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arXiv 2007.07347physics.comp-phphysics.flu-dyn
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一种用于不可压缩流动的简化离散统一气体动理学格式

A simplified discrete unified gas kinetic scheme for incompressible flow

Mingliang Zhong, Sen Zou, Dongxin Pan, Congshan Zhuo, Chengwen Zhong

AI总结:

提出一种简化离散统一气体动理学格式,通过在全时间步重构变换分布函数预测通量,省略半时间步计算,在保持稳定性的同时简化计算,并验证了多种流动案例。

摘要:

离散统一气体动理学格式(DUGKS)是一种用于连续流和稀薄流的新型有限体积(FV)格式,它结合了格子玻尔兹曼方法(LBM)和统一气体动理学格式(UGKS)的优点。通过利用粒子速度特征线重构气体分布函数,通量包含了更详细的流体流动信息和更具体的物理性质。在本工作中,提出了一种简化的DUGKS,其重构阶段在完整时间步上进行,而非原始DUGKS中的半时间步。利用时间/空间积分的玻尔兹曼 Bhatnagar-Gross-Krook(BGK)方程,构造了包含碰撞效应的变换分布函数。通过沿粒子速度特征线在界面上重构变换分布函数,预测了下一时间步单元上的宏观和介观通量。根据守恒定律,单元在下一时间步的宏观变量可通过其宏观通量进行更新。下一时间步的平衡分布函数也可更新。气体分布函数通过有限体积格式,利用其在时间步内预测的介观通量进行更新。与原始DUGKS相比,所提方法的计算过程更为简洁,因为省略了半时间步通量计算。数值时间步仅受Courant-Friedrichs-Lewy(CFL)条件限制,并保持了相对较好的稳定性。进行了多个测试案例,包括库埃特流、顶盖驱动空腔流、平板、圆柱和翼型上的层流,以及微空腔流案例,以验证当前格式。数值模拟结果与参考文献结果吻合良好。

英文摘要:

The discrete unified gas kinetic scheme (DUGKS) is a new finite volume (FV) scheme for continuum and rarefied flows which combines the benefits of both Lattice Boltzmann Method (LBM) and unified gas kinetic scheme (UGKS). By reconstruction of gas distribution function using particle velocity characteristic line, flux contains more detailed information of fluid flow and more concrete physical nature. In this work, a simplified DUGKS is proposed with reconstruction stage on a whole time step instead of half time step in original DUGKS. Using temporal/spatial integral Boltzmann Bhatnagar-Gross-Krook (BGK) equation, the transformed distribution function with inclusion of collision effect is constructed. The macro and mesoscopic fluxes of the cell on next time step is predicted by reconstruction of transformed distribution function at interfaces along particle velocity characteristic lines. According to the conservation law, the macroscopic variables of the cell on next time step can be updated through its macroscopic flux. Equilibrium distribution function on next time step can also be updated. Gas distribution function is updated by FV scheme through its predicted mesoscopic flux in a time step. Compared with the original DUGKS, the computational process of the proposed method is more concise because of the omission of half time step flux calculation. Numerical time step is only limited by the Courant-Friedrichs-Lewy (CFL) condition and relatively good stability has been preserved. Several test cases, including the Couette flow, lid-driven cavity flow, laminar flows over a flat plate, a circular cylinder, and an airfoil, as well as micro cavity flow cases are conducted to validate present scheme. The numerical simulation results agree well with the references' results.

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