Hypersonic Boundary-Layer Transition Experiments in a Mach-6 Quiet Tunnel
Author:
Affiliation:
1. Purdue University
2. University of Minnesota
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-1061
Reference25 articles.
1. Boundary-Layer Stability Calculations for the HIFiRE-1 Transition Experiment
2. Hypersonic laminar–turbulent transition on circular cones and scramjet forebodies
3. Aerothermodynamics and Transition in High-Speed Wind Tunnels at NASA Langley
4. Effects of High-Speed Tunnel Noise on Laminar-Turbulent Transition
5. Flight Data for Boundary-Layer Transition at Hypersonic and Supersonic Speeds
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