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A smoke visualization study of the flow over a square cylinder at incidence and tandem square cylinders

机译:入射和串联方筒上方筒上的流动的烟雾可视化研究

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An experimental investigation of flow around a square cylinder placed at various incidence angles (0-45) with respect to the approach flow is reported (Re_d = 2,033, 6,776, 7,575, 8,246). Also flow over two square cylinders in a tandem arrangement at zero incidence is studied for different gap spacing values ranging from 1d to 6d, where d is cylinder side length (Re_d - 2,033). A low-speed vertical smoke tunnel is used to visualize flow patterns. For single cylinder, the flow patterns, stagnation and separations points, separation angle, attachment point, transient and turbulence lengths of the shear layer, wake length, frequency and Strouhal number for various incidence angles are determined quantitatively using flow visualization and image digitization process. It is found that a critical value appears around α = 15° for aforementioned parameters due to occurrence of the reattachment of the separated shear layer on the lateral face of the cylinder.For tandem cylinders, the effect of gap spacing between cylinders on the flow patterns, separation angle, wake length, and transient and turbulence lengths of the shear layer of the upstream cylinders is investigated. The results showed that there are three flow patterns when the gap spacing values are varied from 1d to 6d. Also it is observed that the aforementioned parameters for the upstream cylinder become approximately similar to those for single cylinder due to reduction in the flow interference of the cylinders at higher gap spacing values, i.e., 5d and 6d.
机译:报道了围绕着相对进近流以不同入射角(0-45)放置的方圆柱体周围流的实验研究(Re_d = 2,033、6,776、7,575、8,246)。还研究了从1d到6d的不同间隙间距值,以零入射的方式串联排列在两个方形圆柱体上的流动,其中d是圆柱体的边长(Re_d-2,033)。低速垂直烟道用于可视化流动模式。对于单缸,使用流动可视化和图像数字化过程定量确定各种入射角的流型,停滞和分离点,分离角,附着点,瞬变和湍流长度,尾流长度,频率和斯特劳哈尔数。发现上述参数的临界值出现在α= 15°附近,这是由于在气缸侧面上分离的剪切层的重新附着所致。对于串联气缸,气缸之间的间隙间距对流型的影响,研究了上游气缸的剪切层的分离角,尾流长度以及瞬变和湍流长度。结果表明,当间隙间隔值从1d变为6d时,存在三种流动模式。还观察到,由于减小了在较高的间隙间距值,即5d和6d处的气缸的流动干扰,上游气缸的上述参数变得与单气缸的参数大致相似。

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