Large Eddy Simulation of a Submerged Vortex in a Simplified Computational Model

Y. Yamade, C. Kato, T. Nagahara, J. Matsui
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Abstract

The flow structures of a submerged vortex that appears in a model pump sump were numerically investigated by performing large eddy simulation (LES) of a model vortex in a simplified computational model with a sufficiently fine grid that could resolve the vortex core. The simplified model is designed to simulate the flow under the bellmouth in a model pump sump. The model pump sump is composed of a 2,500 mm-long water channel of rectangular cross section with a width of 300 mm, a water height of 150 mm and a vertical suction pipe with a diameter of 100 mm installed at its downstream end. Our previous large eddy simulations, which used approximately 2 billion grids and were applied to the model pump sump, have fully clarified the origin and formation mechanism of a submerged vortex. In these computations, however, the static pressure in the vortex core decreased only by as much as 4 kPa at a channel velocity of 0.37 m/s. The decrease in the static pressure was far smaller than the one for which one can expect initiation of cavitation in the vortex core. The static pressure drop was most likely to be underpredicted in our previous LES. Insufficient grid resolution was assumed to be one of the reasons for this underprediction. In the present study, LES with a sufficiently fine grid was applied to the simplified computational model that represents the stretch of a submerged vortex under a constant acceleration of the vertical velocity. Case studies for which the grid resolution was varied between 3.25 and 150 micrometres were performed while the size of the vortex core appeared in the simplified model was 500 micrometres. As a result, we confirmed the grid resolution finer than 15 micrometres is needed to resolve the vortex core with a diameter of 500 micrometres. Vertical and tangential velocities obtained by averaging those distributions of a submerged vortex that was computed in our previous LES were prescribed at the bottom wall of the computational domain as the inlet boundary conditions. In the present LES with the grid resolution finer than 15 micrometres, the static pressure decreased by more than 100 kPa. In addition, the parametric studies where the initial swirl numbers were changed have fully clarified the change in the dynamics of a submerged vortex. We found that a strong submerged vortex appears only at a relatively small range of the swirl-number from 1 to 3.
水下大涡的简化计算模型模拟
通过对模型涡进行大涡模拟(LES),在简化计算模型中采用足够细的网格来分解涡核,对模型泵水池中出现的淹没涡的流动结构进行了数值研究。设计了简化模型来模拟某型号水泵水槽内钟口下的流动。该模型水泵水槽由宽300mm的矩形截面长2500mm的水槽,水高150mm,下游端安装直径100mm的垂直吸水管组成。我们以前的大涡模拟使用了大约20亿个网格,并应用于模型泵水池,已经充分阐明了淹没涡的起源和形成机制。然而,在这些计算中,当通道速度为0.37 m/s时,漩涡核心的静压仅下降了4 kPa。静压的下降远远小于涡核中空化的产生。在我们以前的LES中,静压降最有可能被低估。网格分辨率不足被认为是这种预测不足的原因之一。在本研究中,将具有足够细网格的LES应用于表示垂直速度恒定加速度下淹没涡伸展的简化计算模型。对网格分辨率在3.25 ~ 150微米之间变化,而简化模型中出现的涡核尺寸为500微米的情况进行了案例研究。因此,我们确认需要小于15微米的网格分辨率来解析直径为500微米的涡旋核心。在计算区域的底部壁面上规定了垂直速度和切向速度作为入口边界条件。在目前的网格分辨率小于15微米的LES中,静压降低了100 kPa以上。此外,改变初始旋涡数的参数化研究也充分阐明了淹没涡动力学的变化。我们发现强烈的淹没涡只出现在漩涡数1到3的相对较小范围内。
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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