separation, stability, and other properties of compressible laminar boundary layer with pressure gradient and heat transfer

to U) and for flow with a pressure gradient but without heat trsnsfer at the wall (refs.12 and 4).Tbe smal.ysisin the present investigation is based on the assumption of a uniform wall temperature, a Prandtl nuniberof unity, and a linear l-Shock-waveinteraction with the boundary layer, however, is not considered.-..