Abstract:
Parametric analysis has been performed, and dependences characterizing the variation of thermal flows and coefficients of the ascensional force and drag force acting on a “magnetized” blunted cone in a hypersonic flow of rarefied plasma have been obtained for a wide range of Stewart numbers. Under the conditions of the MHD approximation, effects inherent to the MHD interaction of a blunted cone with a hypersonic air flow under continuum streamlining of the cone are shown to take place for a blunted cone in a hypersonic flow of rarefied plasma.