Three-dimensional hypersonic shock wave/turbulent boundary-layer interactions
Author:
Affiliation:
1. Floret Institute, Palo Alto, California 94303
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.11310
Reference5 articles.
1. Swept shock/boundary-layer interactions - Tutorial and update
2. An experimental study of a three-dimensional shock wave/turbulent boundary-layer interaction at a hypersonic Mach number
3. The hypersonic shock wave-turbulent boundary layer interaction generated by a sharp fin at Mach 8.2
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