Volume 27 Issue 12
Dec.  2012
Turn off MathJax
Article Contents
HAN Xu, ZHOU Jin, LIN Zhi-yong, LIU Shi-jie. Initiation mechanism investigation of saltation and smoothness oblique detonation waves[J]. Journal of Aerospace Power, 2012, 27(12): 2674-2680.
Citation: HAN Xu, ZHOU Jin, LIN Zhi-yong, LIU Shi-jie. Initiation mechanism investigation of saltation and smoothness oblique detonation waves[J]. Journal of Aerospace Power, 2012, 27(12): 2674-2680.

Initiation mechanism investigation of saltation and smoothness oblique detonation waves

  • Received Date: 2011-09-07
  • Publish Date: 2012-12-28
  • Euler equations with chemical reaction were used to study the difference in the initiation mechanism and characteristics of saltation and smoothness oblique detonation waves (ODW).The result shows that the criterion which determines the oblique detonation wave configuration is whether a subsonic zone exists behind the oblique shock wave(OSW).If the OSW raised by the flame behind it can lead to the formation of a subsonic zone, the transverse shock wave and triple point would appear and saltation ODW would form.The smoothness ODW would form if all zones are supersonic behind the OSW so the flame can not touch the upriver OSW.The OSW critical angle which leads to the formation of transverse shock wave is calculated from the equations of OSW.When the OSW angle is bigger than this critical angle, saltation ODW would form.otherwise, smoothness ODW would form.

     

  • loading
  • [1]
    Dudebout R,Sislian J P,Oppitz R.Numerical simulation of hypersonic shock-induced combustion ramjets[J].Journal of Propulsion and Power,1998,14(6):869-879.
    [2]
    Kailasanath K.Review of propulsion applications of detonation waves[J].AIAA Journal,2000,38(9):1698-1708.
    [3]
    Fusina G.Numerical investigation of oblique detonation waves for shcramjet combustor[D].Toronto:University of Toronto,2003.
    [4]
    Shinichi M,Inada R,Kasahara J,et al.Visualization of the non-steady state oblique detonation wave phenomena around hypersonic spherical projectile[J].Proceedings of the Combustion Institute,2011,33(2):2343-2349.
    [5]
    Kasahara J,Aral T,Matsuo A,et al.Experimental investigations of steady-state oblique detonation waves generated around hypersonic projectiles[R].AIAA-2001-1800,2001.
    [6]
    Morris C I,Kamel M R,Hansom R K.Shock-induced combustion in high-speed wedge flows[C]//27th Symp.(International) on Combustion.Boulder:The Combustion Institute,1998:2157-2164.
    [7]
    Morris C I,Kamel M R,Ben-Yakar A,et al.Combined schlieren and OH PLIF imaging study of ram accelerator flowfields[R].AIAA-98-0244,1998.
    [8]
    Broda J C.An experimental study of oblique detonation waves[D].Storrs:The University of Connecticut,1993.
    [9]
    林志勇.高静温超声速预混气爆震起爆与发展过程机理研究[D].长沙:国防科学技术大学,2008.LIN Zhiyong.Research on detonation and development mechanisms in elevated temperature supersonic premixed mixture[D].Changsha:National University of Defense Technology,2008.(in Chinese)
    [10]
    王爱峰,赵伟,姜宗林.驻定斜爆震波中横向激波存在与否的判定标准[C]//第十四届全国激波与激波管学术会议论文集.安徽 黄山:中国力学学会激波与激波管专业委员会,2010:230-235.
    [11]
    Choi J Y,Kim D W,In-Seuck J,et al.Cell-like structure of unstable oblique detonation wave from high-resolution numerical simulation[J].Proceedings of the Combustion Institute,2007,31(2):2473-2480.
    [12]
    Choi J Y.Computational fluid dynamics algorithms for unsteady shock-induced combustion:PartⅠ validation[J].AIAA Journal,2000,38(7):1179-1187.
    [13]
    Choi J Y,Shin E J R,Cho D R,et al.Onset condition of oblique detonation wave cell structures[R].AIAA-2008-1032,2008.
    [14]
    Choi J Y,Jeung I S,Roh T S.Periodical oscillation of combustion induced by oblique shock wave [R].AIAA-2002-3717,2002.
    [15]
    刘君,张涵信,高树椿.一种新型的计算化学非平衡流动的解耦方法[J].国防科技大学学报,2000,22(5):19-23.LIU Jun,ZHANG Hanxin,GAO Shuchun.A new uncoupled method for numerical simulation of nonequilibrium flow[J].Journal of National University of Defense Technology,2000,22(5):19-23.(in Chinese)
    [16]
    刘世杰,孙明波,林志勇,等.钝头体激波诱导振荡燃烧现象的数值模拟[J].力学学报,2010,42(4):1-10.LIU Shijie,SUN Mingbo,LIN Zhiyong,et al.Numerical research on blunt body shock-induced oscillating combustion phenomena[J].Chinese Journal of Theoretical and Applied Mechanics,2010,42(4):1-10.(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 (1960) PDF downloads(1500) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return