INTERPHASE HEAT AND MASS TRANSFER BEHIND A SHOCK WAVE SLIDING ALONG A FILM OF LIQUID FUEL.

The gasdynamic parameters on the surface of a liquid-fuel film along which a shock wave propagates in the gaseous oxidizer are determined in this paper. It is assumed that a plane shock wave moves in a gaseous oxidizer at rest with constant velocity U//S parallel to the boundary of liquid fuel with initial temperature T//0, and that p//1 and T//1 are the pressure and temperature, respectively, of the gaseous oxidizer, occupying half-space y greater than 0 ahead of the shock wave.