Control of Shock-Induced Boundary Layer Separation by High Momentum Blowing
Author:
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-4763
Reference9 articles.
1. Passive Device Flow Control for Normal Shock/Boundary Layer Interactions in External Compression Inlets
2. Supersonic-inlet boundary-layer bleed flow
3. The application of boundary layer suction to suppress strong shock-induced separation in supersonic inlets
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3. Hypersonic flow control of shock wave/turbulent boundary layer interactions using magnetohydrodynamic plasma actuators;Journal of Zhejiang University-SCIENCE A;2020-09
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