305
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.13387
Reference23 articles.
1. On sound generated aerodynamically I. General theory
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5. Structure of supersonic jet flow and its radiated sound
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