Comparison of Unsteady Flow Similarities in Various Shock/Boundary-Layer Interaction Configurations
Author:
Affiliation:
1. University of Arizona, Tucson
2. Imperial College London
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2017-0986
Reference41 articles.
1. Progress in Astronautics & Aeronautics;Settles G. S.,1992
2. Some Advances in Research of Shock Wave Turbulent Boundary Layer Interactions
3. Self-sustained shock oscillations on airfoils at transonic speeds
4. 4Dailey, C. L., Supersonic diffuser instability, Ph.D. thesis,California Institute of Technology, 1954.
5. Fifty Years of Shock-Wave/Boundary-Layer Interaction Research: What Next?
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