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Numerical simulation of flow over a circular cylinder with a splitter plate near a moving wall

机译:流动壁附近带有隔板的圆柱体上流动的数值模拟

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The flow past a circular cylinder with a splitter plate (CCSP) above a moving wall is simulated numerically in this paper. A large-eddy based lattice Boltzmann model is used to calculate the turbulent flow. The flows are simulated in the range of gap ratios (GID) from 0.1 to 3.0 and Reynolds number from 200 to 400, respectively, where G is the gap between cylinder and wall, D is the diameter of cylinder. The mechanism of the vortex shedding suppression near a moving wall is analyzed. Vorticity contours are demonstrated to reveal the wake flow patterns and the suppression of vortex generation. The vortex shedding from lower side of the CCSP system completely disappears when the gap ratio is less than 0.2. As gap ratio decreases from 3.0 to 0.1, the vortex shedding frequency increases and reaches the summit firstly, and then decreases for the gap ratio decreasing continuously. Compared with the near wall case which is without splitter-plate, the drag and lift coefficients of CCSP system are reduced significantly. The results. are in good agreement with the previous experiment and numerical simulations. (C) 2016 Elsevier Ltd. All rights reserved.
机译:本文通过流动壁上方流经带有隔板(CCSP)的圆柱体的流动进行了数值模拟。基于大涡流的格子Boltzmann模型用于计算湍流。分别在间隙比(GID)从0.1到3.0范围和雷诺数从200到400的范围内模拟流动,其中G是圆柱体和壁之间的间隙,D是圆柱体的直径。分析了动壁附近涡流抑制的机理。涡度等高线显示出尾流模式并抑制了涡流的产生。当间隙比小于0.2时,从CCSP系统的下侧脱落的涡流完全消失。当间隙比从3.0减小到0.1时,涡旋脱落频率先上升并到达顶点,然后随着间隙比连续减小而减小。与不带隔板的近壁箱相比,CCSP系统的阻力和升力系数大大降低。结果。与先前的实验和数值模拟非常吻合。 (C)2016 Elsevier Ltd.保留所有权利。

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