Computation of Shock Cell Structure of Dual-Stream Jets for Noise Prediction
Author:
Affiliation:
1. Florida State University, Tallahassee, Florida 32306-4510
2. The Boeing Company, Seattle, Washington 98124
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.37045
Reference32 articles.
1. An experimental study of jet noise part II: Shock associated noise
2. Shock associated noise of supersonic jets from convergent-divergent nozzles
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