Fluctuating Disturbances in a Mach 5 Wind Tunnel
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Va.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.60763
Reference26 articles.
1. Factors Affecting Transition Reynolds Numbers on Models in Supersonic Wind Tunnels
2. Radiated aerodynamic noise effects on boundary-layer transition in supersonic and hypersonic wind tunnels.
3. Measurements and Correlations of Transition Reynolds Numbers on Sharp Slender Cones at High Speeds
4. Influence of measured freestream disturbances on hypersonic boundary-layer transition
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