Shock-wave/boundary-layer interactions with bleed through rows of holes
Author:
Affiliation:
1. Carnegie-Mellon University, Pittsburgh, Pennsylvania 15213-3890
2. NASA Ames Research Center, Moffett Field, California 94035
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.24016
Reference23 articles.
1. Shock wave/turbulent boundary layer interaction and its control
2. Survey of validation data base for shockwave boundary-layer interactions in supersonic inlets
3. Experimental and numerical investigation of an oblique shock wave/turbulent boundary layer interaction with continuous suction
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1. Effects of Number of Bleed Holes on Shock-Wave/Boundary-Layer Interactions in a Transonic Compressor Stator;Journal of Thermal Science;2024-01-10
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