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首页> 外文期刊>Acta astronautica >Numerical simulation of a CO_2, CO, O_2, O, C mixture: Validation through comparisons with results obtained in a ground-based facility and thermochemical effects
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Numerical simulation of a CO_2, CO, O_2, O, C mixture: Validation through comparisons with results obtained in a ground-based facility and thermochemical effects

机译:CO_2,CO,O_2,O,C混合物的数值模拟:通过与地面设施获得的结果和热化学作用的比较进行验证

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摘要

Various issues of numerical simulation of high-enthalpy non-equilibrium flows of a gas mixture of CO2, CO, O-2, O, and C are discussed. Navier-Stokes equations are considered within the framework of one-, two-, and three-temperature approximations with allowance for chemical reactions. In the one-temperature approximation, chemical reactions are modelled by the Arrhenius law. In the multi-temperature approximations, simulations are performed with the use of the Treanor-Marrone model for carbon dioxide dissociation and the Park model for dissociation of diatomic gas molecules, which take into account vibrational non-equilibrium of molecules. The Arrhenius law is also used for calculating recombination reactions and also forward and backward exchange reactions. Translational-vibrational and vibrational-vibrational energy exchange is simulated by a simplified Landau-Teller model. Some examples of flows with the use of the above-mentioned approximations are calculated. It is demonstrated that the one-temperature approach ensures an adequate reproduction of experimental data on the shock standoff distance, heat flux, and pressure coefficient on the cone, which are obtained in a high-enthalpy wind tunnel. The calculation of the flow around a cylinder under Martian re-entry conditions reveals a significant effect of thermochemical non-equilibrium.
机译:讨论了CO2,CO,O-2,O和C气体混合物的高焓非平衡流数值模拟的各个问题。 Navier-Stokes方程是在一,二和三温度近似的框架内考虑的,并考虑到了化学反应。在单温度近似中,化学反应通过阿伦尼乌斯定律建模。在多温度近似中,考虑到分子的振动非平衡,使用Treanor-Marrone模型进行二氧化碳离解和Park模型进行双原子气体分子离解的模拟。阿累尼乌斯定律还用于计算重组反应以及正向和反向交换反应。平移振动和振动振动的能量交换是通过简化的Landau-Teller模型进行模拟的。计算了使用上述近似值的一些流量示例。结果表明,单温度方法可确保充分再现有关在高焓风洞中获得的冲击距离,热通量和锥上压力系数的实验数据。火星再入条件下圆柱体周围流动的计算揭示了热化学非平衡的显着影响。

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