Direct Computation of Mach Wave Radiation in an Axisymmetric Supersonic Jet
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/10.2514/2.15
Reference28 articles.
1. Supersonic Jet Noise
2. Structure of supersonic jet flow and its radiated sound
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