Stability of Hypersonic Boundary Layers over a Compression Corner
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681
2. Old Dominion University, Norfolk, Virginia 23529
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.3479
Reference17 articles.
1. Experimental investigation of supersonic laminar, two-dimensional boundary-layer separation in a compression corner with and without cooling.
2. Similitude Properties of High-Speed Laminar and Turbulent Boundary-Layer Incipient Separation
3. Computation of laminar hypersonic compression-corner flows
4. Validation procedure for the analysis of shock-wave/boundary-layer interaction problems
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