Roughness-Induced Instabilities and Transition on a Generic Hypersonic Forebody at Mach 6
Author:
Affiliation:
1. Université Paris Saclay, F-92190, Meudon, France
2. Université de Toulouse, F-31055 Toulouse, France
3. University of Southampton, Southampton, England SO17 1BJ, United Kingdom
4. MBDA-France, 92350 Le Plessis-Robinson, France
Funder
GENCI-CINES
Direction Générale de l'Armement
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J059972
Reference36 articles.
1. Effects of Roughness on Hypersonic Boundary-Layer Transition
2. Hypersonic Boundary-Layer Transition: Application to High-Speed Vehicle Design
3. Linear modal instabilities of hypersonic flow over an elliptic cone
4. Crossflow instability in a hypersonic boundary layer
5. Secondary Instability of Stationary Crossflow Vortices on an Inclined Cone at Mach 6
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