高温空气正激波流动的态-态模型与多温度模型对比分析
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国防科技大学空天科学学院

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V211.3

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国家自然科学基金项目(11927803)


Comparative analysis of state-to-state and multi-temperature thermochemical models in simulation for high-temperature air flow behind normal shock waves
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    摘要:

    分别采用态-态模型和多温度模型进行11化学组元的高温空气正激波流动数值模拟与分析。态-态模型区分中性分子的振动能级和中性原子的电子能级;多温度模型区分平动-转动温度、各中性分子的振动温度和电子温度。波前气流速度5~11km/s范围的模拟结果表明:在紧靠激波区域,由于离解和电离反应,高振动能级和原子高电子能级的分布低于对应温度下的玻尔兹曼分布;与态-态模型相比,多温度模型下激波后振动能、电子能的激发和各内能模式的平衡都更晚,化学反应更晚发生,但更早结束;多温度模型预测的起因于化学反应的振动能损失偏小、起因于电子碰撞电离的电子能损失偏大,获得的表征各模式内能的温度不能准确描述粒子能级的非平衡分布。

    Abstract:

    State-to-state (StS) model and multi-temperature (MT) model are used to numerically simulate the high-temperature air flow behind normal shock waves. In the StS model, each vibrational state of neutral molecules and electronic excited states of neutral atoms were regarded as pseudo species. MT model described the different modes of internal energy with translational–rotational temperature, the vibrational temperatures of every neutral molecules and electron–electronic excitation temperature specifically. The simulations with freestream speeds range from 5 to 11 km/s are carried out. The results indicate that there are obvious under-population of the high-lying vibrational and electronic states in the near shock region, which are caused by the rapid dissociation and ionization processes respectively. As compared with StS model, in MT model the vibrational and electronic excitation, chemical reactions take place later, the flow attains thermal equilibrium later while attains chemical equilibrium earlier. The vibrational energy loss caused by chemical reactions is less and the electronic energy loss through the impact ionization reactions is more predicted by the MT model, and the specific temperatures cannot correctly describe the non-equilibrium vibrational and electronic population distribution.

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  • 收稿日期:2024-01-22
  • 最后修改日期:2025-07-12
  • 录用日期:2024-06-25
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