Numerical investigation of vortex suppression regions for three staggered circular cylinders

被引:15
作者
Yang, Shuchao [1 ,2 ]
Yan, Weiwei [1 ]
Wu, Jie [2 ]
Tu, Chengxu [1 ]
Luo, Dan [1 ]
机构
[1] China Jiliang Univ, Coll Metrol & Measurement Engn, Hangzhou 310018, Zhejiang, Peoples R China
[2] Nanjing Univ Aeronaut & Astronaut, Dept Aerodynam, Nanjing 210016, Jiangsu, Peoples R China
基金
中国国家自然科学基金;
关键词
Lattice Boltzmann method; Immersed boundary method; Vortex shedding; Suppression regions; LATTICE BOLTZMANN METHOD; SIDE-BY-SIDE; FLOW INTERFERENCE; SIMULATION;
D O I
10.1016/j.euromechflu.2015.10.004
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The flow patterns and vortex suppression regions for three circular cylinders with two different staggered arrangements were numerically investigated by the immersed boundary method based lattice Boltzmann method. The first arrangement is that one primary cylinder was placed in front of two assistant cylinders, and the second arrangement is that one primary cylinder was arranged in the wake of two assistant cylinders. The calculations were carried out at fixed spacing ratios with varied Reynolds numbers (100 <= Re <= 200). The flow visualization experiments based on the laser-induced fluorescence technique were also conducted to verify the reliability of simulation results. It was found that the arrangement has a significant influence on the wake structures, force fluctuations and vortex shedding suppression. In the first arrangement, the vortex shedding behind the leading cylinder is suppressed by two assistant cylinders at 100 <= Re <= 200. In the second arrangement, however, the vortex shedding of the trailing cylinder is suppressed by two assistant cylinders at 103 <= Re <= 175. The current results are helpful for designing multiple piers in the practical applications. (C) 2015 Elsevier Masson SAS. All rights reserved.
引用
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页码:207 / 214
页数:8
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