具有曲面壁边界条件的D3Q19晶格玻尔兹曼方法在实际流动问题模拟中的实现

E. Ezzatneshan
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引用次数: 1

摘要

本文给出了求解复杂几何不可压缩流体流动的三维晶格玻尔兹曼方法(LBM)无滑移壁边界条件的一种扩展形式的实现。边界条件基于非点阵格式,采用多项式插值法重构相邻点阵节点上的曲面或不规则壁面边界。这种处理提高了求解算法处理复杂几何图形的计算效率,并且与反弹法的阶梯近似相比,具有更高的精度。通过计算具有弯曲壁或不规则壁的几何形状的流体流动,验证了所提出的数值方法的有效性和准确性。为了验证本文的计算,本文考虑了三个测试用例,即NACA0012机翼截面周围的流动计算和在不同流动条件下通过两种不同多孔介质的流动计算。研究表明,基于三维点阵玻尔兹曼方法的计算方法,采用弯曲壁面边界条件,对于求解具有实际几何形状的层流具有鲁棒性和有效性,并且具有足够的精度,可以用于工程设计的流动特性预测。
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Implementation of D3Q19 Lattice Boltzmann Method with a Curved Wall Boundary Condition for Simulation of Practical Flow Problems
In this paper, implementation of an extended form of a no-slip wall boundary condition is presented for the three-dimensional (3-D) lattice Boltzmann method (LBM) for solving the incompressible fluid flows with complex geometries. The boundary condition is based on the off-lattice scheme with a polynomial interpolation which is used to reconstruct the curved or irregular wall boundary on the neighboring lattice nodes. This treatment improves the computational efficiency of the solution algorithm to handle complex geometries and provides much better accuracy comparing with the staircase approximation of bounce-back method. The efficiency and accuracy of the numerical approach presented are examined by computing the fluid flows around the geometries with curved or irregular walls. Three test cases considered herein for validating the present computations are the flow calculation around the NACA0012 wing section and through the two different porous media in various flow conditions. The study shows the present computational technique based on the implementation of the three-dimensional Lattice Boltzmann method with the employed curved wall boundary condition is robust and efficient for solving laminar flows with practical geometries and also accurate enough to predict the flow properties used for engineering designs.
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发文量
29
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