Numerical Study on Wall Temperature Effects on Shock Wave/Turbulent Boundary-Layer Interaction
Author:
Affiliation:
1. State Key Laboratory of High-Temperature Gas Dynamics, 100190 Beijing, People’s Republic of China
2. China Aerodynamics Research and Development Center, 621000 Mianyang, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J054939
Reference25 articles.
1. Fifty Years of Shock-Wave/Boundary-Layer Interaction Research: What Next?
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3. Progress in shock wave/boundary layer interactions
4. LarchevêqueL.DupontP.MartelE. D.GarnierE.DebièveJ. F., Experimental and Numerical Study of Unsteadiness in Boundary Layer/Shock Wave Interaction/Turbulence and Interactions, Springer–Verlag, Berlin, 2010, pp. 263–269.
5. Skin Friction and Heat Flux Measurements in Shock/Boundary Layer Interaction Flows
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