During the research on Solid Ducted Rocket (SDR), it is an important link for the design and experiment of SDR that a suitable mathematical model is built to simulate its internal working process. The turbulent reacting model presented in this paper was based on a 3 D ducted rocket. Then the numerical simulation of the model was given and some conclusions were obtained. The conclusions are useful for the design and experiment of the ducted rocket.
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余勇,陈小前,王振国.三维实验固体火箭冲压发动机燃烧室湍流反应流数值模拟. Numerical Simulation of 3 D Turbulent ReactingFlow in a Solid Ducted Rocket[J].国防科技大学学报,2002,24(5):1-4.