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Force coefficients and Strouhal numbers of four cylinders in cross flow

机译:交叉流中四个气缸的力系数和斯特劳哈尔数

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This paper presents the measurements of force coefficients and Strouhal numbers (St) on four cylinders in a square configuration at subcritical Reynolds numbers (Re) using a piezo-electric load cell in a wind tunnel. Six spacing ratios (LID) varying from 1.69 to 3.83 and 13 angles of incidence α ranging from 0° to 180° at a 15° interval covering all orientations were investigated. With the help of a laser-induced fluorescence visualization technique, it is found that the variation of forces and Strouhal numbers with LID are governed by three distinct flow patterns. They are: (a) free oscillations of shear layers and vortex formation at large LID; (b) reattachment of shear layer or shielding flow for intermediate LID and (c) narrow gap flows for small LID. Two major causes for large fluctuating forces are discussed in this paper and the force results are compared with other measurements. It is concluded that the flow patterns, i.e., the development and the interferences of the free shear layers and the distribution of the wake vortices of the cylinders play a key role in the variation of the forces and shedding frequencies. Consequently, the downstream cylinders are usually subjected to more serious fluctuating forces under the influence of unsteady wake vortices. Also, the upstream cylinders normally experience larger mean drags than the downstream ones.
机译:本文介绍了在风洞中使用压电称重传感器在亚临界雷诺数(Re)下以方形配置的四个圆柱体上的力系数和Strouhal数(St)的测量结果。研究了六个间距比(LID),它们在1.69到3.83之间变化,并且以15°的间隔覆盖了所有方向,从13°的入射角α在0°到180°范围内变化。借助激光诱导的荧光可视化技术,发现力和Strouhal数随LID的变化受三种不同的流型控制。它们是:(a)大LID时剪切层的自由振荡和涡旋形成; (b)中间LID的剪切层或屏蔽流的重新附着,以及(c)小LID的窄间隙流。本文讨论了引起较大波动力的两个主要原因,并将力结果与其他测量结果进行了比较。结论是,流动模式,即自由剪切层的发展和干涉以及圆柱的尾流涡流的分布在力和脱落频率的变化中起关键作用。因此,下游汽缸通常在不稳定的尾流涡流的影响下承受更大的波动力。同样,上游气缸通常比下游气缸承受更大的平均阻力。

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