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水燃比对水冲压发动机性能影响数值模拟与试验研究
引用本文:韩超,夏智勋,胡建新,赵宁,方丁酉.水燃比对水冲压发动机性能影响数值模拟与试验研究[J].国防科技大学学报,2009,31(4):117-121.
作者姓名:韩超  夏智勋  胡建新  赵宁  方丁酉
作者单位:国防科技大学,航天与材料工程学院,湖南,长沙,410073
基金项目:国家自然科学基金资助项目 
摘    要:为了研究水燃比对二次进水水冲压发动机比冲性能的影响规律,建立了发动机补燃室两相反应模型,对镁基水冲压发动机进行了数值模拟,获得了发动机比冲、喷管出口温度及出口速度随水燃比变化趋势,在此基础上进行了水冲压发动机地面直连式试验研究.结果表明,存在最佳水燃比使二次进水水冲压发动机比冲性能较优.

关 键 词:水冲压发动机  比冲性能  水燃比  数值模拟  直连式试验
收稿时间:2009/5/10 0:00:00

Numerical and Experiment Studies on Water Ramjet with Effect of Water-fuel Ratio
HAN Chao,XIA Zhixun,HU Jianxin,ZHAO Ning and FANG Dingyou.Numerical and Experiment Studies on Water Ramjet with Effect of Water-fuel Ratio[J].Journal of National University of Defense Technology,2009,31(4):117-121.
Authors:HAN Chao  XIA Zhixun  HU Jianxin  ZHAO Ning and FANG Dingyou
Institution:College of Aerospace and Materials Engineering, National Univ. of Defense Technology, Changsha 410073, China;College of Aerospace and Materials Engineering, National Univ. of Defense Technology, Changsha 410073, China;College of Aerospace and Materials Engineering, National Univ. of Defense Technology, Changsha 410073, China;College of Aerospace and Materials Engineering, National Univ. of Defense Technology, Changsha 410073, China;College of Aerospace and Materials Engineering, National Univ. of Defense Technology, Changsha 410073, China
Abstract:A two-phase reaction model of the secondary combustor was established to study the effect of water-fuel ratio on engine performance of magnesium-based water ramjet with twice water penetration. The change tendency of specific impulse, temperature and velocity of nozzle exit were obtained with water-fuel ratio. Direct-connected tests were carried out in order to validate the correctness of the numerical simulation. The result shows that there exists the optimum water-fuel ratio, which can improve the performance of water ramjet.
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