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六管吸气式脉冲爆震发动机试验

袁成 范玮 彭畅新 张群 陈文娟 严传俊

袁成, 范玮, 彭畅新, 张群, 陈文娟, 严传俊. 六管吸气式脉冲爆震发动机试验[J]. 航空动力学报, 2011, 26(9): 1981-1985.
引用本文: 袁成, 范玮, 彭畅新, 张群, 陈文娟, 严传俊. 六管吸气式脉冲爆震发动机试验[J]. 航空动力学报, 2011, 26(9): 1981-1985.
YUAN Cheng, FAN Wei, PENG Chang-xin, ZHANG Qun, CHEN Wen-juan, YAN Chuan-jun. Experimental investigation on a six-tube air-breathing pulse detonation engine[J]. Journal of Aerospace Power, 2011, 26(9): 1981-1985.
Citation: YUAN Cheng, FAN Wei, PENG Chang-xin, ZHANG Qun, CHEN Wen-juan, YAN Chuan-jun. Experimental investigation on a six-tube air-breathing pulse detonation engine[J]. Journal of Aerospace Power, 2011, 26(9): 1981-1985.

六管吸气式脉冲爆震发动机试验

Experimental investigation on a six-tube air-breathing pulse detonation engine

  • 摘要: 设计了单管内径为68mm的六管吸气式脉冲爆震发动机试验系统,以汽油为燃料,空气为氧化剂,成功地进行了多循环爆震试验.结果表明:六管均能形成多次可重复的爆震波;各管之间的相互影响小;共同工作的同步性好;长时间工作起爆稳定.研究结果对多管脉冲爆震发动机的工程应用具有较大的参考价值.

     

  • [1] 严传俊,范玮.脉冲爆震发动机原理及关键技术[M].西安:西北工业大学出版社,2005.
    [2] Rasheed A,Furman A,Dean A J.Wave attenuation and interactions in a pulsed detonation combustor-turbine hybrid system .AIAA 2006-1235,2006.
    [3] Rasheed A,Furman A,Dean A J.Experimental investigations of an axial turbine driven by a multi-tube pulsed detonation combustor system .AIAA 2005-4209,2005.
    [4] Rasheed A,Furman A,Dean A J.Wave interactions in a multi-tube pulsed detonation combustor-turbine hybrid system .AIAA 2006-4447,2006.
    [5] Rasheed A,Furman A,Dean A J.Pressure measurements and attenuation in a hybrid multi-tube pulse detonation turbine system .AIAA 2006-1235,2006.
    [6] 李建中,王家骅,唐豪,等.煤油/空气三管气动阀式脉冲爆震发动机[J].航空学报,2009,30(11):2052-2058. LI Jianzhong,WANG Jiahua,TANG Hao,et al.Kerosene/air triple-tube aero-valve pulse detonation engine[J].Acta Aeronautica et Astronautica Sinica,2009,30(11):2052-2058.(in Chinese)
    [7] 李建中,王家骅,唐豪,等.煤油/空气三管脉冲爆震发动机共用尾喷管研究[J]. 航空动力学报,2008,23(5):840-844. LI Jianzhong,WANG Jiahua,TANG Hao,et al.Investigation on common nozzle of triple-tube pulse detonation engine with kerosene/air[J].Journal of Aerospace Power,2008,23(5):840-844.(in Chinese)
    [8] Ebrahimi H B,Malo-Molina F J,Merkle C L.Numerical investigation of multi-tube pulse detonation .AIAA 2003-718,2003.
    [9] Ebrahimi H B.Multidimensional analysis of multitube pulse detonation .AIAA 2003-6975,2003.
    [10] 刘建文,钟诚文,赵书苗.多管脉冲爆震发动机流场数值研究[J].推进技术,2007,28(6):674-678. LIU Jianwen,ZHONG Chengwen,ZHAO Shumiao.Numerical investigation of multi-tube pulse detonation engine[J].Journal of Propulsion Technology,2007,28(6):674-678.(in Chinese)
    [11] 李建中,王家骅,王春,等.共用尾喷管多管脉冲爆震发动机数值模拟研究[J].空气动力学学报,2008,26(1):96-100. LI Jianzhong,WANG Jiahua,WANG Chun,et al.Numerical investigation of multi-tube pulse detonation engine with common nozzle[J].Acta Aerodynamica Sinica,2008,26(1):96-100.(in Chinese)
    [12] 黄玥,唐豪,李建中,等.多管脉冲爆震发动机共用喷管特性的数值模拟[J].南京航空航天大学学报,2009,41(4):432-438. HUANG Yue,TANG Hao,LI Jianzhong,et al.Numerical investigation on characteristic of multi-tube pulse detonation engines with different common nozzles[J].Journal of Nanjing University of Aeronautics and Astronautics,2009,41(4):432-438.(in Chinese)
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出版历程
  • 收稿日期:  2010-10-23
  • 修回日期:  2010-12-18
  • 刊出日期:  2011-09-28

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