Exhaust Nozzle Plume Effects on Sonic Boom
Author:
Affiliation:
1. NASA John H. Glenn Research Center at Lewis Field, Cleveland, Ohio 44135
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031305
Reference7 articles.
1. WIND - The production flow solver of the NPARC Alliance
2. Analysis of Plume Effects on Sonic Boom Signature for Isolated Nozzle Configurations
3. Wind Tunnel Testing of a Sonic Boom Minimized Tail-Braced Wing Transport Configuration
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