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SHEAR-LAYER INSTABILITY IN A ROTATING SYSTEM

机译:旋转系统中的剪切层不稳定

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摘要

The shear-layer instability in the flow over a rotating disk with a free surface is investigated experimentally by flow visualizations for a large range of the flow control parameters: the aspect ratio G of the cavity, the rotationnal Reynolds number Re, and the radius ratio s between the inner and outer radii of the rotating disk. This instability develops along the cylindrical shroud as sharp-corner polygonal patterns characterized by the number of vortices m. This number m can be scaled by considering an Ekman number based on the water depth, which confirms that the shroud boundary layer is of Stewartson type. The appearance threshold of the first polygonal mode is constant by considering the mixed Reynolds number introduced by Niino and Misawa based on both the water depth at rest and the rotating disk radius. For large values of s, the instability patterns appear along the hub as small stationary cells.
机译:通过流动可视化,通过实验对大范围的流动控制参数进行了实验,以研究具有自由表面的旋转圆盘上的流动中的剪切层不稳定性:空腔的长宽比G,旋转雷诺数Re和半径比在旋转盘的内半径和外半径之间。这种不稳定性沿着圆柱状护罩发展为尖角多边形图案,其特征是涡旋数m。可以通过考虑基于水深的埃克曼数来缩放此数字m,这确认了护罩边界层是Stewartson类型的。通过基于静止时的水深和转盘半径,考虑由Niino和Misawa引入的混合雷诺数,第一多边形模式的出现阈值是恒定的。对于较大的s,不稳定性模式沿中心线显示为小型固定单元。

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