Quiet-flow Ludwieg tube for high-speed transition research
Author:
Affiliation:
1. Purdue University, West Lafayette, Indiana 47907
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.12434
Reference29 articles.
1. Aerothermodynamics and Transition in High-Speed Wind Tunnels at NASA Langley
2. Boundary layer instability, transition and control
3. On hypersonic boundary-layer stability
4. Suggested Future Directions in High-Speed Transition Experimental Research
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