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Numerical Simulations of Co- and Counter-Taylor-Couette Flows: Influence of the Cavity Radius Ratio on the Appearance of Taylor Vortices

机译:共泰勒流和反泰勒涡流的数值模拟:腔半径比对泰勒涡流外观的影响

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Taylor-Couette flows in the annular region between rotating concentric cylinders are studied numerically to determine the combined effects of the co - and counter-rotation of the outer cylinder and the radius ratio on the system response. The computational procedure is based on a finite volume method using staggered grids. The axisymmetric conservative governing equations are solved using the SIMPLER algorithm. One considers the flow confined in a finite cavity with radius ratios η = 0.25, 0.5, 0.8 and 0.97. One has determined the critical points and properties for the bifurcation from the basic circular Couette flow (CCF) to the Taylor Vortex Flow (TVF) state. Indeed, the results are presented in terms of the critical Reynolds number Re_i of the inner cylinder that depends on the rotational Reynolds number of the outer cylinder Re_o andη. To show the capability of the present code, excellent quantitative agreement has been obtained between the calculations and previous experimental measurements for a wide range of radius ratios and rotation rates.
机译:数值研究了旋转同心圆柱之间的环形区域中的Taylor-Couette流动,以确定外圆柱的同向和反向旋转以及半径比对系统响应的综合影响。计算过程基于使用交错网格的有限体积方法。使用SIMPLER算法求解轴对称保守控制方程。人们认为流动被限制在半径比为η= 0.25、0.5、0.8和0.97的有限腔中。人们已经确定了从基本圆形库埃特流(CCF)到泰勒涡流(TVF)状态的分叉的临界点和性质。实际上,结果根据内筒的临界雷诺数Re_i来表示,该临界雷诺数取决于外筒Re_o和η的旋转雷诺数。为了显示当前代码的功能,在各种半径比和旋转速率的计算和以前的实验测量之间已经获得了出色的定量一致性。

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