Shock-wave reflection from a turbulent boundary layer with mass bleed.
Author:
Affiliation:
1. The Boeing Company, Seattle, Wash.
2. University of Washington, Seattle, Wash.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.43967
Reference12 articles.
Cited by 12 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. Survey of validation data base for shockwave boundary-layer interactions in supersonic inlets;Journal of Propulsion and Power;1991-07
2. Shock-wave-turbulent-boundary-layer interaction and its control: A survey of recent developments;Sadhana;1988-02
3. Shock wave/turbulent boundary layer interaction and its control;Progress in Aerospace Sciences;1985
4. Bleed Effects on ShockA3oundary-layer Interactions in Supersonic Mixed Compression Inlets;Journal of Aircraft;1977-02
5. Control of shock-wave boundary-layer interactions by bleed in supersonic mixed compression inlets;11th Propulsion Conference;1975-08-16
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