Wedge-induced turbulent boundary-layer separation on a roughened surface at Mach 6.0

作者: P. J. Disimile , N. E. Scaggs

DOI: 10.2514/3.26293

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参考文章(12)
Anthony W. Fiore, C. H. Law, Aerodynamic Calibration of the Aerospace Research Laboratories' M=6 High Reynolds Number Facility Defense Technical Information Center. ,(1975) , 10.21236/ADA012201
DANIEL C. REDA, FRANCIS C. KETTER, CHIEN FAN, Compressible Turbulent Skin Friction on Rough and Rough/ Wavy Walls AIAA Journal. ,vol. 13, pp. 553- 554 ,(1975) , 10.2514/3.49761
P. DISIMILE, N. SCAGGS, The effect of separation on turbulent boundary layer characteristicsover a smooth surface at Mach 6.0 Flight Simulation Technologies Conference and Exhibit. ,(1990) , 10.2514/6.1990-3028