Hypersonic Transitional Boundary Layers
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference13 articles.
1. On Supersonic Wind Tunnels With Low Free-Stream Disturbances
2. Aerodynamic Noise in Supersonic Wind Tunnels
3. Radiated aerodynamic noise effects on boundary-layer transition in supersonic and hypersonic wind tunnels.
4. Unusual boundary-layer transition results on cones in hypersonic flow.
5. Observations on the influence of ambient pressure on boundary-layer transition.
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