Large-Eddy Simulation of an Oblique Shock Impinging on a Turbulent Boundary Layer-Reference-Cited by-同舟云学术

Large-Eddy Simulation of an Oblique Shock Impinging on a Turbulent Boundary Layer

Published:2010-06-28 Issue: Volume: Page:
ISSN:
Container-title:40th Fluid Dynamics Conference and Exhibit
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Author:

Morgan Brandon¹,Kawai Soshi¹,Lele Sanjiva¹

Affiliation:

1. Stanford University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-4467

Reference45 articles.

1. 1Settles, G.S., Fitzpatrick, T., and Bogdonoff, S.M.Detailed Study of Attached and Separated Compression Corner Flowfieldsin High ReynoldsNumber SupersonicFlow,‖ AIAA Journal,Vol. 17, No.6,1979,pp.579-585.

2. 2Zheltovodov, A.A.,Advances and Problems in Modeling of Shockwave Turbulent Boundary Layer Interactions,‖ Proceedings of the International Conference on the Methods of Aerophysical Research, Institute of Theoretical and Applied Mechanics, Novosibirsk, Russia,2004,pp.149-157.

3. Low-frequency dynamics of shock-induced separation in a compression ramp interaction

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