Boundary-layer receptivity and breakdown in hypersonic flow over a swept blunt wedge with three-dimensional freestream acoustic disturbances
Author:
Affiliation:
1. University of Southampton
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-4247
Reference33 articles.
1. BOUNDARY-LAYER RECEPTIVITY TO FREESTREAM DISTURBANCES
2. Transition and Stability of High-Speed Boundary Layers
3. Receptivity of a Supersonic Boundary Layer to Acoustic Disturbances
4. Boundary-layer receptivity of Mach 7.99 flow over a blunt cone to free-stream acoustic waves
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3. Effects of Wall Temperature on the Evolution of a Large-Amplitude Entropy Wave;Journal of Aerospace Engineering;2020-11
4. Receptivity to Freestream Acoustic Noise in Hypersonic Flow over a Generic Forebody;Journal of Spacecraft and Rockets;2019-03
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