Control of Shock-Induced Separation of a Turbulent Boundary Layer Using Air-Jet Vortex Generators
Author:
Affiliation:
1. RWTH Aachen University, 52062 Aachen, Germany
Funder
Deutsche Forschungsgemeinschaft
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference53 articles.
1. Fifty Years of Shock-Wave/Boundary-Layer Interaction Research: What Next?
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3. SmitsA.DussaugeJ., Turbulent Shear Layers in Supersonic Flow, American Institute of Physics, New York, 1996, pp. 319–363. 10.1007/b137383
4. Shock Wave—Turbulence Interactions
5. Shock Wave–Boundary-Layer Interactions
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