Experimental investigation of normal-shock/turbulent-boundary-layer interactions with and without mass removal
Author:
Affiliation:
1. McDonnell Douglas Research Laboratories, St. Louis, Missouri 63166
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.10926
Reference12 articles.
1. Shock wave/turbulent boundary layer interaction and its control
2. 5Wong, W. F. "The Application of Boundary Layer Suction to Suppress Strong Shock-Induced Separation in Supersonic Inlets," AIAA Paper 74-1063, Oct.1974.
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