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Large-scale Parallel Unstructured Mesh Computations for 3D High-lift Analysis

机译:大型并行非结构化网格计算,用于3D高扬程分析

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摘要

A complete "geometry to drag-polar" analysis capability for the three-dimensional high-lift configurations is described. The approach is based on the use of unstructured meshes in order to enable rapid turnaround for complicated geometries that arise in high-lift configurations. Special attention is devoted to creating a capability for enabling analyses on highly resolved grids. Unstructured meshes of several million vertices are initially generated on a work-station, and subsequently refined on a supercomputer. The flow is solved on these refined meshes on large parallel computers using an unstructured agglomeration multigrid algorithm. Good prediction of lift and drag throughout the range of incidences is demonstrated on a transport take-off configuration using up to 24.7 million grid points. The feasibility of using this approach in a production environment on existing parallel machines is demonstrated, as well as the scalability of the solver on machines using up to 1450 processors.
机译:描述了针对三维高升力配置的完整的“几何到阻力极”分析功能。该方法基于非结构化网格的使用,以便能够快速翻转高升程配置中出现的复杂几何形状。尤其要注意创建一种功能,以便对高度解析的网格进行分析。首先在工作站上生成几百万个顶点的非结构化网格,然后在超级计算机上进行精炼。使用非结构化集聚多网格算法在大型并行计算机上的这些精炼网格上求解流。在使用多达2470万个网格点的运输起飞配置中,可以很好地预测整个事件范围内的升力和阻力。演示了在现有并行计算机上的生产环境中使用此方法的可行性,以及使用多达1450个处理器的计算机上求解器的可伸缩性。

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