Overexpansion Effects on Characteristics of Mach Waves from a Supersonic Cold Jet
Author:
Affiliation:
1. Japan Aerospace Exploration Agency, Sagamihara 229-8510, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J051054
Reference52 articles.
1. Experimental Study and Simulation of Rocket Engine Freejet Noise
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