Scaling of Two- and Three-Dimensional Shock/Turbulent Boundary-Layer Interactions at Compression Corners
Author:
Affiliation:
1. Princeton University, Princeton, N.J.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.51135
Reference33 articles.
1. Interactions between shock waves and turbulent boundary layers
2. Analysis of Two-Dimensional Interactions Between Shock Waves and Boundary Layers
3. Incipient Separation of a Supersonic Turbulent Boundary Layer at High Reynolds Numbers
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