The drag of a compressible turbulent boundary layer on a smooth flat plate with and without heat transfer
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[1] Robert E. Wilson,et al. Turbulent Boundary-Layer Characteristics at Supersonic Speeds-Theory and Experiment , 1950 .
[2] E. R. V. Driest. The turbulent boundary layer with variable Prandtl number , 1954 .
[3] J. Kaye. SURVEY OF FRICTION COEFFICIENTS, RECOVERY FACTORS, AND HEAT-TRANSFER COEFFICIENTS FOR SUPERSONIC FLOW , 1954 .
[4] F. K. Hill. Boundary-Layer Measurements in Hypersonic Flow , 1956 .
[5] Donald Coles,et al. Measurements of Turbulent Friction on a Smooth Flat Plate in Supersonic Flow , 1954 .
[6] G. Young,et al. THE COMPRESSIBLE BOUNDARY LAYER , 1952 .
[7] Dean R. Chapman,et al. Measurements of Turbulent Skin Friction on Cylinders in Axial Flow at Subsonic and Supersonic Velocities , 1953 .
[8] D. B. Spalding,et al. A new analytical expression for the drag of a flat plate valid for both the turbulent and laminar regimes , 1962 .
[9] V. P. Goddard. Visual Supersonic Flow Patterns by Means of Smoke Lines , 1959 .
[10] R. Korkegi. Transition Studies and Skin-Friction Measurements on an Insulated Flat Plate at a Mach Number of 5.8 , 1956 .
[11] O. Burggraf. The Compressibility Trasnformation and Turbulent-Boundary-Layer Equations , 1962 .
[12] F. K. Hill. Turbulent Boundary Layer Measurements at Mach Numbers from 8 to 10 , 1959 .