Quiet Tunnel Measurements of HIFiRE-5 Boundary-Layer Transition
Author:
Affiliation:
1. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433-7542
2. Purdue University, West Lafayette, Indiana 47907-1282
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J053189
Reference52 articles.
1. Aerodynamic Noise in Supersonic Wind Tunnels
2. Development of a High Reynolds Number Quiet Tunnel for Transition Research
3. Effects of High-Speed Tunnel Noise on Laminar-Turbulent Transition
4. Radiated aerodynamic noise effects on boundary-layer transition in supersonic and hypersonic wind tunnels.
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