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首页> 外文期刊>Computers & mathematics with applications >A simplified finite volume lattice Boltzmann method for simulations of fluid flows from laminar to turbulent regime, Part Ⅱ: Extension towards turbulent flow simulation
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A simplified finite volume lattice Boltzmann method for simulations of fluid flows from laminar to turbulent regime, Part Ⅱ: Extension towards turbulent flow simulation

机译:一种简化的有限体积格子玻尔兹曼方法,用于模拟从层流到湍流的流动,第二部分:向湍流模拟的扩展

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In this paper, the original finite volume lattice Boltzmann method (FVLBM) on an unstructured grid (Part I of these twin papers) is extended to simulate turbulent flows. To model the turbulent effect, the k - omega SST turbulence model is incorporated into the present FVLBM framework and is also solved by the finite volume method. Based on the eddy viscosity hypothesis, the eddy viscosity is computed from the solution of the k - omega SST model, and the total viscosity is modified by adding this eddy viscosity to the laminar (kinematic) viscosity given in the Bhatnagar-Gross-Krook collision term. Because of solving for the collision term with the explicit method in the original FVLBM scheme, the computational efficiency is much lower for simulating high Reynolds number flow. This is due to the fact that the largest time step decided by the stability condition of the collision term, which is less than twice the relaxation time, is much smaller than that decided by the CFL condition. In order to enhance the computational efficiency, the three-stage second-order implicit-explicit (IMEX) Runge-Kutta method is used for temporal discretization, and the time step can be one or two orders of magnitude larger as compared with the explicit Euler forward scheme. Although the computational cost is increased, the final computational efficiency is enhanced by about one-order of magnitude and good results can also be obtained at a large time step through the test case of a lid-driven cavity flow. Two turbulent flow cases are carried out to validate the present method, including flow over a backward-facing step and flow around a NACA0012 airfoil. The numerical results are found to be in agreement with experimental data and numerical solutions, demonstrating the applicability of the present FVLBM coupled with the k - omega SST model to accurately predict the incompressible turbulent flows. (C) 2019 Elsevier Ltd. All rights reserved.
机译:在本文中,对非结构化网格上的原始有限体积晶格玻尔兹曼方法(FVLBM)进行了扩展(这些论文的第一部分),以模拟湍流。为了模拟湍流效应,将k-ωSST湍流模型合并到当前的FVLBM框架中,并且也通过有限体积法进行求解。根据涡流粘度假设,从k-omega SST模型的解中计算出涡流粘度,并通过将该涡流粘度添加到Bhatnagar-Gross-Krook碰撞中给出的层流(运动)粘度中来修改总粘度。术语。由于在原始FVLBM方案中使用显式方法解决了碰撞项,因此模拟高雷诺数流的计算效率要低得多。这是由于以下事实:由碰撞项的稳定性条件决定的最大时间步长(小于松弛时间的两倍)比由CFL条件决定的最大时间步长要小得多。为了提高计算效率,将三阶段二阶隐式显式(IMEX)Runge-Kutta方法用于时间离散化,并且时间步长可以比显式Euler大一到两个数量级。前向计划。尽管增加了计算成本,但最终计算效率却提高了大约一个数量级,并且通过盖驱动腔流的测试案例,还可以在较大的时间步长上获得良好的结果。进行了两个湍流情况以验证本方法,包括在向后步骤上的流动和围绕NACA0012机翼的流动。数值结果与实验数据和数值解相吻合,证明了目前的FVLBM与k-omega SST模型相结合可准确预测不可压缩的湍流。 (C)2019 Elsevier Ltd.保留所有权利。

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