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Aerodynamic characteristics of two side-by-side circular cylinders and application of wavelet analysis on the switching phenomenon

机译:两个并列圆柱的空气动力学特性及小波分析在切换现象中的应用

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The aerodynamic characteristics of two stationary cylinders, both circular and square, in a side-by-side arrangement were investigated experimentally in a uniform flow at a Reynolds number of 5.5 × 10{sup}4, although the square cylinder results are rather limited. This Reynolds number is within the range in which fluid forces acting on a single cylinder are comparatively insensitive to change in the Reynolds number. The focus of this study was on the determination of the characteristics of steady and fluctuating fluid forces, wake frequencies and switching phenomena in two side-by-side cylinders. For a spacing ratio of T/D<1.2 (T, gap spacing between cylinders; D, diameter), the gap flow was biased to one side, resulting in the formation of a narrower wake behind one cylinder and a wider wake behind the other. Steady and fluctuating fluid forces acting on the cylinders were decomposed for the narrower wake and the wider wake flow patterns. For T/D > 0.20, the action of lift forces on both cylinders was in an outward direction (repulsive); however, for T/D = 0.10, the action of lift force on the cylinder associated with the narrower wake was inward and that on the other cylinder was outward. In the bistable flow regime, T/D = 0.2-1.2, when the gap flow switched spontaneously from one side to the other, another short duration stable flow pattern (which can be termed an intermediate flow pattern) persisted in the intermediate time, in which the gap flow was oriented parallel to the free-stream flow and the Strouhal number was almost equal to that of a single cylinder. Flow visualization images and results of modal analysis and wavelet analysis of velocity signals obtained from two hot-wires corroborated the appearance of the intermediate flow pattern. In the case of synchronized vortex shedding and even in the intermediate flow pattern, a predominant antiphase synchronized vortex was found in both the case of two side-by-side circular cylinders and the case of two side-by-side square cylinders.
机译:尽管均方箱的结果相当有限,但在均流下以5.5×10 {sup} 4的雷诺数实验研究了两个固定并排的圆形和方形固定缸的空气动力学特性。该雷诺数在以下范围内:作用在单个气缸上的流体力相对不敏感于雷诺数的变化。这项研究的重点是确定两个并排气缸中稳定和波动的流体力,尾流频率和切换现象的特性。对于T / D <1.2的间距比(T,圆柱之间的间隙间距; D,直径),间隙流偏向一侧,导致在一个圆柱后面形成较窄的尾流,在另一个圆柱后面形成较宽的尾流。 。对于较窄的尾流和较宽的尾流流型,作用在气缸上的稳定且波动的流体力被分解。当T / D> 0.20时,两个气缸上的提升力都朝外(排斥);反之,但是,当T / D = 0.10时,升力在与较窄尾流相关的圆柱上的作用是向内的,而在另一个圆柱上的作用是向外的。在双稳态流态,T / D = 0.2-1.2,当间隙流从一侧自发地切换到另一侧时,另一短时稳定流型(可以称为中间流型)在中间时间内持续存在。间隙流的方向平行于自由流,斯特劳哈尔数几乎等于单个气缸的数。流动可视化图像以及从两条热线获得的速度信号的模态分析和小波分析结果证实了中间流动模式的出现。在同步涡流脱落的情况下,甚至在中间流动模式下,在两个并排的圆柱体和两个并排的方筒体中都发现了主要的反相同步涡流。

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