Shock wave - Turbulent boundary layer interaction in a three dimensional flow-Reference-Cited by-同舟云学术

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Shock wave - Turbulent boundary layer interaction in a three dimensional flow

Published:1995-01-09 Issue: Volume: Page:
ISSN:
Container-title:33rd Aerospace Sciences Meeting and Exhibit
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Author:

Barberis D,Molton P

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1995-227

Reference39 articles.

1. Settles, G.S. "Swept ShocWBoundary-Layer Interactions-Scaling Laws, Flowfield Structure, and Experimental Methods". Special Course on Shock-WmefBoundary-Layer Interactions in Supersonic and Hypersonic Flows. AGARD Report 792 (August 1993).

2. July 1983;Degrez G.

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1. A review of three-dimensional shock wave–boundary-layer interactions;Progress in Aerospace Sciences;2023-11

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3. Turbulence modelling for separated flows with anisotropy-resolving closures;Philosophical Transactions of the Royal Society of London. Series A: Mathematical, Physical and Engineering Sciences;2000-12-15

4. CFD for aerodynamic turbulent flows: progress and problems;The Aeronautical Journal;2000-08

5. Modelling shock-affected near-wall flows with anisotropy-resolving turbulence closures;International Journal of Heat and Fluid Flow;2000-06

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