Boundary-Layer Transition on a Flared Cone in the Texas A&M Mach 6 Quiet Tunnel
Author:
Affiliation:
1. Texas A&M University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-923
Reference13 articles.
1. NASA Langley Mach 6 Quiet Wind-Tunnel Performance
2. Goertler instability and hypersonic quiet nozzle design
3. Transition and Stability of High-Speed Boundary Layers
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