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adiabatic wall assumed Baronti-Libby behavior boundary layer flow choice closure principle coefficient Comparison of Theory corresponding CP flow CP formulation Crocco integral cutoff point Data of Res density described in Appendix developed dp/dx equation evaluated exhibit experimental data flat plate flow variables form of transformation free stream total heat transfer Jacobian Mach number mass transfer modification modified transformation momentum thickness Reynolds normal coordinates normal pressure gradient ordinary differential equations OVRIDE card PILOT 2 program potential flow power law present analysis present method presented in Reference pressure gradient effects procedure restricted shown in Figure skin friction Spalding-Chi static pressure stream function streamwise coordinate stretching parameter sub-layer term Theory with Data Theory with Velocity thickness Reynolds numbers Thousands 100 Figure tion turbulent boundary layer utilized values Velocity Profile Data viscous layer wake parameter wake region wall to free zero pressure gradient