Методика моделирования нестационарных процессов зажигания ракетного двигателя на газообразном топливе кислород и водород

Abstract

Has been described method to simulate the transient ignition processes in the rocket engine operating on gaseous hydrogen and oxygen. Have been considered features of the method and its relevance to tasks with transient ignition simulation. Has been given the description of used software tools. Has been described the chemical reaction system. Has been given the way of estimating the chemical reaction system from the physical process point of view.