Affiliation:
1. Calspan-UB Research Center
Publisher
American Institute of Aeronautics and Astronautics
Reference74 articles.
1. A study of flow separation in regions of shock wave-boundary layer interaction in hypersonic flow
2. Holden, M.S. "Theoretical and Experimental Studies of Laminar Flow on Separation on Flat Plate-Wedge Compression Surfaces in the Hypersonic Strong Interaction Regime - Final Report", Calspan Report No. AF-1894-A-2 ARL 67-0112, May1967.
Cited by
21 articles.
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