Investigation of Second-Mode Instability Attenuation Over Silicon-Carbide Coated Carbon Foam
Author:
Affiliation:
1. Purdue University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-4203
Reference30 articles.
1. Stabilization of Hypersonic Boundary Layers by Porous Coatings
2. Aspects of Hypersonic Boundary Layer Transition Control
3. Problems in high speed flow prediction relevant to control
4. Receptivity of a high-speed boundary layer to acoustic disturbances
5. Experiments on Passive Hypervelocity Boundary-Layer Control Using an Ultrasonically Absorptive Surface
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