Unsteadiness of the shock wave structure in attached and separated compression ramp flowfields
Author:
Affiliation:
1. Princeton University, Princeton, NJ
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1983-1715
Reference22 articles.
1. Fluctuating Wall Pressure under a Separated Supersonic Flow
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