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An implicit gas-kinetic scheme for turbulent flow on unstructured hybrid mesh

机译:非结构混合网格上湍流的隐式气体动力学方案

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In this study, an implicit scheme for the gas-kinetic scheme (GKS) on the unstructured hybrid mesh is proposed. The Spalart-Allmaras (SA) one equation turbulence model is incorporated into the implicit gas-kinetic scheme (IGKS) to predict the effects of turbulence. The implicit macroscopic governing equations are constructed and solved by the matrix-free lower-upper symmetric-Gauss-Seidel (LU-SGS) method. To reduce the number of cells and computational cost, the hybrid mesh is applied. A modified non-manifold hybrid mesh data(NHMD) is used for both unstructured hybrid mesh and uniform grid. Numerical investigations are performed on different 2D laminar and turbulent flows. The convergence property and the computational efficiency of the present IGKS method are investigated. Much better performance is obtained compared with the standard explicit gas-kinetic scheme. Also, our numerical results are found to be in good agreement with experiment data and other numerical solutions, demonstrating the good applicability and high efficiency of the present IGKS for the simulations of laminar and turbulent flows. (C) 2018 Elsevier Ltd. All rights reserved.
机译:在这项研究中,提出了一种非结构混合网格上的气体动力学方案(GKS)的隐式方案。将Spalart-Allmaras(SA)一方程式湍流模型合并到隐式气体动力学方案(IGKS)中,以预测湍流的影响。通过无矩阵的上下对称高斯-赛德尔(LU-SGS)方法构造和求解隐式宏观控制方程。为了减少像元数量和计算成本,应用了混合网格。改进的非流形混合网格数据(NHMD)用于非结构化混合网格和均匀网格。对不同的二维层流和湍流进行了数值研究。研究了当前IGKS方法的收敛性和计算效率。与标准的显式气体动力学方案相比,可以获得更好的性能。而且,我们的数值结果与实验数据和其他数值解非常吻合,证明了本IGKS在层流和湍流模拟中的良好适用性和高效率。 (C)2018 Elsevier Ltd.保留所有权利。

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