Effect of Freestream Noise on Roughness-Induced Transition for a Slender Cone
Author:
Affiliation:
1. Purdue University, West Lafayette, Indiana 47907-1282
2. University of Minnesota, Minneapolis, Minnesota 55455
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.48300
Reference24 articles.
1. Effects of Roughness on Hypersonic Boundary-Layer Transition
2. Review of wind-tunnel freestream pressure fluctuations
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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