Мартюшов С.Н.  

Numerical simulation of flows in rotation detonation engine

The simplified mathematical model of two-phase chemical reaction, including the induction period and the subsequent reaction period was used. The gas was assumed to be non viscous, and the one-stage Arrhenius model for chemical reaction rate was employed. Spatial discretization of the fluxes vector normal  to the cell boundary direction is performed on the basis of  TVD-schemes. The goal of this study is to investigate numerically the flow in a rotational detonation engine..