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..
| Abstracts file: | MartyushDetonMIT2013.doc |