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ON PLASMA DYNAMIC ASPECTS OF DETONATION AND BURNING PROCESSES SIMULATION

机译:爆炸的等离子体动力学方面及燃烧过程模拟

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The simulation of detonation and burning waves propagation based on hydrodynamic heat transfer plasma approach are presented. The considered simulation gets good enough correlation with experimental data for detonation wave velocities and shows that these velocities coincide with the maximum of ion-sonic soliton velocities which determine by a ionic compound chemical components of initial detonation medium. Proposed mathematical model describes the main physical stages of detonation wave propagation: the outstripping radiation heat of detonation medium with ionization process and ion-sonic soliton formation, which determines the detonation wave velocity. Paper presents the exact solution of two-fluid hydrodynamic plasma equations. This exact solutions give the maximum velocities of ion sonic nonlinear solitons. Special consideration has fulfilled for plasma dynamic description of traditional hydrocarbon fuel. Typical structures of initial and ending burning components are demonstrated.
机译:提出了基于流体动力传热等离子体方法的爆轰波和燃烧波传播的仿真。所考虑的模拟与爆轰波速度的实验数据具有足够好的相关性,并且表明这些速度与由初始爆炸介质的离子化合物化学成分确定的离子声孤子速度的最大值一致。提出的数学模型描述了爆炸波传播的主要物理阶段:爆炸介质的电离辐射热与电离过程和离子声孤子形成有关,这决定了爆炸波的速度。论文提出了双流体流体动力学方程的精确解。这种精确的解决方案提供了离子声波非线性孤子的最大速度。对于传统碳氢燃料的等离子体动力学描述,已经完成了特殊考虑。演示了初始和结束燃烧组件的典型结构。

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