Instability of Hypersonic Boundary Layer on a Wall with Resonating Micro-Cavities
Author:
Affiliation:
1. Moscow Institute of Physics and Technology
2. California Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-373
Reference27 articles.
1. 1Malik, M.R., Zang, T.A., and Bushnell, D.M. "Boundary Layer Transition in Hypersonic Flows," AIAA-90-5232,
2. Flight Data for Boundary-Layer Transition at Hypersonic and Supersonic Speeds
3. Hypersonic laminar–turbulent transition on circular cones and scramjet forebodies
4. Stabilization of Hypersonic Boundary Layers by Porous Coatings
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