Author:
Liu Jian-xin,Luo Ji-sheng
Publisher
Springer Science and Business Media LLC
Subject
Applied Mathematics,Mechanical Engineering,Mechanics of Materials
Reference14 articles.
1. Fischer, M. C. An Experimental Investigation of Boundary-Layer Transition on a 10° Half-angle Cone at Mach 6.9, NASA-TN-D-5766 (1970)
2. Martellucci, A., Neff, R. S., and True, W. H., III. An Experimental Investigation of Boundary Layer Transition on a Cone at Angle of Attack, SAMSO TR-69-383 (1969)
3. Muir, J. F. and Trujillo, A. A. 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. The 10th Aerospace Sciences Meeting of AIAA, AIAA-1972-216, San Diego, California, Jan. 17–19, 1972 (1972)
4. Stetson, K. F., Thompson, E. R., Donaldson, J. C., and Siler, L. G. Laminar boundary layer stability experiments on a cone at Mach 8. I — sharp cone. The 16th Fluid and Plasma Dynamics Conference of AIAA, AIAA-1983-1761, Danvers, MA, July 12–14, 1983 (1983)
5. Stetson, K. F., Thompson, E. R., Donaldson, J. C., and Siler, L. G. Laminar boundary layer stability experiments on a cone at Mach 8. III — sharp cone at angle of attack. The 23rd Aerospace Sciences Meeting of AIAA, AIAA-1985-492, Reno, NV, Jan. 14–17, 1985 (1985)
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