Author:
Zhang Changxian,Xu Jinglei,Gao Lin,Gao Ge
Reference10 articles.
1. Detailed study of attached and separated compression corner flowfields in high Reynolds number Supersonic Flow[J];Settles;AIAA Journal,1979
2. Settles G S., An Experimental Study of Compressible Turbulent Boundary Layer Separation at High Reynolds Number, Ph. D. Dissertation, Princeton University, Princeton, N. J., Sept. 1975.
3. Settles G S, Dodson L J. Hypersonic shock/boundary-layer interaction database.[R]. NASA-CR-177577,1991.
4. Heat Transfer from Hypersonic Turbulent Flow at a Wedge Compression Corner[J];Elfstrom;Journal of Fluid Mechanics,1972
5. A survey of measurements and measuring techniques in rapidly distorted compressible turbulent boundary layers;Fernholz;AGARDograph,1989
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