The combustion in the swirl chamber is broken into three phases: low temperature ignition kinetics, high temperature premixed kinetics burn and diffusion burn phase.While the burn in the main chamber is considered as diffusion combustion. The shell ignition model, global Arrhenius equation and coherent flamelet model are used to model low temperature ignition, high temperature premixed burn and diffusion burn respectively. Three-dimensional numerical calculation code is developed. The change of temperature fields in the swirl chamber is studied. The pressure and the heat release rate predicted by the model are coincided with the results derived from experiments.
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