Instability Modes in Boundary Layers of an Inclined Cone at Mach 6
Author:
Affiliation:
1. Technical University of Braunschweig
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-2823
Reference19 articles.
1. Flight Data for Boundary-Layer Transition at Hypersonic and Supersonic Speeds
2. Effects of High-Speed Tunnel Noise on Laminar-Turbulent Transition
3. Hypersonic laminar–turbulent transition on circular cones and scramjet forebodies
4. On the generation of sound by supersonic turbulent shear layers
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