Abstract
In this paper we present a general method for calculating turbulent boundary layers in twodimensional flows and investigate its accuracy for compressible flows with heat and mass transfer. The method is based on the ideas of eddy transport coefficients and the numerical solution of the governing equations in differential form. The experimental data considered cover a Mach number range of 0 to 6.7 and include flows with and without pressure gradients. The results indicate good agreement at high Reynolds numbers. At low Reynolds numbers the agreement is not as good, and further work needs to be done in such cases.
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