火箭推进2011，Vol.37Issue(4)：35-39,5.
过氧化氢／煤油发动机推力室气液燃烧数值模拟
Numerical simulation of combustion characteristics for thrust chamber in hydrogen peroxide/kerosene engine
摘要
Abstract
The gas-liquid combustion and flow field in HTP/kerosene engine thrust chamber were numerically simulated in the paper. Discrete phase modeling （DPM） and SST k-to turbulence model were used to simulate the kerosene gas-liquid flow and turbulence respectively. A one-step general reaction model of fuel was employed to simulate the kerosene vapour combustion. The combustion flow field and performance parameters of the combustion chamber were numerically investigated. A foundation for the further numerical research was established in this paper.关键词
过氧化氢发动机/推力室/燃烧/数值模拟Key words
hydrogen peroxide engine/thrust chamber/combustion/numerical simulation引用本文复制引用
李强,聂嵩,刘业奎,潘亮,马梦颖..过氧化氢／煤油发动机推力室气液燃烧数值模拟[J].火箭推进,2011,37(4):35-39,5.基金项目
中国航天科技集团公司支撑项目 （）
