Volume 26 Issue 9
Sep.  2011
Turn off MathJax
Article Contents
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.

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

  • Received Date: 2010-10-23
  • Rev Recd Date: 2010-12-18
  • Publish Date: 2011-09-28
  • A experimental system for six-tube air-breathing pulse detonation engine (PDE) with the single tube's inner diameter of 68mm was designed.Using gasoline as fuel and air as oxidizer,multi-cycle experimental study was successfully performed.The results show that all of the six tubes can obtain continuous detonation waves.The interaction among the tubes is not obvious and the engine can work synchronously and stably.The research results are very helpful to engineering applications of multi-tube PDE.

     

  • loading
  • [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)
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views (2112) PDF downloads(15) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return