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Effect of tube spacing on the vortex shedding characteristics of laminar flow past an inline tube array: A numerical study

机译:管间距对通过直列管阵列的层流涡流脱落特性的影响:数值研究

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摘要

The effect of tube spacing on the vortex shedding characteristics and fluctuating forces in an inline cylinder array is studied numerically. The examined Reynolds number is 100 and the flow is laminar. The numerical methodology and the code employed to solve the Navier-Stokes and continuity equations in an unstructured finite volume grid are validated for the case of flow past two tandem cylinders at four spacings. Computations are then performed for a six-row inline tube bank for eight pitch-to-diameter ratios, s, ranging from 2.1 to 4. At the smallest spacing examined (s = 2.1) there are five stagnant and symmetric recirculation zones and weak vortex shedding activity occurs only behind the last cylinder. As s increases, the symmetry of the recirculation zones breaks leading to vortex shedding and this process progressively moves upstream, so that for s = 4 there is clear shedding from every row. For any given spacing, the shedding frequency behind each cylinder is the same. A critical spacing range between 3.0 and 3.6 is identified at which the mean drag as well as the rms lift and drag coefficients for the last three cylinders attain maximum values. Further increase to s = 4 leads to significant decrease in the force statistics and increase in the Strouhal number. It was found that at the critical spacing there is 180° phase difference in the shedding cycle between successive cylinders and the vortices travel a distance twice the tube spacing within one period of shedding.
机译:数值研究了管间距对直列圆柱阵列中涡流脱落特性和脉动力的影响。检查的雷诺数为100,流为层流。数值方法和用于求解非结构有限体积网格中的Navier-Stokes和连续性方程的代码已针对流过两个串联圆柱体且间隔为四个的情况进行了验证。然后针对六列直列管束进行计算,其八节距与直径之比s为2.1到4。在所检查的最小间距(s = 2.1)下,有五个停滞且对称的回流区和弱涡旋脱落活动仅在最后一个圆柱后面发生。随着s的增加,再循环区域的对称性破裂,导致涡旋脱落,并且该过程逐渐向上游移动,因此对于s = 4,每行都有明显的脱落。对于任何给定的间距,每个圆柱体后面的脱落频率是相同的。确定了一个介于3.0和3.6之间的临界间距范围,在该范围内,最后三个气缸的平均阻力以及均方根升力和阻力系数达到最大值。进一步增加到s = 4会导致力统计显着下降和Strouhal数增加。已经发现,在临界间距处,连续圆柱体之间的脱落循环中存在180°的相位差,并且涡旋在一个脱落周期内的行进距离是管间距的两倍。

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