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Multi-temperature Model Derived from State-to-State Kinetics for Hypersonic Entry in Jupiter Atmosphere

机译:来自Jupiter大气中的超音速进入的状态对状态动力学的多温模型

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A state-to-state model of H_2/He plasmas coupling the master equations for internal distributions of heavy species with the transport equation for the free electrons has been used as a basis for implementing a multi-temperature kinetic model. In the multi-temperature model internal distributions of heavy particles are Boltzmann, the electron energy distribution function is Maxwell, and the rate coefficients of the elementary processes become a function of local temperatures associated to the relevant equilibrium distributions. The state-to-state and multi-temperature models have been compared in the case of a homogenous recombining plasma, reproducing the conditions met during supersonic expansion though converging-diverging nozzles.
机译:H_2 / H HE等离子体的状态到状态模型与自由电子的传输方程一起耦合用于重型物种的内部分布的母版方程被用作实现多温动力学模型的基础。在重质颗粒的多温模型内部分布中是Boltzmann,电子能量分布函数是MaxWell,并且基本过程的速率系数成为与相关平衡分布相关的局部温度的函数。已经在均匀的重组等离子体的情况下比较了状态和多温模型,再现在超音速扩张期间满足的条件虽然会聚 - 发散喷嘴。

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