Studies of surface roughness and blowing effects on hypersonic turbulent boundary layers over slender cones
Author:
Affiliation:
1. Calspan-UB Research Center, Buffalo, NY
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1989-458
Reference44 articles.
1. Transition and Surface Roughness Effects in Hypersonic Flow," Final Report, AFOSR Contract No. F49620-82-C-0026, October 1983.
2. Combined influence of roughness and mass transfer on turbulent skin friction at Mach 2.9
3. Boundary-layer displacement and leading-edge bluntness effects on attached and separated laminar boundary layers in a compression corner. II - Experimental study
4. Holden, M.S., Shock Wave Turbulent-Boundary Layer Interaction in Hypersonic Flow, AIAA 77-45.
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