Investigation of shock-induced separation of a turbulent boundary layer using laser velocimetry-Reference-Cited by-同舟云学术

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Investigation of shock-induced separation of a turbulent boundary layer using laser velocimetry

Published:1976-07-14 Issue: Volume: Page:
ISSN:
Container-title:9th Fluid and PlasmaDynamics Conference
language:
Short-container-title:

Author:

MODARRESS D.¹,JOHNSON D.¹

Affiliation:

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

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1976-374

Reference22 articles.

1. Calculation of Turbulent Boundary-Layer Shock-Wave Interaction

2. Layer," AIAA Paper 74-558, 1974. T. 2. Rubesin,M. M., and Marvin, J. G. "Shock

Cited by 5 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Particle image velocimetry measurements of a shock wave/turbulent boundary layer interaction;Experiments in Fluids;2007-06-23

2. Turbulence model assessment for shock wave/turbulent boundary-layer interaction in transonic and supersonic flows;Computers & Fluids;2000-03

3. Wall pressure fluctuations in a supersonic separated compression ramp flowfield;3rd Joint Thermophysics, Fluids, Plasma and Heat Transfer Conference;1982-06-07

4. Wall Shear Stress Measurements in a Shock-Wave Boundary-Layer Interaction;AIAA Journal;1978-07

5. Turbulent wake/shock interaction at Mach 6;16th Aerospace Sciences Meeting;1978-01-16

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