Volume 21 Issue 1
Feb.  2006
Turn off MathJax
Article Contents
LI Jian-zhong, WANG Jiahua, FAN Yu-xin, ZHANG Yi-ning, ZHANG Jing-zhou. Investigation on Pneumatic-Valve Pulse Detonation Engine with Partial Detonable Mixture Filling[J]. Journal of Aerospace Power, 2006, 21(1): 45-49.
Citation: LI Jian-zhong, WANG Jiahua, FAN Yu-xin, ZHANG Yi-ning, ZHANG Jing-zhou. Investigation on Pneumatic-Valve Pulse Detonation Engine with Partial Detonable Mixture Filling[J]. Journal of Aerospace Power, 2006, 21(1): 45-49.

Investigation on Pneumatic-Valve Pulse Detonation Engine with Partial Detonable Mixture Filling

  • Received Date: 2004-11-02
  • Rev Recd Date: 2005-03-21
  • Publish Date: 2006-02-28
  • Effects of partial detonable mixture filling proportion on detonation wave pressure properties of kerosene/air pneumatic-valve pulse detonation engine were investigated.A preliminary analysis of a series of wave's reciprocity was carried out.Experimental results show that with given double swirl and direct pneumaticvalve and detonation tube structure,the decrease of partial detonable mixture filling proportion causes a little decrease of the peak value of detonation waves' pressure,but impulse per unit volume of detonable mixture increases linearly.This investigation is important to the design optimization of the kerosene/air pneumatic-valve PDE,and to improve the performance of PDE.

     

  • loading
  • [1]
    Chiping Li,Kailasanath K.Performance Analysis of Pulse Detonation Engines with Partial Fuel Filling[R].AIAA 2002-0610,January 14-17,2002.
    [2]
    Cooper M,Shepherd J E.The Effect of Nozzles and Extensions on Detonation Tube Performance[R].AIAA 02-3628,July 7-10,2002.
    [3]
    李建中,王家骅,范育新,等.多循环脉冲爆震发动机净推力估算[J].推进技术,2004,25(3);241~245.LI Jianzhong,WANG Jiahua,FAN Yuxin,et al.Net Thrust Prediction of Multi-Cycle Pulse Detonation Engine[J].Journal of Propulsion Technology,2004,25 (3); 241 ~ 245.
    [4]
    何小民,王家骅.气动阀式两相脉冲爆震发动机研究[J].航空学报,2004,25(6);529~533.He XiaoMin,Wang JiaHua.Investigation on the Aerovalve Two Phase Pulse Detonation Engine[J].ACTA Aeronautical ET Astronautica Sinica,2004,25 (6); 529~ 533.
    [5]
    韩启祥.爆震机理及旋转阀脉冲爆震发动机原理样机研究[D].南京;南京航空航天大学,2004.
    [6]
    童秉纲,孔祥言,邓国华.气体动力学[M].北京;高等教育出版社,1989.241~285.
    [7]
    陈义良,张孝春,孙慈,等.燃烧原理[M].北京;航空工业出版社,1992.185~231.
    [8]
    Dean A J.Recent Developments in Approaches to Pulsed Detonation Propulsion[R].AIAA 2003-4510,July 2003.
    [9]
    Kailasanath K.Multiphase Detonation in Pulse Detonation Engines-A Status Report[R].AIAA 2003-4683,July 2003.
  • 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 (1635) PDF downloads(442) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return