Working process with reburning of generating gas at supercritical parameters in the chamber of combustion of rocket engine on liquid fuel numerical modeling

Аuthors

Bachev N. L., Matunin O. O., Kozlov A. A.^*, Bacheva N. J.

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: kozlov202@yandex.ru

Abstract

The non-stationary two-dimensional equations reacting at supercritical parameters of «gaz+liquid drop» stream are considered. Results of thermal gas-dynamic calculation of parameters of working process in the chamber of combustion of rocket engine on liquid fuel with reburning of oxidizing generating gas are resulted.

Keywords:

gas; a drop; interphase interaction; concentration of steam; profiles of speed, temperatures, pressure.