Shock curvature effect on the outer edge conditions of a laminar boundary layer
Author:
Affiliation:
1. Republic Aviation Corporation, Farmingdale, N. Y.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.2184
Reference10 articles.
1. Townsend, A. A., The Structure of Turbulent Shear Flow (Cambridge University Press, Cambridge, England, 1956), Chap. VII, pp.169-171.
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1. Hypersonic turbulent boundary-layer parameters on spherically blunted cones, including entropy-layer swallowing and real-gas effects;16th Thermophysics Conference;1981-06-23
2. Real-Gas Scale Effects on Shuttle Orbiter Laminar Boundary-Layer Parameters;Journal of Spacecraft and Rockets;1977-05
3. Experimental investigation of the effects of nose bluntness, free-stream unit Reynolds number, and angle of attack on cone boundary layer transition at a Mach number of 6;10th Aerospace Sciences Meeting;1972-01-17
4. Stability of density stratified rotating flows.;AIAA Journal;1969-01
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