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Effect of Reynolds numbers on flow past four square cylinders in an in-line square configuration for different gap spacings

机译:雷诺数对不同间隙间距的直角正方形配置中流过四个正方形圆柱体的流量的影响

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摘要

In this paper two-dimensional (2-D) numerical investigation of flow past four square cylinders in an in-line square configuration are performed using the lattice Boltzmann method. The gap spacing g=s/d is set at 1, 3 and 6 and Reynolds number ranging from Re=60 to 175. We observed four distinct wake patterns: udud(i) a steady wake pattern (Re=60 and g=1)udud(ii) a stable shielding wake pattern (80≤Re≤175 and g=1)udud(iii) a wiggling shielding wake pattern (60≤Re≤175 and g=3)udud(iv) a vortex shedding wake pattern (60≤Re≤175 and g=6) ududAt g=1, the Reynolds number is observed to have a strong effect on the wake patterns. It is also found that at g=1, the secondary cylinder interaction frequency significantly contributes for drag and lift coefficients signal. It is found that the primary vortex shedding frequency dominates the flow and the role of secondary cylinder interaction frequency almost vanish at g=6. It is observed that the jet between the gaps strongly influenced the wake interaction for different gap spacing and Reynolds number combination. To fully understand the wake transformations the details vorticity contour visualization, power spectra of lift coefficient signal and time signal analysis of drag and lift coefficients also presented in this paper.
机译:在本文中,使用格子Boltzmann方法对通过四个方形圆柱体以直角正方形配置的流动进行二维(2-D)数值研究。间隙间隔g = s / d设置为1、3和6,雷诺数范围从Re = 60到175。我们观察到四个不同的唤醒模式: ud ud(i)稳定唤醒模式(Re = 60和g = 1) ud ud(ii)稳定的屏蔽唤醒模式(80≤Re≤175且g = 1) ud ud(iii)不稳定的屏蔽唤醒模式(60≤Re≤175且g = 3) ud ud(iv)涡旋脱落的尾波模式(60≤Re≤175且g = 6) ud ud在g = 1时,观察到雷诺数对尾波模式有很强的影响。还发现在g = 1时,次级气缸相互作用频率显着有助于阻力和升力系数信号。发现在g = 6时,一次涡旋脱落频率主导了流动,而次要圆柱体相互作用频率的作用几乎消失了。观察到,对于不同的间隙间距和雷诺数组合,间隙之间的射流强烈影响尾流相互作用。为了充分了解尾波变换,还介绍了详细的涡度轮廓可视化,升力系数信号的功率谱以及阻力和升力系数的时间信号分析。

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