Experimental, analytical, and computational methods applied to hypersonic compression ramp flows
Author:
Affiliation:
1. Karman Institute for Fluid Dynamics, B-1640 Rhode St-Genese, Belgium
2. Dornier Luftfahrt GmbH, D-88039 Friedrichshafen 1, Germany
3. Kdrmdn Institute for Fluid Dynamics, B-1640 Rhode St-Genese, Belgium
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.11985
Reference36 articles.
1. Interactions between shock waves and turbulent boundary layers
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