Receptivity and Forced Response to Acoustic Disturbances in High-Speed Boundary Layers
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J056145
Reference23 articles.
1. MackL. M. “Boundary Layer Stability Theory,” Jet Propulsion Lab. Rept. JPL 900-277, Rev. A, Pasadena, CA, Nov. 1969.
2. Linear Stability Theory and the Problem of Supersonic Boundary- Layer Transition
3. Interaction between a supersonic boundary layer and acoustic disturbances
4. Sensitivity of a supersonic boundary layer to acoustic disturbances
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