Technique of Calculation of Two-Phase Flow Parameters Behind the Nozzle Oblique Section

A technique is proposed to calculate the velocity and deflection angle of the two-phase flow behind the supersonic nozzle oblique section. Basic assumptions for the calculation model are as follows: a flow in the nozzle is one-dimensional and unsteady, the condensed phase velocity vector is not changed within the oblique section part of the nozzle. Calculation results are confirmed by experimental data for model working medium.