Flow physics of a normal-hole bled supersonic turbulent boundary layer
Author:
Affiliation:
1. University of Cambridge
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-526
Reference37 articles.
1. 1Syberg, J. and Hickcox, T. E. “Design of a Bleed System for a Mach 3.5 Inlet,” Tech. Rep. January, 1973.
2. Control of shock-wave boundary-layer interactions by bleed in supersonic mixed compression inlets
3. Survey of validation data base for shockwave boundary-layer interactions in supersonic inlets
4. Flowfield measurements in a normal-hole-bled oblique shock-wave and turbulent boundary-layer interaction
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