Goertler instability and hypersonic quiet nozzle design
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681
2. George Washington University, Hampton, Virginia 23681
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.11525
Reference27 articles.
1. Radiated aerodynamic noise effects on boundary-layer transition in supersonic and hypersonic wind tunnels.
2. Boundary-layer transition on a 10-deg cone - Wind tunnel/flight correlation
3. Effects of Wind Tunnel Disturbances on Boundary-Layer Transition with Emphasis on Radiated Noise: A Review
4. Influence of measured freestream disturbances on hypersonic boundary-layer transition
5. Hypersonic boundary-layer transition in the presence of wind-tunnel noise.
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