INVESTIGATION OF THE SYSTEM OF EQUATIONS OF THE LAMINARY BOUNDARY LAYER IN A COMPRESSIBLE GAS NEAR THE STAGNATION LINE

摘要

In this work there is investigated a system of equations of the laminar boundary layer in a compressible gas near the stagnation (critical) line0 The physical properties of the gas are assigned functions of the temperature.nA system of equations is obtained relative to the friction “(o) and the heat flux g' (0) in such a way that the precision of these values does not depend on the magnitude of the parameter of the in-blowing into the boundary layer.