Vortex flow visualization using tetrahedral cell subdivision

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

Abstract

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.
使用四面体单元细分的涡流可视化
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。
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