Insights in Turbulence Modeling for Crossing-Shock-Wave/Boundary-Layer Interactions
Author:
Affiliation:
1. ONERA, 31055 Toulouse Cedex 4, France
2. Rutgers University, Piscataway, New Jersey 08854
3. Institute of Theoretical and Applied Mechanics, Novosibirsk, 630090, Russia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1417
Reference40 articles.
1. Shock-Wave/Boundary-Layer Interactions in Supersonic and Hypersonic Flows, R 792, AGARD, Aug. 1993.
2. Flowfield visualization of crossing shock-wave/boundary-layer interactions
3. Interaction strength and model geometry effects on the structure of crossing-shock wave/turbulent boundary-layer interactions
4. Structure of crossing-shock-wave/turbulent-boundary-layer interactions
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