Shock wave-turbulent boundary layer interactions in rectangular channels. II - The influence of sidewall boundary layers on incipient separation and scale of the interaction-Reference-Cited by-同舟云学术

Shock wave-turbulent boundary layer interactions in rectangular channels. II - The influence of sidewall boundary layers on incipient separation and scale of the interaction

Published:1973-01-10 Issue: Volume: Page:
ISSN:
Container-title:11th Aerospace Sciences Meeting
language:
Short-container-title:

Author:

REDA D.¹,MURPHY J.¹

Affiliation:

1. NASA, Ames Research Center, Moffett Field, Calif.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1973-234

Reference9 articles.

1. Survey of viscous interactions associated with high Mach number flight

2. Shock wave-turbulent boundary layer interactions in rectangular channels

3. Green, 3. E. "Interactions Between Shock Waves and Turbulent Boundary Layers," i n Progress i n Aerospace Sciences, vol.11, pp.235-340, Pergamon Press, 1970.

4. Interactions Between Wholly Laminar or Wholly Turbulent Boundary Layers and Shock Waves Strong Enough to Cause Separation

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