Disturbances from Shock/Boundary Layer Interactions Affecting Upstream Hypersonic Flow
Author:
Affiliation:
1. Purdue University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-4897
Reference22 articles.
1. Hypersonic laminar–turbulent transition on circular cones and scramjet forebodies
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4. Flight Data for Boundary-Layer Transition at Hypersonic and Supersonic Speeds
5. S. P.Wilkinson, S.G.Anders, andF.J. Chen. Status of Langley quiet flow facility developments. Paper 94-2498, AIAA, June
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