Separation shock dynamics in Mach 5 turbulent interactions induced by cylinders
Author:
Affiliation:
1. University of Texas at Austin, Austin, Texas
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.10323
Reference23 articles.
1. 2Dolling, D. S. and Bogdonoff, S. M. "An Experimental Investigation of the Unsteady Behavior of Blunt Fin-Induced Shock Wave Turbulent Boundary Layer Interactions,"AIAA Paper 81-1287, June 1981.
2. Unsteadiness of the Separation Shock Wave Structure in a Supersonic Compression Ramp Flowfield
3. Unsteadiness of the shock wave structure in attached and separated compression ramp flows
4. Some new aspects of the shock-wave/boundary-layer interaction in compression-ramp flows
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