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Flow past a circular cylinder over a free surface: Interaction between the near wake and the free surface deformation

机译:流过自由表面上的圆柱体:近尾流和自由表面变形之间的相互作用

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Air-flow around a circular cylinder placed above a free surface and liquid flow under the free surface were investigated experimentally in a wind/wave tunnel. The cylinder spanned the tunnel test-section and was oriented normal to the freestream direction. The main objective of this study was to investigate the interaction of the cylinder wake with the free surface. The flow structure was analyzed for various gap widths, H, between the cylinder and the free surface using a digital particle image velocimetry (PIV) system with a spatial resolution of 2048 × 2048 pixels. The Reynolds number based on the cylinder diameter was 3.3 × 10{sup}3. For each experimental condition, 400 instantaneous velocity fields were measured and ensemble-averaged to obtain spatial distributions of the mean velocity and turbulence statistics. The results showed that the cylinder near-wake inclined upward due to the influence of the free surface elevation. Vortices were shed, even at a small gap ratio of H/D = 0.2.5, where D is the cylinder diameter. Strong jet-like flow appeared in the gap beneath the cylinder. At a gap ratio of H/D = 0.50, the jet flow exhibited a quasi-periodic vibration with a period of 2-3 s. The free surface deformation was caused by the pressure difference in the air-flow immediately above it. As the gap ratio increased, the inclination angle of the wake and the height of the free surface elevation decreased gradually. The liquid flow under the free surface followed a convective flow motion, and the range of the convection depended on the gap width between the cylinder and the free surface.
机译:在风/波隧道中,对位于自由表面上方的圆柱周围的气流和自由表面下方的液体进行了实验研究。圆柱体跨过隧道测试段,并垂直于自由流方向定向。这项研究的主要目的是研究圆柱尾流与自由表面的相互作用。使用具有2048×2048像素空间分辨率的数字粒子图像测速(PIV)系统分析了圆柱和自由表面之间的各种间隙宽度H的流动结构。基于圆柱直径的雷诺数为3.3×10 {sup} 3。对于每个实验条件,测量了400个瞬时速度场并进行了集合平均,以获得平均速度和湍流统计的空间分布。结果表明,由于自由表面高度的影响,圆柱接近尾流向上倾斜。即使在H / D = 0.2.5的小间隙比(其中D是圆柱直径)的情况下,也不会产生涡流。强烈的喷射流出现在圆柱体下方的间隙中。在间隙比H / D = 0.50时,射流表现出2-3 s的准周期振动。自由表面变形是由紧邻其上方的气流中的压力差引起的。随着间隙比的增加,尾流的倾斜角和自由表面高度的高度逐渐减小。自由表面下的液体流动遵循对流流动运动,对流范围取决于圆柱体和自由表面之间的间隙宽度。

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