The Reynolds Number Effect on Receptivity to a Localized Disturbance in a Hypersonic Boundary Layer
Author:
Affiliation:
1. University of Arizona, Tucson
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-4246
Reference32 articles.
1. Transition and Stability of High-Speed Boundary Layers
2. 3Schubauer, G. B. and Klebanoff, P. S. "Contributions on the mechanics of boundary layer transition," NACA Technical Report 1289, 1956.
3. Experimental Investigation of Laminar-Turbulent Transition Process in Supersonic Boundary Layer Using Controlled Disturbances
4. Three-dimensional spatial normal modes in compressible boundary layers
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