Investigation of a hypersonic viscous shock layer on rotating axisymmetric bodies in the presence of blowing (Q1082203)

The hypersonic flow of a laminar stream of viscous compressible gas past blunt axisymmetric bodies rotating about the longitudinal axis is considered. It is assumed that gas blows from the surface of the body. The solution of the problem is obtained by a finite-difference method in a wide range of Reynolds numbers and blowing and rotation parameters. Some results of the calculations characterizing the effect of the rotation on the velocity and temperature profiles across the shock layer, on the friction and heat transfer coefficients, and the shock wave separation are given for the neighborhood of the stagnation point.