Critical deflagration waves leading to detonation onset under different boundary conditions

被引:4
作者
Lin Wei [1 ]
Zhou Jin [1 ]
Fan Xiao-Hua [2 ]
Lin Zhi-Yong [1 ]
机构
[1] Natl Univ Def Technol, Sci & Technol Scramjet Lab, Changsha 410073, Hunan, Peoples R China
[2] China Aerodynam Res & Dev Ctr, Mianyang 621000, Peoples R China
基金
中国国家自然科学基金;
关键词
critical deflagration waves; wall boundary condition; zonary flame; pressure waves; FLAME ACCELERATION; TRANSITION; DDT; MECHANISM;
D O I
10.1088/1674-1056/24/1/014701
中图分类号
O4 [物理学];
学科分类号
0702 ;
摘要
High-speed turbulent critical deflagration waves before detonation onset in H-2-air mixture propagated into a square cross section channel, which was assembled of optional rigid rough, rigid smooth, or flexible walls. The corresponding propagation characteristic and the influence of the wall boundaries on the propagation were investigated via high-speed shadowgraph and a high-frequency pressure sampling system. As a comprehensive supplement to the different walls effect investigation, the effect of porous absorbing walls on the detonation propagation was also investigated via smoke foils and the high-frequency pressure sampling system. Results are as follows. In the critical deflagration stage, the leading shock and the closely following turbulent flame front travel at a speed of nearly half the CJ detonation velocity. In the preheated zone, a zonary flame arises from the overlapping part of the boundary layer and the pressure waves, and then merges into the mainstream flame. Among these wall boundary conditions, the rigid rough wall plays a most positive role in the formation of the zonary flame and thus accelerates the transition of the deflagration to detonation (DDT), which is due to the boost of the boundary layer growth and the pressure wave reflection. Even though the flexible wall is not conducive to the pressure wave reflection, it brings out a faster boundary layer growth, which plays a more significant role in the zonary flame formation. Additionally, the porous absorbing wall absorbs the transverse wave and yields detonation decay and velocity deficit. After the absorbing wall, below some low initial pressure conditions, no re-initiation occurs and the deflagration propagates in critical deflagration for a relatively long distance.
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页数:8
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共 22 条
  • [1] An experimental investigation of the onset of detonation
    Chao, J
    Otsuka, T
    Lee, JHS
    [J]. PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2005, 30 : 1889 - 1897
  • [2] Flame acceleration and transition to detonation in ducts
    Ciccarelli, G.
    Dorofeev, S.
    [J]. PROGRESS IN ENERGY AND COMBUSTION SCIENCE, 2008, 34 (04) : 499 - 550
  • [3] Flame acceleration and DDT in channels with obstacles: Effect of obstacle spacing
    Gamezo, Vadim N.
    Ogawa, Takanobu
    Oran, Elaine S.
    [J]. COMBUSTION AND FLAME, 2008, 155 (1-2) : 302 - 315
  • [4] Experimental observation of the onset of detonation downstream of a perforated plate
    Grondin, J. -S.
    Lee, John H. S.
    [J]. SHOCK WAVES, 2010, 20 (05) : 381 - 386
  • [5] Deflagration-to-Detonation Transition Induced by Hot Jets in a Supersonic Premixed Airstream
    Han Xu
    Zhou Jin
    Lin Zhi-Yong
    Liu Yu
    [J]. CHINESE PHYSICS LETTERS, 2013, 30 (05)
  • [6] HIGH-SPEED TURBULENT DEFLAGRATIONS AND TRANSITION TO DETONATION IN H2-AIR MIXTURES
    LEE, JHS
    KNYSTAUTAS, R
    FREIMAN, A
    [J]. COMBUSTION AND FLAME, 1984, 56 (02) : 227 - 239
  • [7] Lee JHS, 2008, DETONATION PHENOMENON, P250, DOI 10.1017/CBO9780511754708.009
  • [8] Relativistic R-matrix studies of photoionization processes of Ar5+
    Li Chuan-Ying
    Han Xiao-Ying
    Wang Jian-Guo
    Qu Yi-Zhi
    [J]. CHINESE PHYSICS B, 2013, 22 (12)
  • [9] Experimental investigation on performance of pulse detonation rocket engine model
    Li Qiang
    Fan Wei
    Yan Chuan-jun
    Hu Cheng-qi
    Ye Bin
    [J]. CHINESE JOURNAL OF AERONAUTICS, 2007, 20 (01) : 9 - 14
  • [10] Deflagration-to-detonation transition in highly reactive combustible mixtures
    Liberman, M. A.
    Ivanov, M. F.
    Kiverin, A. D.
    Kuznetsov, M. S.
    Chukalovsky, A. A.
    Rakhimova, T. V.
    [J]. ACTA ASTRONAUTICA, 2010, 67 (7-8) : 688 - 701