Drag and lift forces for the thin body in the supersonic flow of the non-equilibrium gas

Abstract

The classical problem of the fluid mechanics is the problem of a supersonic motion around a thin body was generalized to the case of non-equilibrium gas. The drag and lift force coefficients were founded. It is shown that the drag and lift force coefficients in the acoustically active supersonic flow are both decreased

Latex2e, 7pages, 13kb