Initial stage of formation of vortex flow in an inductor with counter-rotating magnetic fields

Владимир Сергеевич Озерных, Геннадий Леонидович Лосев, Ефим Гольбрайх, Илья Владимирович Колесниченко
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Abstract

In this article, unsteady flows of electrically conductive fluid in a cylindrical cavity under the action of differently directed rotating magnetic fields are investigated. The relevance of the study is due to the presence of such a flow in the flow meter for liquid-metal heat carrier which is currently under development. The subject of study is the process of formation of the spin-up flow stage in a combined inductor of a rotating magnetic field. The acceleration or the spin-up stage is characterized by a significant change in the angular velocity of the liquid and begins with the formation of low pressure areas due to centrifugal forces. The alternation and movement of low and high pressure areas lead to velocity pulsations. For small values of the control parameter, which is the Taylor number, the flow energy gradually increases. In this case, the steady flow consists of two azimuthal and several poloidal vortices with clearly defined structures. When the Taylor number exceeds a critical value, strong pulsations occur in the flow, resulting in the decay of large-scale vortices. The intensity of the current is characterized by the Reynolds number. A power-law relationship with an exponent of 1.57 has been established between the Reynolds and Taylor numbers. It has been found that the time of formation of a steady flow varies from several seconds to tens of seconds, depending on the value of the Taylor number. The estimates of the control parameters have been obtained for a flowmeter operating in a typical mode. It has been shown that for the correct measurement of flow velocity in the flowmeter, it is necessary that that the Taylor numbers be higher than 108. The study is carried out using mathematical modeling and the obtained results are verified by experiment. The average calculated profiles are located within the confidence intervals of the experimental profiles.
带有反向旋转磁场的感应器中形成涡流的初始阶段
本文研究了在不同方向的旋转磁场作用下,圆柱形空腔中导电流体的非稳态流动。这项研究之所以具有现实意义,是因为目前正在开发的液态金属热载体流量计中存在这种流动。研究主题是旋转磁场组合感应器中旋流阶段的形成过程。加速或旋流阶段的特点是液体角速度发生显著变化,并在离心力作用下开始形成低压区。低压区和高压区的交替和移动导致速度脉动。在控制参数(即泰勒数)值较小的情况下,流动能量会逐渐增加。在这种情况下,稳定流由两个方位涡旋和几个结构清晰的极涡旋组成。当泰勒数超过临界值时,流动中会出现强烈脉动,导致大尺度涡旋衰减。电流强度由雷诺数表征。雷诺数和泰勒数之间存在指数为 1.57 的幂律关系。研究发现,形成稳定流的时间从几秒到几十秒不等,取决于泰勒数的值。在典型模式下运行的流量计的控制参数估计值已经获得。研究表明,要正确测量流量计中的流速,泰勒数必须大于 108。研究是通过数学模型进行的,所获得的结果通过实验进行了验证。计算得出的平均剖面位于实验剖面的置信区间内。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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