航空航天应用中平行二维非结构各向异性Delaunay网格生成

Juliette Pardue, Andrey N. Chernikov
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引用次数: 2

摘要

本文从原理出发,构建网格生成器,提出了一种自下而上的并行各向异性网格生成方法。侧重于高升力设计或动态失速的应用,或数值方法和建模测试用例仍然侧重于二维。本文提出的按钮式并行网格生成方法可以生成具有各向异性边界层的高保真非结构化网格,可用于计算流体力学领域。各向异性要求通过使计算依赖于元素的局部对齐,从而增加了并行网格算法的复杂性,这反过来又由几何边界和密度函数决定。实验结果表明,在256个分布式存储节点上,最快的顺序各向同性网格生成器的并行效率为70%。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Parallel Two-Dimensional Unstructured Anisotropic Delaunay Mesh Generation of Complex Domains for Aerospace Applications
In this paper, we present a bottom-up approach to parallel anisotropic mesh generation by building a mesh generator from principles. Applications focusing on high-lift design or dynamic stall, or numerical methods and modeling test cases still focus on the two-dimensions. Our push-button parallel mesh generation approach can generate high-fidelity unstructured meshes with anisotropic boundary layers for use in the computational fluid dynamics field. The anisotropy requirement adds a level of complexity to a parallel meshing algorithm by making computation depend on the local alignment of elements, which in turn is dictated by geometric boundaries and the density functions. Our experimental results show 70% parallel efficiency over the fastest sequential isotropic mesh generator on 256 distributed memory nodes.
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