6 research outputs found
An Analytical and Experimental Investigation of the Skin Friction of the Turbulent Boundary Layer on a Flat Plate at Supersonic Speeds
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NACA Technical Notes
Report presenting average and local skin-friction coefficients for laminar flow on a plate plate at Mach number 2.4 and compared with the laminar-boundary-layer theory of Chapman and Rubesin. The average skin-friction coefficients were calculated by the momentum-loss method from impact-pressure surveys of the boundary layer
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NACA Technical Notes
Report presenting a review of turbulent-boundary-layer analyses and experimental data for average skin-friction coefficients on a flat plate in high-speed flow. New solutions are presented which show the effect of using a continuous velocity gradient and the effect of the extent of the laminar sublayer on the average skin-friction coefficient