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三组元喷嘴混合特性的试验研究
引用本文:沈赤兵,姜春林,童荣瑜,周进,王振国.三组元喷嘴混合特性的试验研究[J].国防科技大学学报,1999,21(4):12-16.
作者姓名:沈赤兵  姜春林  童荣瑜  周进  王振国
作者单位:国防科技大学航天技术系!长沙410073
摘    要:本文对四种类型的气氢/液氧/煤油三组元喷嘴进行了混合特性试验, 研究了内喷嘴的缩进长度对同轴离心外混式喷嘴混合特性的影响, 对比了相同的三组元工况下各喷嘴的混合特性, 分析了喷嘴结构对混合特性的影响, 进行了单喷嘴和三喷嘴的混合特性试验, 试验结果表明: 在相同的三组元工况下, 同轴直流式喷嘴的流强分布跨度比同轴离心式喷嘴小。所得结论对三组元喷嘴和气液同轴式喷嘴的优化设计有参考价值。

关 键 词:三组元喷嘴  混合特性  冷流试验  液体火箭发动机  流强分布
收稿时间:1998/10/15 0:00:00

Experimental Investigation on Mixing Characteristics of Tripropellant Injectors
Shen Chibing,Jiang Chunlin,Tong Rongyu,Zhou Jin and Wang Zhenguo.Experimental Investigation on Mixing Characteristics of Tripropellant Injectors[J].Journal of National University of Defense Technology,1999,21(4):12-16.
Authors:Shen Chibing  Jiang Chunlin  Tong Rongyu  Zhou Jin and Wang Zhenguo
Institution:Department of Aerospace Technology, NUDT, Changsha, 410073;Department of Aerospace Technology, NUDT, Changsha, 410073;Department of Aerospace Technology, NUDT, Changsha, 410073;Department of Aerospace Technology, NUDT, Changsha, 410073;Department of Aerospace Technology, NUDT, Changsha, 410073
Abstract:Four types of GH 2/LO 2/RP-1 tripropellant injectors are employed to present the mixing characteristics test in this paper. The effects of the internal injector's recess on the mixing characteristics of the swirl coaxial injector with separate fuel injection are studied. The mixing characteristics of each injector are compared with those of the others in the same tripropellant operating condition. The effects of the injectors' configuration on the mixing characteristics are analyzed. The mixing characteristics tests of the single injector and three injectors are presented. The tests results show that the span of the mass flux distribution of the shear coaxial injector is smaller than that of the swirl coaxial injector in the same tripropellant operating condition. The conclusions reached in this paper provide a reference for the optimization design of the tripropellant injectors and the gas/liquid coaxial injectors.
Keywords:tripropellant injector  mixing characteristics  cold flow test  liquid rocket engine  mass flux distribution    
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