Viscous slipstream flow downstream of a centerline Mach reflection
Author:
Affiliation:
1. Jet Propulsion Laboratory, Pasadena, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.6486
Reference13 articles.
1. Efficiency of Supersonic Nozzles for Rockets and Some Unusual Designs
2. Investigation of Supersonic Flow Separation in Nozzles
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