Time-Resolved Visualization of Instability Waves in a Hypersonic Boundary Layer
Author:
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J051112
Reference18 articles.
1. Transition on a slender cone in hypervelocity flow
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4. Effects of High-Speed Tunnel Noise on Laminar-Turbulent Transition
5. Measurement of Hypersonic Boundary Layer Transition on Cone Models in the Free-Piston Shock Tunnel HIEST
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