Recent Progress on Supercomputer Modelling of High-Speed Rarefied Gas Flows Using Kinetic Equations

A. Frolova, V. Titarev
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引用次数: 7

Abstract

Numerical solution of the Boltzmann equation for stationary high-speed flows around complex three-dimensional bodies is an extremely difficult computational problem. This is because of high dimension of the equation and lack of efficient implicit methods for the calculation of the collision integral on arbitrary non-uniform velocity grids. Therefore, the use of the so-called model (approximate) kinetic equations appears to be more appropriate and attractive. This article uses the numerical methodology recently developed by the second author which includes an implicit method for solving the approximating kinetic equation of E.M. Shakhov (S-model) on arbitrary unstructured grids in both velocity and physical spaces. Since most of model equations have a well-known drawback associated with the velocityindependent collision frequency it is important to determine the deviations of solutions of these equations from the solution of the complete Boltzmann equation or DSMC for high-speed gas flows. Our recent comparison of the DSMC and S-model solutions for monatomic gases with a soft interaction potential shows good agreement of surface coefficients of the pressure, heat transfer and friction, which are most important for industrial applications. In this paper, we compare the solution of model equations and the Boltzmann equation for the problem of supersonic gas flow around a cylinder when molecules interact according to the law of hard spheres. Since this law of molecular interaction is the most rigid, the difference in solutions can show the maximum error that can be obtained by using model equations instead of the exact Boltzmann equation in such problems. Our high-fidelity computations show that the use of model kinetic equations with adaptation in phase space is very promising for industrial applications.
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用动力学方程模拟高速稀薄气体流动的超级计算机研究进展
绕复杂三维物体的静止高速流动的玻尔兹曼方程的数值解是一个极其困难的计算问题。这是由于方程的高维数和缺乏有效的隐式方法来计算任意非匀速网格上的碰撞积分。因此,使用所谓的模型(近似)动力学方程显得更为合适和有吸引力。本文采用第二作者最近开发的数值方法,其中包括一种隐式方法,用于在速度和物理空间中求解任意非结构网格上的Shakhov (s模型)近似动力学方程。由于大多数模型方程都有与速度无关的碰撞频率相关的众所周知的缺点,因此确定这些方程的解与完全玻尔兹曼方程或DSMC的解的偏差对于高速气体流动是很重要的。我们最近对具有软相互作用势的单原子气体的DSMC和s模型解进行了比较,结果表明压力、传热和摩擦的表面系数非常一致,这对于工业应用是最重要的。本文比较了分子按硬球定律相互作用时超声速气体绕圆柱体流动问题的模型方程和玻尔兹曼方程的解。由于这种分子相互作用的规律是最严格的,所以解的差异可以显示在这类问题中使用模型方程而不是精确玻尔兹曼方程所能得到的最大误差。我们的高保真计算表明,在相空间中使用具有自适应的模型动力学方程非常有希望用于工业应用。
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