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激波与爆轰波对撞的数值模拟研究 被引量:4

NUMERICAL INVESTIGATION ON THE COLLISION BETWEEN DETONATIONS AND SHOCKS
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摘要 采用二阶精度NND差分格式和改进的二阶段化学反应模型模拟了爆轰波与激波的对撞过程,研究了不同强度入射激波对爆轰过渡区域的影响.当对撞激波较弱时,透射爆轰波演变主要受流动膨胀作用的影响,可划分为对撞影响区、爆轰恢复区和稳定发展区3个阶段,在爆轰恢复区和稳定发展区,前导激波压力经历一个过冲、然后向稳定爆轰过渡的过程,表现了爆轰波熄爆和再起爆的物理特征,当对撞激波较强时,可燃混合气体的高热力学参数导致了更高的化学反应活化程度,形成了弱爆轰向稳定爆轰的直接转变. Collisions between detonations and shock waves of different strength have been numerically simulated by using NND scheme implemented with the improved two-step chemical reaction model. The collision effects on the detonation transition zone were investigated. In the case of detonation interacting with weaker shock waves, the detonation transition is dominated by flow expansion which lowers the post-shock thermo-states and reduces the chemical reaction rate. The detonation transition can be divided into three stages, named as the collision effect zone, the detonation growth zone and the steady detonation development zone respectively, which indicates some characteristics of detonation-decoupling and reigniting. When detonation interacts with a stronger shock waves, the thermal properties of the explosive mixture are so high that the induced chemical reactions become more active and the flow expansion is compensated. The transition appears to be a direct transformation from a weak detonation to a quasi-steady CJ detonation.
出处 《力学学报》 EI CSCD 北大核心 2008年第2期154-161,共8页 Chinese Journal of Theoretical and Applied Mechanics
基金 国家自然科学基金(10632090,90205027)
关键词 激波对撞 过渡区域 爆轰波 激波 数值模拟 shock wave collision, transition zone, detonation waves, shock waves, numerical simulation
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参考文献6

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同被引文献21

  • 1朱雨建,杨基明.爆轰波与激波对撞的实验研究[J].力学学报,2008,40(6):721-728. 被引量:2
  • 2袁镒吾.直线爆炸所形成的柱面波的近似分析解[J].应用数学和力学,1993,14(5):415-418. 被引量:1
  • 3Ng HD, Botros BB, Chao J, et al. Head-on collision of a detonation with a planar shock wave. Shock Waves, 2006, 2:745-750.
  • 4Botros BB, Zhu Y J, Ng HD, et al. The unsteady dynamics of the head-on collision between a detonation and a shock wave, In: Proc. 20th ICDERS, 2005.
  • 5Sichel M, Tonello NA, Oran ES, et al. A two-step kinetics model for numerical simulation of explosions and detonations in H2-O2 mixtures. Proc R Soc Lond A, 2002, 458: 49-82.
  • 6Mcbride B J, Zehe M J, Cordon S. NASA Glenn coefficients for calculating thermodynamic properties of individoual species, NASA/TP-2002-211556, 2002.
  • 7Zhang HX. Non-oscillatory and non-free-parameter dissipation difference scheme. Acta Aerodynamica Sinica, 1988, 6:143-165.
  • 8Sharpe G J, Quirk JJ. Nonlinear cellular dynamics of the idealized detonation model: regular cells. Combustion Theory and Modelling, 2007, 12(1): 1-21.
  • 9H. D. Ng,B. B. Botros,J. Chao,J. M. Yang,N. Nikiforakis,J. H. S. Lee. Head-on Collision of a Detonation with a Planar Shock Wave[J] 2006,Shock Waves(5):341~352
  • 10J. H. S. Lee,M. I. Radulescu. On the Hydrodynamic Thickness of Cellular Detonations[J] 2005,Combustion, Explosion, and Shock Waves(6):745~765

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