An investigation of interactions between normal shocks and transitional boundary layers-Reference-Cited by-同舟云学术

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An investigation of interactions between normal shocks and transitional boundary layers

Published:2014-06-13 Issue: Volume: Page:
ISSN:
Container-title:44th AIAA Fluid Dynamics Conference
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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/10.2514/6.2014-3334

Reference21 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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1. WP-1 Reference Cases of Laminar and Turbulent Interactions;Notes on Numerical Fluid Mechanics and Multidisciplinary Design;2020-07-31

2. Numerical Investigation of Transitional Shock-Wave/Boundary-Layer Interaction in Supersonic Regime;AIAA Journal;2018-07

3. Influence of Boundary-Layer State on Development Downstream of Normal Shock Interactions;AIAA Journal;2018-06

4. Hypersonic Shock Wave Transitional Boundary Layer Interactions - A Review;47th AIAA Fluid Dynamics Conference;2017-06-02

5. Study of the Dynamics of Transitional Shock Wave-Boundary Layer Interactions using Optical Diagnostics;47th AIAA Fluid Dynamics Conference;2017-06-02

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