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Comparing macroscopic continuum models for rarefied gas dynamics : a new test method

机译:比较稀有气体动力学的宏观连续模型:一种新的测试方法

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摘要

We propose a new test method for investigating which macroscopic continuum models, among the many existing models, give the best description of rarefied gas flows over a range of Knudsen numbers. The merits of our method are: no boundary conditions for the continuum models are needed, no coupled governing equations are solved, while the Knudsen layer is still considered. This distinguishes our proposed test method from other existing techniques (such as stability analysis in time and space, computations of sound speed and dispersion, and the shock wave structure problem). Our method relies on accurate, essentially noise-free, solutions of the basic microscopic kinetic equation, e.g. the Boltzmann equation or a kinetic model equation; in this paper, the BGK model and the ES-BGK model equations are considered. Our method is applied to test whether one-dimensional stationary Couette flow is accurately described by the following macroscopic transport models: the Navier-Stokes-Fourier equations, Burnett equations, Grad's 13 moment equations, and the regularized 13 moment equations (two types: the original, and that based on an order of magnitude approach). The gas molecular model is Maxwellian. For Knudsen numbers in the transition-continuum regime (Kn less-than-or-equals, slant 0.1), we find that the two types of regularized 13 moment equations give similar results to each other, which are better than Grad's original 13 moment equations, which, in turn, give better results than the Burnett equations. The Navier-Stokes-Fourier equations give the worst results. This is as expected, considering the presumed accuracy of these models. For cases of higher Knudsen numbers, i.e. Kn > 0.1, all macroscopic continuum equations tested fail to describe the flows accurately. We also show that the above conclusions from our tests are general, and independent of the kinetic model used.
机译:我们提出了一种新的测试方法,以研究在许多现有模型中哪些宏观连续模型能够最好地描述一系列努森数范围内稀薄气体的流动。我们方法的优点是:不需要连续模型的边界条件,不需要求解耦合的控制方程,而仍要考虑Knudsen层。这将我们提出的测试方法与其他现有技术(例如,时间和空间的稳定性分析,声速和弥散的计算以及冲击波结构问题)区分开来。我们的方法依赖于基本微观动力学方程的精确,基本无噪声的解决方案,例如玻尔兹曼方程或动力学模型方程;本文考虑了BGK模型和ES-BGK模型方程。我们的方法适用于测试以下宏观运输模型是否能准确描述一维平稳Couette流:Navier-Stokes-Fourier方程,Burnett方程,Grad的13矩方程和正则化的13矩方程(两种类型:原始数据,以及基于数量级方法的数据)。气体分子模型是麦克斯韦。对于过渡连续体制中的Knudsen数(Kn小于或等于,斜率为0.1),我们发现两种类型的正则化13矩方程互为相似的结果,这比Grad最初的13矩方程要好。 ,这反过来会比Burnett方程提供更好的结果。 Navier-Stokes-Fourier方程给出的结果最差。考虑到这些模型的假定准确性,这是预期的。对于更高的克努森数(即Kn> 0.1),所有测试的宏观连续方程都无法准确描述流量。我们还表明,我们的测试得出的上述结论是笼统的,并且与所使用的动力学模型无关。

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