Publication | Closed Access
The drag of a compressible turbulent boundary layer on a smooth flat plate with and without heat transfer
384
Citations
12
References
1964
Year
AeroacousticsEngineeringFluid MechanicsMechanical EngineeringTurbulenceDrag CoefficientBoundary LayerUnsteady FlowCompressible FlowNumerical SimulationTransport PhenomenaThermodynamicsNew ProcedureTheoretical TreatmentsSmooth Flat PlateHeat TransferMultiphase FlowAerospace EngineeringTurbulent Flow Heat TransferTurbulence ModelingAerodynamics
The theoretical treatments given by earlier authors are classified, reviewed and where necessary extended; then the predictions of twenty of these theories are evaluated and compared with all available experimental data, the root-meansquare error being computed for each theory. The theory of van Driest-II gives the lowest root-mean-square error (11.0%). A new calculation procedure is developed from the postulate that a unique relation exists between c f F c and RF R where c f is the drag coefficient, R is the Reynolds number, and F c and F R are functions of Mach number and temperature ratio alone. The experimental data are found to be too scanty for both F c and F R to be deduced empirically, so F c is calculated by means of mixing-length theory and F R is found semi-empirically. Tables and charts of values of F c and F R are presented for a wide range of M G and T S / T G . When compared with all experimental data, the predictions of the new procedure give a root-mean-square error of 9.9%.
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