Roughness-Induced Boundary-Layer Transition on a Hypersonic Capsule-Like Forebody Including Nonequilibrium
Author:
Affiliation:
1. Technical University of Munich, 85748 Garching, Germany
Funder
Deutsche Forschungsgemeinschaft
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Reference44 articles.
1. Summary of Hypersonic Boundary-Layer Transition Experiments on Blunt Bodies with Roughness
2. Real gas effects on hypersonic boundary‐layer stability
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5. Linear disturbances in hypersonic, chemically reacting shock layers
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