Oblique-Shock-Wave/Boundary-Layer Interaction Using Near-Wall Reynolds-Stress Models
Author:
Affiliation:
1. Universite Pierre-et-Marie-Curie, 75252 Paris, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.1984
Reference68 articles.
1. Shock wave/turbulent boundary layer interaction and its control
2. Fifty Years of Shock-Wave/Boundary-Layer Interaction Research: What Next?
3. Comparison of Multiequation Turbulence Models for Several Shock Boundary-Layer Interaction Flows
4. Structure of supersonic turbulent flow past a swept compression corner
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