卫星推进系统发动机启动过程数值仿真
Numerical Simulation on the Starting Process of Satellite Propulsion System
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摘要: 以一维管道瞬变流理论和特征线方法为基础,建立了仿真系统部件流体动力学模型。计算方法采用带内插的特征线方法和四阶龙格库塔法。对燃烧室模型,考虑燃烧时滞的影响,计算了卫星推进系统发动机在启动过程中各参数的变化。仿真结果与卫星推进系统热试车试验结果基本吻合。结果表明计算模型较好地描述了发动机启动过程中的水击和管流振荡现象,采用的仿真方法符合精度要求,在工程上可为卫星推进系统的设计与试验提供指导。Abstract: The analytical model was developed using the water hammer and one-dimensional fluid transient theory.The combustion time delay was considered.All system parameter changes during the propulsion system engine starting process were considered.The characteristic method and the classical Runge-Kutta method were adopted for simulation.The simulation results are consistent with experiments.The results show that these models give reasonable descriptions for water hammer and flow oscillation during engine starting process.The simulation methods meet the accuracy requirements and could provide guidance for designs and experiments of propulsion system.
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