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Two-dimensionality of a cantilevered-cylinder wake in the presence of an oscillating upstream cylinder

机译:上游存在振荡圆柱时悬臂圆柱尾流的二维

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The effect of a longitudinally oscillating cylinder on the two-dimensionality of flow around a downstream cylinder is studied based on a two-point correlation measured using two hot-wires. The oscillation amplitude is A/d = 0.472 and the oscillation frequency f{sub}e/f{sub}s = 0.0372 and 0.186, where d is the cylinder diameter and f{sub}s the frequency of natural vortex shedding from an isolated stationary cylinder. Three centre-to-centre spacing (L) ratios of the two cylinders were examined, i.e., L/d= 1.8, 2.5 and 4.8, representing three typical flow regimes. The experiment was conducted at a Reynolds number (Re) of 5920, based on d and the free-stream velocity. It is found that the spanwise correlation of the flow depends on not only the oscillation but also the flow regimes. At L/d= 1.8, the correlation is strongest among the three regimes, but worst in the co-shedding regime (L/d =4.8). The upstream cylinder oscillation improves the spanwise correlation of the flow in the gap of the cylinders, irrespective of regimes, especially for L/d =1.8 and 2.5, but impairs that behind the cylinders for L/d = 1.8 and 2.5 due to a change in the flow regime. A theoretical analysis based on the boundary vorticity theory indicates that the oscillation increases the vorticity flux, in particular, in the spanwise direction between the cylinders, resulting in a significantly improved spanwise correlation, though this increase is negligibly small behind the downstream cylinder.
机译:基于使用两根热线测量的两点相关性,研究了纵向振荡圆柱体对下游圆柱体二维流动的影响。振荡振幅为A / d = 0.472,振荡频率f {sub} e / f {sub} s = 0.0372和0.186,其中d为圆柱直径,f {sub} s为孤立涡流从自然涡流中脱落的频率固定缸。检查了两个气缸的三个中心距(L),即L / d = 1.8、2.5和4.8,代表了三种典型的流动状态。实验基于d和自由流速度在5920的雷诺数(Re)下进行。发现流动的翼展方向相关性不仅取决于振荡而且还取决于流动状态。在L / d = 1.8时,这三种关系之间的相关性最强,但在共同脱落模式中则最差(L / d = 4.8)。上游汽缸振动改善了汽缸间隙中流量的跨度相关性,而与状态无关,尤其是对于L / d = 1.8和2.5而言​​,但由于变化,削弱了L / d = 1.8和2.5时汽缸后面的流量在流动状态。基于边界涡度理论的理论分析表明,振荡会增加涡流通量,特别是在圆柱体之间的翼展方向上,从而显着改善了翼展方向的相关性,尽管这种增加在下游圆柱体后面微不足道。

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