使用四面体单元细分的涡流可视化

A. Doi, Satoshi Suzuki, K. Koyamada, Shinji Sannakanishi
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引用次数: 6

摘要

提出了一种有效的搜索临界点的技术,即速度矢量为零的点。以往采用四面体单元细分的方法,往往会在一个六面体单元中产生多个临界点,这给流动显示带来了一些缺陷。首先,我们提出了一种新的插值函数差异判据,并探讨了六面体单元中产生多个临界点的原因。其次,为了防止产生多个临界点,我们提出了一种改进的方法,使用四面体单元细分和三线性插值函数。我们的方法通过使用线性插值函数找到临界点,当在六面体单元中找到多个临界点时,应用数值积分方案(牛顿法)并计算更精确的位置。我们将我们的方法应用于几组速度数据,并以几种方式对其进行评估。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Vortex flow visualization using tetrahedral cell subdivision
Proposes an effective technique for searching for critical points, which are points at which the velocity vector is zero. The previous method, using tetrahedral-cell subdivision, often generates multiple critical points in a hexahedral cell, and this causes several defects in flow visualization. First, we propose a new criterion for differences between interpolation functions, and investigate the reasons for the generation of multiple critical points in a hexahedral cell. Next, to prevent the generation of multiple critical points, we propose an improved method using both tetrahedral-cell subdivision and a trilinear interpolation function. Our method finds critical points by using a linear interpolation function, and, when multiple critical points are found in a hexahedral cell, a numerical integration scheme (Newton's method) is applied and a more precise position is calculated. We apply our approach to several sets of velocity data and evaluate it in several ways.
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