Abstract

Three-dimensional flow over smooth blunted bodies of a hypersonic stream of a homogeneous viscous gas in the presence of injection or suction is considered. A numerical solution is obtained for the problem in a wide range of Reynolds numbers and of injection (suction) parameters. Velocity and temperature profiles across the shock layer are presented, as well as the dependence of the coefficients of friction and heat transfer at the body surface, on the Reynolds number and the injection (suction) parameter; the dependence on the injection parameter is universal. An approximate analytic solution of the problem, which is in satisfactory agreement with the numerical solution for low Reynolds numbers is obtained using the integral method of successive approximations.

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