Boundary-Layer Instability Measurements in a Mach-6 Quiet Tunnel
Author:
Affiliation:
1. Purdue University
2. Perude University
3. Perdue University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-3147
Reference40 articles.
1. Hypersonic laminar–turbulent transition on circular cones and scramjet forebodies
2. Aerothermodynamics and Transition in High-Speed Wind Tunnels at NASA Langley
3. Effects of High-Speed Tunnel Noise on Laminar-Turbulent Transition
4. Flight Data for Boundary-Layer Transition at Hypersonic and Supersonic Speeds
5. The Mach 6 Quiet Tunnel at Texas A&M: Quiet Flow Performance
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