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喷管收敛-扩张角对爆震发动机性能影响分析
引用本文:曾昊,何立明,章雄伟,罗俊. 喷管收敛-扩张角对爆震发动机性能影响分析[J]. 推进技术, 2011, 32(1): 97-102
作者姓名:曾昊  何立明  章雄伟  罗俊
作者单位:空军工程大学,工程学院,陕西,西安,710038
摘    要:为了研究喷管收敛-扩张角对爆震发动机性能的影响,以氢气和氧气混合物为例,对不同喷管收敛-扩张角下的爆震发动机工作过程进行了数值模拟,结果表明,不同喷管收敛-扩张角对爆震发动机性能的影响并不相同。增大扩张角,喷管出口面积增大,推力投影面积增大,排气时间减少,喷管内压力下降较快。收敛角为5°或扩张角为5°时的爆震发动机性能较好。

关 键 词:脉冲爆震发动机  爆震波  喷管
收稿时间:2009-12-03
修稿时间:2010-05-07

Investigation on the effects of nozzles with different convergent-divergent angle on PDE performance
ZENG Hao,HE Li-ming,ZHANG Xiong-wei and LUO Jun. Investigation on the effects of nozzles with different convergent-divergent angle on PDE performance[J]. Journal of Propulsion Technology, 2011, 32(1): 97-102
Authors:ZENG Hao  HE Li-ming  ZHANG Xiong-wei  LUO Jun
Affiliation:(Engineering Inst.,Air Force Engineering Univ.,Xian 710038,China)
Abstract:In order to investigate the effects of nozzles with different convergent-divergent angle on PDE performance,PDE with different nozzle convergent-divergent angle were simulated and hydrogen-oxygen mixture was used.The results indicate that different nozzle convergent-divergent angle has different effects on PDE performance.As divergent angle increases,area of nozzle outlet and thrust projection area increases,but exhaust time and pressure in nozzle decreases.When convergent angle is of 5°or divergent angle is of 5°,the performance of PDE is good.
Keywords:Pulse detonation engine  Detonation  Nozzle  
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