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Detonation Initiation in H{sub}2-Air and CH{sub}4-Air Mixtures by Incident Shock Wave - One-Dimensional Numerical Simulation

机译:冲击波在H {sub} 2-空气和CH {sub} 4-空气混合物中起爆的一维数值模拟

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Detonation processes in gas mixtures for a long time have been an object of interest of many scientists studying combustion processes. This paper is the contribution to expanding growth of numerical investigations in detonation processes and increasing knowledge of physical aspects of this phenomenon. This paper presents detailed analysis of one-dimensional model of shock initiation of detonation wave. Two combustible mixtures hydrogen-air and methane-air were taken under consideration. Hydrogen-air mixture was analyzed with different concentration of hydrogen, from rich to very lean and with two Mach numbers of strong incident shock wave. The analysis of the transition to detonation process was performed for a bursting diaphragm experiment. In the presented simulation, an increase of Mach number of incident shock wave was made by releasing chemical energy in the driver section at the moment of bursting of the diaphragm. The hot gas in the driver section and fuel mixture in the shock tube is separated by inert gas section. The physical model deals with Euler conservation equations, using an ideal gas law. The set of conservation equations was integrated numerically with the FCT method. The heat release mechanism bases on integration of detailed chemical kinetics equation with the use of CHEMKIN package. Results of the investigation include distribution of thermodynamic and flow parameters in respective time sequence from hot spots formation to detonation relaxation, including collision of retonation wave and contact surface. The main events occurring in the shock tube simulation are also presented on position-time diagrams.
机译:长期以来,气体混合物中的爆轰过程一直是许多研究燃烧过程的科学家关注的对象。本文为扩大爆炸过程中数值研究的发展以及增加对该现象的物理方面的了解做出了贡献。本文对一维爆轰波起爆模型进行了详细分析。考虑了氢-空气和甲烷-空气的两种可燃混合物。分析了氢-空气混合物中氢气的浓度(从浓到稀)以及两个马赫数的强入射冲击波。对于爆破膜片实验进行了向爆轰过渡的分析。在提出的模拟中,通过在隔膜破裂时释放驱动器部分中的化学能来增加入射冲击波的马赫数。驱动器部分中的热气和减震管中的混合燃料被惰性气体部分隔开。物理模型使用理想气体定律处理欧拉守恒方程。该守恒方程组与FCT方法进行了数值积分。放热机制基于使用CHEMKIN软件包对详细的化学动力学方程式进行整合。研究结果包括从热点形成到爆轰弛豫(包括雷轰波与接触面的碰撞)在各个时间序列中的热力学和流量参数分布。在冲击管仿真中发生的主要事件也显示在位置时间图上。

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