Numerical Prediction of Supersonic Shock-Boundary Layer Interaction-Reference-Cited by-同舟云学术

Numerical Prediction of Supersonic Shock-Boundary Layer Interaction

Published:2011-01-04 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Bhagwandin Vishal¹,DeSpirito James¹

Affiliation:

1. Army Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-859

Reference15 articles.

1. Bardin, J E, Coakley, T J, "Three-Dimensional Navier-Stokes Simulations with Two-Equation Turbulence Models of Intersecting Shock-Waves/Turbulent BoundaryLayer at Mach 8.3," AIAA 94-1905,June1994

2. Reynolds-Stress-Transport Modeling for Compressible Aerodynamics Applications

3. Benek, J A, "Lessons Learned from the 2010 AIAA Shock Boundary Layer Interaction Prediction Workshop," AIAA 2010-4825, June/July 2010

4. Benek,JA,"Overviewofthe2010AIAAShockBoundaryLayerInteractionPredictionWorkshop,"AIAA2010-4821,July2010

5. Predictions of Channel and Boundary-Layer Flows with a Low-Reynolds-Number Turbulence Model

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