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Master Equation Study of Hydrogen Relaxation Using Complete Sets of State-to-state Transition Rates

机译:使用整套状态间转换速率进行氢弛豫的主方程研究

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The complete sets of state-to-state transition rate coefficients for both target and projectile molecules are derived from the predicted response surface designed by the ordinary Kriging model. A system of master equations is constructed for bound-bound and bound-free transitions with these designed transition rate coefficients, and the rovibrational number densities are numerically evaluated by implicitly integrating a system of master equations. In these master equation studies, relaxation of rotation and vibration modes, number density relaxation, reaction rate coefficients, and average rotational and vibrational energy losses due to dissociation are each considered in strong nonequilibrium conditions. A system of master equations are coupled with one-dimensional flow equations to analyze the relaxations of H_2 in post-normal shock and nozzle expanding flows. In post-normal shock flows, the relaxation of the rotational mode is slightly faster or almost similar to the relaxation of the vibrational mode. In nozzle expanding flows, the relaxations of both rotational and vibrational modes seem to be frozen.
机译:目标分子和射弹分子的状态到状态跃迁速率系数的完整集合是从由普通Kriging模型设计的预测响应曲面中得出的。利用这些设计的跃迁速率系数构建用于有界和无界跃迁的主方程组,并通过隐式集成主方程组对旋转振子数密度进行数值评估。在这些主方程研究中,旋转和振动模式的弛豫,数密度弛豫,反应速率系数以及由于解离而产生的平均旋转和振动能量损失均在强非平衡条件下被考虑。将主方程组与一维流动方程相耦合,以分析法线后冲击和喷嘴扩展流动中H_2的弛豫。在法线后冲击流中,旋转模式的松弛略快或几乎类似于振动模式的松弛。在喷嘴膨胀流中,旋转模式和振动模式的松弛似乎都被冻结了。

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