Nonweiler, T.2012-09-112012-09-111953-01http://dspace.lib.cranfield.ac.uk/handle/1826/7558A numerical solution is found for the equations governing the motion of a two-dimensional laminar boundary layer, in the absence of a pressure gradient, which would be valid if the flight Mach number is very high (i.e. M2>>1). The effects of surface slip, and the finite thickness of the boundary layer are shown to be negligible if the Reynolds Number (R) exceeds about 105, and are neglected. Continues …enReport