Cinematographic Planar Imaging of a Mach 2 Shock Wave/Turbulent Boundary Layer Interaction-Reference-Cited by-同舟云学术

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Cinematographic Planar Imaging of a Mach 2 Shock Wave/Turbulent Boundary Layer Interaction

Published:2005-01-10 Issue: Volume: Page:
ISSN:
Container-title:43rd AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Bueno Pablo¹,Clemens Neol¹,Dolling David¹,Ganapathisubramani B.¹

Affiliation:

1. University of Texas at Austin

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-441

Reference29 articles.

1. Shock Wave—Turbulence Interactions

2. Fifty Years of Shock-Wave/Boundary-Layer Interaction Research: What Next?

3. High-Speed Turbulent Separated Flows: Consistency of Mathematical Models and Flow Physics

4. Erengil, M. E., and Dolling, D. S. "Physical causes of separation shock unsteadiness in shock wave/turbulent boundary layer interactions", AIAA paper93-3134,July1993.

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