Unsteady nature of shock-wave/turbulent boundary-layer interaction
Author:
Affiliation:
1. Princeton University, Princeton, New Jersey
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.9870
Reference23 articles.
1. 4Winkelman, A.E. "Experimental Investigation of a Fin Protuberance Partially Immersed in a Turbulent Boundary Layer at Mach 5," NOLTR-72-33, Jan.1972.
2. Fluctuating Wall Pressure under a Separated Supersonic Flow
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