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Reordering of hybrid unstructured grids for an implicit Navier-Stokes solver based on OpenMP parallelization

机译:基于OpenMP并行化的隐式Navier-Stokes求解器的混合非结构化网格的重新排序

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摘要

Grid reordering is an efficient way to obtain better implicit convergence speed in viscous flow simulation based on unstructured grids. When performing parallel computation on the shared memory machines, the convergence performance for solving high-Reynolds number flow with LU-SGS implicit scheme is ruined by the interface between different sub-domains divided by OpenMP parallelization, In order to improve the compatibility between OpenMP parallel environment and the implicit LU-SGS time-stepping scheme, a grid reordering method for unstructured hybrid grids is proposed. In this method, the structured-grid cells in the viscous layer near-body surface are reordered along the normal direction (like columns) and the unstructured part is reordered layer by layer according to the neighboring relations. To investigate the performance of the current implementation, turbulent flows around the RAE2822 airfoil, the NHLP-2D L1T2 multi-element airfoil configuration, the DLR-F6 wing-body-nacelle-pylon configuration and an aerospace plane has been simulated on unstructured hybrid grids. The numerical results show that the grid reordering method is an efficient and practical strategy for improving the convergence rate and the overall efficiency in the parallel computation with unstructured flow solver. (C) 2014 Elsevier Ltd. All rights reserved,
机译:网格重排序是在基于非结构化网格的粘性流模拟中获得更好的隐式收敛速度的有效方法。在共享存储计算机上执行并行计算时,通过不同子域之间的接口(通过OpenMP并行化划分)破坏了使用LU-SGS隐式方案解决高雷诺数流的收敛性能,从而提高了OpenMP并行之间的兼容性提出了一种非结构化混合网格的网格重排序方法。在这种方法中,粘性层近体表面中的结构化网格单元沿着法线方向(像圆柱一样)重新排序,非结构化部分根据相邻关系逐层重新排序。为了研究当前实施方案的性能,围绕RAE2822机翼,NHLP-2D L1T2多元素机翼构型,DLR-F6机体-机舱-塔架构型以及在非结构混合网格上的航空飞机进行了湍流流动。数值结果表明,网格重排序方法是一种在非结构化流求解器并行计算中提高收敛速度和整体效率的有效且实用的策略。 (C)2014 Elsevier Ltd.保留所有权利,

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