On the role of turbulence in detonation induced by Mach stem reflection

被引:4
|
作者
Ingram, D [1 ]
Jiang, B [1 ]
Causon, D [1 ]
机构
[1] Manchester Metropolitan Univ, Ctr Math Modelling & Flow Anal, Manchester M1 5GD, Lancs, England
关键词
turbulent ignition processes; shock induced combustion; shock reflection; reduced chemical kinetics;
D O I
10.1007/s001930050125
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
A series of experiments conducted by Chan has shown that while some shock waves may not be strong enough to induce detonation when they collide with an obstacle the resulting Mach stem will induce detonation if it collides with a subsequent obstruction. A series of numerical simulations, however, failed to demonstrate the expected results if either the Euler or laminar Navier-Stokes equations are solved. On the other hand, calculations using the Favre averaged Navier-Stokes equations with a k-epsilon-F turbulence model are able to reproduce the experimental results, indicating that turbulent effects may play an important role in the ignition process. A detailed examination of the results shows that turbulence causes the formation of activated kernels in a similar process to that observed in deflagration-detonation transition. The simulations in this paper have been undertaken using a modem high resolution hydrocode and a reduced kinetics mechanism for hydrogen combustion. The paper describes the reduced mechanism, the solution methods employed in the hydrocode and discusses the results of the simulations and their implications.
引用
收藏
页码:327 / 336
页数:10
相关论文
共 50 条
  • [41] Mach stem formation in reflection and focusing of weak shock acoustic pulses
    Karzova, Maria M.
    Khokhlova, Vera A.
    Salze, Edouard
    Ollivier, Sebastien
    Blanc-Benon, Philippe
    JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA, 2015, 137 (06): : EL436 - EL442
  • [42] Unsteady Oblique Detonation Waves in a Tunnel Induced by Inflow Mach Number Variation
    Niu, Shuzhen
    Yang, Pengfei
    Wang, Kuanliang
    Teng, Honghui
    AEROSPACE, 2023, 10 (04)
  • [43] Numerical Simulation of Wedge Induced Oblique Detonation at Near Critical Mach Number
    Wang C.
    Wu J.-C.
    Han W.-H.
    Yang T.-H.
    Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology, 2020, 40 (08): : 803 - 809
  • [44] Transition of an overdriven Mach stem in the Mach reflection of detonations in H2/O2 mixtures
    Jing T.
    Ren H.
    Li J.
    Zhongguo Kexue Jishu Kexue/Scientia Sinica Technologica, 2021, 51 (04): : 446 - 458
  • [45] THE INVERSE MACH REFLECTION
    TAKAYAMA, K
    BENDOR, G
    AIAA JOURNAL, 1985, 23 (12) : 1853 - 1859
  • [46] MACH REFLECTION ON A CONE
    MERRITT, DL
    AIAA JOURNAL, 1968, 6 (06) : 1208 - &
  • [47] Similarity in Mach stem evolution and termination in unsteady shock-wave reflection
    Koronio, E.
    Ben-Dor, G.
    Sadot, O.
    Geva, M.
    JOURNAL OF FLUID MECHANICS, 2020, 902 (902)
  • [48] TRANSITION FROM MACH TO REGULAR REFLECTION AND DOMAINS OF VARIOUS MACH REFLECTION CONFIGURATIONS
    GVOZDEVA, LG
    FOKEEV, VP
    COMBUSTION EXPLOSION AND SHOCK WAVES, 1977, 13 (01) : 86 - 93
  • [49] Breakup characteristics of droplets induced by detonation waves under different diameters and Mach numbers
    Yang, Rui
    Zhang, Qibin
    Xiao, Qiang
    Chen, Qingyun
    Jiang, Yuguang
    Fan, Wei
    PHYSICS OF FLUIDS, 2025, 37 (01)
  • [50] Detonation-turbulence interaction
    Massa, L.
    Chauhan, M.
    Lu, F. K.
    COMBUSTION AND FLAME, 2011, 158 (09) : 1788 - 1806