Turbulent Boundary-layer Temperature Recovery Factors in Two-dimensional Supersonic Flow
Maurice Tucker · Stephen H. Maslen
Jan 1951 · National Advisory Committee for Aeronautics
eBook
21
Pages
About this eBook
The analysis indicates that recovery factor decreased with increasing Mach number. For Prandtl numbers considered (0.65 to 0.75), recovery factors at stream Mach numbers of 10 were about 5 percent lower than the limiting values at zero Mach number. Reynolds number effect on recovery factor was of secondary importance. An approximation formulation that represents the computatios to within 1 percent is included for engineering calculations.
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