Acoustic Effect of Chevrons on Supersonic Jets Exiting Conical Convergent-Divergent Nozzles
Author:
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J051337
Reference48 articles.
1. A numerical study of two-dimensional shock vortex interaction
2. Shock-associated noise in supersonic jets
3. Acoustic near-field properties associated with broadband shock noise
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