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用模型喷管模拟研究发动机组外向辐射传热
引用本文:程惠尔,牛禄.用模型喷管模拟研究发动机组外向辐射传热[J].推进技术,2001,22(2):126-128.
作者姓名:程惠尔  牛禄
作者单位:上海交通大学动力与能源工程学院,
摘    要:根据热辐射理论,分析空间发动机外向辐射会传热的基本特点,得出在地面用模型喷管-电热喷管缩比件模拟这一传热现象的必要条件为两者几何相似,壁面热流密度q以及表面黑度ε相等。可行性分析为地面模拟试验提供了科学的依据,其结论可用来指导试验。

关 键 词:并联火箭发动机  发动机喷管  地面模拟试验  辐射传热  可行性研究
文章编号:1001-4055(2001)02-0126-03
修稿时间:2000年6月26日

Simulation research for radiation heat transfer of engine group by model nozzles
Cheng Hui-er and Niu Lv.Simulation research for radiation heat transfer of engine group by model nozzles[J].Journal of Propulsion Technology,2001,22(2):126-128.
Authors:Cheng Hui-er and Niu Lv
Institution:School of Power and Energy Engineering,Shanghai Jiaotong Univ.,Shanghai 200030,China;School of Power and Energy Engineering,Shanghai Jiaotong Univ.,Shanghai 200030,China
Abstract:According to the theory of heat radiation,the essential characteristic of outward radiation heat transfer of engine group was researched,and the necessary conditions for simulation research of this heat transfer phenomenon using nozzles,subscale component of electrically heated nozzles were given out to be simialr geometrically,and equal for heat flux q and emissivity ε on wall surface for the two.Feasibility analysis provides scientific basis for ground simulation test.Its conclusion can be used for guiding the test.
Keywords:Rocket engine cluster  Engine nozzle  Ground simulation test  Radiative heat transfer  Feasibility study
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