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正激波结构与反射的蒙特卡罗模拟 被引量:4

MONTE CARLO SIMULATION OF THE STRUCTURE AND REFLECTION OF NORMAL SHOCK WAVES
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摘要 本文用变径刚球模型(VHS)与Larsen-Borgnakke模型借助直接模拟蒙特卡罗方法模拟正激波结构与反射问题。直接模拟显示了分子间作用力幂次对激波剖面的影响,平动自由度经激波的非平衡效应,双组分气体经激波的组分分离效应,有转动自由度激发(双原子分子)气体中激波结构、传播和反射、双原子轻分子作为载体的混合气体激波结构中重气体的温度超出等。 The structure and reflexion of normal shock wave in simple monoatomic gas, diatomic gas and in gas mixtures are simulated by the direct simulation Monte Carlo method (DSMC). To simulate the intermolecular forces the variable hard sphere model (VHS) is used, and the interchange of translational energy and the internal energy is simulated by the phenomenological model of Larsen and Borgnakke. The thickness of the shock wave transition zone obtained by the VHS model for different values of the power in the intermolecular force is shown to be identical with the result obtained by the inverse power law model, provided the expressions for the mean free path correspond ing to the viscosity expressions derived for relevent models are used accordingly. Also shown is the effect of non-equilibrium in the translational degrees of freedom across shock wave in a simple monoatomic gas, i. e. the difference between the longitudinal (parallel) temperature based on the velocity component in the direction of wave progression and the transverse (perpendicular) temperature based on the velocity component in the direction perpendicular to the wave motion. For gas mixtures of two components calculations reveal the component separation effect and the effect of overshoot of the heavy component parallel temperature. In the paper the structure and the process of propagation and reflexion of normal shock wave in a diatomic gas (i, e. with coupling between the translational and rotational energies of a molecule) is also simulated, with the rotational relaxation number ZR chosen to be 5. The density profiles across the shock obtained are in good agreement with the experimental data, and the change of the parameters experienced in the reflection of the shock from a solid wall are found to be in excellent accordance with the result from the gas dynamic relations. Initiative investigations have been carried on the parellel temperature overshoot in a mixture of heavy (trace)-light (carrier, diatomic) gases. Simulation with more exact method and the analysis of the overshoot data and mechanism are underway and will be published elsewhere.
出处 《空气动力学学报》 CSCD 北大核心 1991年第4期435-441,共7页 Acta Aerodynamica Sinica
基金 国家自然科学基金
关键词 激波结构 激波反射 蒙特卡罗法 shock wave structure, shock wave reflection, direct simulation Monte Carlo method.
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参考文献1

  • 1沈青,1990年

同被引文献22

  • 1李馨东,赵英奎,胡宗民,姜宗林.基于第二粘性的Navier-Stokes方程组求解正激波结构[J].计算物理,2020,37(5):505-513. 被引量:3
  • 2姜毅,傅德彬.固体火箭发动机尾喷焰复燃流场计算[J].宇航学报,2008,29(2):615-620. 被引量:28
  • 3张福祥.火箭燃气射流动力学[M].北京:国防工业出版社,1988..
  • 4韩式方.气体分子动力论模方程及对激波结构的研究(关于波尔兹曼方程的数学模型)[J]数学物理学报,1981(01).
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  • 7Fiscko Kurt Alan.Study of continuum higher order closure models evaluated by a statistical theory of shock structure. . 1988
  • 8Bird G A.Shock wave structure in gas mixtures. Rarefied Gas Dynamics . 1984
  • 9Fiscko,K.A,& Chapman,D.R.Comparison of Burnett,super-Burnett and Monte Carlo solutions for hypersonic shock structure. Proceedings of the 16th International Symposium on Rarefied Gas Dynamics . 1988
  • 10李志辉,张涵信.激波结构内流动问题的气体运动论描述[J].空气动力学学报,2007,25(4):411-418. 被引量:4

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