首页> 外文期刊>Experiments in Fluids: Experimental Methods and Their Applications to Fluid Flow >Two- and three-dimensional flows in nearly rectangular cavities driven by collinear motion of two facing walls
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Two- and three-dimensional flows in nearly rectangular cavities driven by collinear motion of two facing walls

机译:由两个相对壁的共线运动驱动的几乎矩形腔中的二维和三维流动

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Two- and three-dimensional flows in nearly cuboidal cavities are investigated experimentally. A tight cavity is formed in the gap between two long and parallel cylinders of large radii by adding rigid top, bottom, and end walls. The cross-section perpendicular to the axes of the cylinders is nearly rectangular with aspect ratio Gamma. The axial aspect ratio Lambda > 10 is large to suppress end-wall effects. The fluid motion is driven by independent and steady rotation of the cylinders about their axes which defines two Reynolds numbers Re (1,2). Stability boundaries of the nearly two-dimensional steady flow have been determined as functions of Re (1,2) for Gamma = 0.76 and Gamma = 1. Up to six different three-dimensional supercritical modes have been identified. The critical thresholds for the onset of most of the three-dimensional modes, three of which have been observed for the first time, agree well with corresponding linear-stability calculations. Particular attention is paid to the flow for Gamma = 1 under symmetric and parallel wall motion. In that case the basic flow consists of two mirror symmetric counter-rotating parallel vortices. They become modulated in span-wise direction as the driving increases. Detailed LDV measurements of the supercritical three-dimensional velocity field and the bifurcation show an excellent agreement with numerical simulations.
机译:实验研究了接近长方体腔中的二维和三维流动。通过添加刚性的顶壁,底壁和端壁,在两个大半径的长且平行圆柱体之间的间隙中形成了一个紧密的空腔。垂直于圆柱体轴线的横截面几乎为矩形,长宽比为Gamma。轴向纵横比Lambda> 10较大,可以抑制端壁效应。气缸绕其轴线独立且稳定地旋转来驱动流体运动,从而定义了两个雷诺数Re(1,2)。对于Gamma = 0.76和Gamma = 1,已经确定了接近二维稳定流的稳定性边界作为Re(1,2)的函数。最多已经确定了六个不同的三维超临界模式。大多数三维模式的开始的临界阈值与相应的线性稳定性计算非常吻合,其中三个是首次被观察到。要特别注意对称和平行壁运动下Gamma = 1的流量。在这种情况下,基本流由两个镜像对称的反向平行旋转涡流组成。随着驱动力的增加,它们在翼展方向上被调制。对超临界三维速度场和分叉的详细LDV测量结果与数值模拟非常吻合。

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