Transition of compressible high enthalpy boundary layer flow over a flat plate
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R. G. Morgan | R. Morgan | Y. He | Y. He
[1] G. Rushton,et al. Shock tunnel investigation of boundary-layer transition at M equals 5.5. , 1966 .
[2] Roddam Narasimha,et al. The laminar-turbulent transition zone in the boundary layer , 1985 .
[3] G. T. Coleman,et al. A Correlation between Pressure and Heat Transfer Distributions at Supersonic and Hypersonic Speeds , 1975 .
[4] C. J. Schueler,et al. Radiated aerodynamic noise effects on boundary-layer transition in supersonic and hypersonic wind tunnels. , 1969 .
[5] F. K. Owen,et al. Transition experiments on a flat plate at subsonic and supersonic speeds , 1969 .
[6] S. Newman,et al. Pressurized aerosols inhaled through extension devices , 1983 .
[7] Roddam Narasimha,et al. Some properties of boundary layer flow during the transition from laminar to turbulent motion , 1958, Journal of Fluid Mechanics.
[8] G. B. Schubauer,et al. Laminar-boundary-layer oscillations and transition on a flat plate , 1947 .
[9] J. Murphy,et al. Flat plate boundary layer transition at hypersonic speeds , 1965 .
[10] R. J. Stalker,et al. Driver gas contamination in a high-enthalpy reflected shock tunnel , 1978 .
[11] J. M. Kendall. Wind Tunnel Experiments Relating to Supersonic and Hypersonic Boundary-Layer Transition , 1974 .
[12] B. Richards,et al. Further experiments on transition reversal at hypersonic speeds. , 1966 .
[13] Rg Morgan,et al. The University of Queensland free piston shock tunnel T-4: Initial operation and preliminary calibration , 1988 .
[14] G. B. Schubauer,et al. Laminar Boundary-Layer Oscillations and Stability of Laminar Flow , 1947 .
[15] R. Ross. Influence of Total Temperature on Transition in Supersonic Flow , 1973 .
[16] J. R. Moselle,et al. Computer program for the numerical solution of nonequilibrium expansions of reacting gas mixtures , 1966 .
[17] A. M. Cary. Turbulent boundary-layer heat transfer and transition measurements for cold-wall conditions at Mach 6. , 1968 .
[18] J. Kendall. Wind Tunnel Experiments Relating to Supersonic and Hypersonic Boundary-Layer Transition , 1974 .
[19] Samuel R. Pate. Effects of Wind Tunnel Disturbances on Boundary-Layer Transition with Emphasis on Radiated Noise: A Review , 1980 .
[20] Eli Reshotko,et al. BOUNDARY LAYER STABILITY AND TRANSITION , 1976 .
[21] I. E. Beckwith,et al. Boundary-layer transition on a cone and flat plate at Mach 3.5 , 1989 .
[22] C. S. Wells. Effects of freestream turbulence on boundary- layer transition. , 1967 .
[23] F. Smith,et al. Surface-cooling effects on compressible boundary-layer instability , 1990 .
[24] D. Capriotti,et al. Viscous optimized hypersonic waveriders , 1987 .
[25] F. K. Owen,et al. Comparison of Wind Tunnel Transition and Freestream Disturbance Measurements , 1975 .
[26] G. Messing,et al. YBa2Cu3O7−x Superconductor powder synthesis by spray pyrolysis of organic acid solutions , 1991 .
[27] B. J. Abu-Ghannam,et al. Natural Transition of Boundary Layers—The Effects of Turbulence, Pressure Gradient, and Flow History , 1980 .
[28] E. R. V. Driest,et al. Calculation of the Stability of the Laminar Boundary Layer in a Compressible Fluid on a Flat Plate with Heat Transfer , 1952 .