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液体火箭发动机水击特性仿真及试验研究
引用本文:窦唯,胡长喜.液体火箭发动机水击特性仿真及试验研究[J].火箭推进,2013,39(2):40-45.
作者姓名:窦唯  胡长喜
作者单位:北京航天动力研究所,北京,100076
摘    要:建立了液体火箭发动机水击压力的模型,进行了数值仿真和试验对比分析,研究了影响液体火箭发动机水击压力的影响因素,讨论了发动机关机后推进剂管路的压力瞬变特性,从而验证了数值模拟的正确性。

关 键 词:液体火箭发动机  水击特性  仿真  试验

Simulation and testing research for water hammer characteristic of liquid rocket engine
DOU Wei , HU Chang-xi.Simulation and testing research for water hammer characteristic of liquid rocket engine[J].Journal of Rocket Propulsion,2013,39(2):40-45.
Authors:DOU Wei  HU Chang-xi
Institution:(Beij ing Aerospace Propulsion Institute, Beij ing 100076, China)
Abstract:Water hammer pressure model of liquid rocket engine was built. The numerical simulation and testing contrastive analysis were made. The factors that influence water hammer pressure of the liquid rocket engine were investigated. The pressure transient characteristic of the propellant pipes after shutdown of engine was discussed. The correctness of the numerical simulation was approved by the comparison of calculated data with experiment data. The research achievement can be used in the design and testing of liquid rocket engine.
Keywords:liquid rocket engine  water hammer characteristic  simulation  experiment
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