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Numerical simulations of steady flow past two cylinders in staggered arrangements

机译:交错排列流经两个气缸的稳定流动的数值模拟

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摘要

This paper presents a numerical study on steady flow around two identical circular cylinders of various arrangements at a low subcritical Reynolds number (Re = 10(3)). The ratio of centre-to-centre pitch distance (P) to the diameter of the cylinder (D) ranges from 1.5 to 4, and the alignment angle (alpha) between the two cylinders and the direction of the cross-flow varies from 0 to 90 degrees. The detailed flow information obtained from direct numerical simulation allows a comprehensive interpretation of the underlying physics responsible for some interesting flow features observed around two staggered cylinders. Four distinct vortex shedding regimes are identified and it is demonstrated that accurate classification of vortex shedding regimes around two staggered cylinders should consider the combination of the flow visualization with the analyses of lift forces and velocity signal in the wake. It is revealed that the change in pressure distribution, as a result of different vortex shedding mechanisms, leads to a variety of characteristics of hydrodynamic forces on both cylinders, including negative drag force, attractive and repulsive lift forces. Two distinct vortex shedding frequencies are identified and are attributed to the space differences based on the flow structures observed in the wake of the cylinders. It is also found that the three-dimensionality of flow in the gap and the shared wake region is significantly weakened in almost two of the classified flow regimes; however, compared with the flow around a single cylinder, active wake interaction at large alpha does not clearly increase the three-dimensionality.
机译:本文提出了在低亚临界雷诺数(Re = 10(3))下围绕各种布置的两个相同圆柱体进行稳定流动的数值研究。中心距螺距(P)与圆柱直径(D)之比为1.5至4,两个圆柱之间的对准角(α)和错流方向为0到90度从直接数值模拟获得的详细流量信息可以全面解释导致两个交错圆柱体周围观察到的有趣流量特征的基本物理原理。确定了四个不同的涡流脱落方式,并证明了围绕两个交错圆柱体的涡流脱落方式的准确分类应考虑流动可视化与尾流中升力和速度信号分析的结合。结果表明,由于不同的涡旋脱落机理,压力分布的变化导致了两个气缸上的流体动力的各种特性,包括负阻力,吸引力和排斥力。基于在汽缸尾流中观察到的流动结构,识别出两个不同的涡旋脱落频率,并将它们归因于空间差异。还发现,在几乎两种分类的流态中,间隙和共享尾流区的三维流动性显着减弱。但是,与围绕单个圆柱体的流动相比,在较大的alpha处的主动尾流交互作用并不能明显增加三维度。

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