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脉冲爆震发动机的可爆范围及内流燃气温度与壁温的实验研究
引用本文:何立明,严传俊,范玮,雷恒仁.脉冲爆震发动机的可爆范围及内流燃气温度与壁温的实验研究[J].推进技术,1999,20(3):21-24.
作者姓名:何立明  严传俊  范玮  雷恒仁
作者单位:1. 空军工程学院航空机械工程系,西安,710038
2. 西北工业大学航空动力与热力工程系,西安,710072
基金项目:国家自然科学基金,“八六三”基金
摘    要:在脉冲爆震发动机原理性试验模型上对脉冲爆震发动机的可爆范围和内流燃气温度、壁温进行实验研究,掌握在脉冲爆震发动机中形成爆震波的条件、机理,以及影响可爆范围和内流燃气温度、壁温的因素及其规律,为脉冲爆震发动机的设计提供技术基础。

关 键 词:脉冲式喷气发动机,爆燃,爆震波+,可爆范围+,燃烧温度,壁温

EXPERIMENTAL INVESTIGATION ON DETONATIVE RANGE,INNER FLOW GAS TEMPERATURE AND WALL TEMPERATURE OF PULSED DETONATION ENGINE
He Liming,Yan Chuanjun,Fan Wei and Lei Hengren.EXPERIMENTAL INVESTIGATION ON DETONATIVE RANGE,INNER FLOW GAS TEMPERATURE AND WALL TEMPERATURE OF PULSED DETONATION ENGINE[J].Journal of Propulsion Technology,1999,20(3):21-24.
Authors:He Liming  Yan Chuanjun  Fan Wei and Lei Hengren
Abstract:Experimental investigation on detonative range,inner flow gas temperature and wall temperature of pulsed detonation engine was made.The experimental investigation was carried out on a test model of pulsed detonation engine that adopted gasoline/air mixture and its purpose was to master the condition,mechanism and regularities of forming detonation wave as well as factors influencing detonative range,inner flow gas temperature and wall temperature in pulsed detonation engine in order to provide technical base for the design of pulsed detonation engine
Keywords:Pulsejet engine  Deflagration  Detonation wave    Detonative range    Combustion temperature  Wall temperature  
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