Numerical Analysis of Critical Reynolds Number of Wavy Taylor Vortex Flow with Changing Aspect Ratio

H. Furukawa, Takashi Watanabe, Y. Toya
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引用次数: 0

Abstract

Taylor vortex flow is one of the important vortex flows that have been studied since its classic study made by G. I. Taylor in 1923. State of the flow between inner and outer cylinders of a rotating co-axial cylinder transits from Couette flow to Taylor vortex flow and to wavy Taylor vortex flow as the increase of Reynolds number. This study has identified the critical Reynolds number when the flow changes from Taylor vortex flow to wavy Taylor vortex flow. The numerical analysis making use of the attractor in the chaos theory has been used in this identification of the critical Reynolds number. The calculated critical Reynolds numbers of each flow mode are almost identical to the values obtained by the visualization experiment at small aspect ratios. In the region where the aspect ratio is larger than the ratio at the peak critical Reynolds number, the distribution of the Reynolds number is qualitatively similar between the calculated and experimental values.
变化展弦比的波状泰勒涡临界雷诺数数值分析
泰勒涡旋是自1923年G. I. Taylor进行经典研究以来所研究的重要涡旋之一。随着雷诺数的增加,同轴旋转圆柱内外柱间的流动状态由库埃特流过渡到泰勒涡流,再过渡到波浪泰勒涡流。本文确定了泰勒涡向波浪泰勒涡转变时的临界雷诺数。利用混沌理论中的吸引子对临界雷诺数进行了数值分析。计算得到的各流型临界雷诺数与小展弦比下的可视化实验结果基本一致。在展弦比大于峰值临界雷诺数比值的区域,雷诺数的计算值与实验值的分布在性质上相似。
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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