Influence of transition on the flow downstream of normal shock wave--boundary layer interactions-Reference-Cited by-同舟云学术

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Influence of transition on the flow downstream of normal shock wave--boundary layer interactions

Published:2016-01-02 Issue: Volume: Page:
ISSN:
Container-title:54th AIAA Aerospace Sciences Meeting
language:
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Author:

Davidson Todd S.¹,Babinsky Holger¹

Affiliation:

1. University of Cambridge

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-0044

Reference22 articles.

1. Shock wave/turbulent boundary layer interaction and its control

2. Shock Wave–Boundary-Layer Interactions

3. 5Sawyer, W. G. and Long, C. J. “A Study of Normal Shock-Wave Turbulent Boundary-Layer Interactions at Mach Numbers of 1.3, 1.4 and 1.5,” Tech. Rep. 82099, NASA, 1982.

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