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CFD modelling of turbulent flows through 5 x 5 fuel rod bundles with spacer-grids

机译:CFD对湍流通过5 x 5燃料棒束(带隔离栅)的CFD建模

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In this investigation, post benchmark evaluation of the OECD/NEA-KAERI MATiS-H benchmark was performed to predict the turbulence intensities as well as velocity variation downstream of the split-vane spacer grid. A three-dimensional Computational Fluid Dynamics (CFD) tool (STAR-CCM+) was used to model the single phase flow through a cold 5-by-5 rod bundle with a split-vane spacer grid. The effects of the domain length upstream of the split-vane spacer grid and the mesh resolution at the split-vane spacer grid regions were assessed for their impact on the predicted attenuation of turbulence intensity downstream of the spacers. Polyhedrons were used to discretize the computational domain, along with prismatic cells near the walls, with an overall mesh count that spanned from 25 M to 64 M cell volumes. The Realizable k-epsilon, k-omega SST and Reynolds stress models were tested to assess their capability in predicting the turbulence intensities as well as the velocities measured in the experiment. The calculated turbulence intensities were found to be dependent on the choice of the turbulence model used, the mesh density on the spacers as well as on the domain length upstream of the spacers. The CFD simulations underpredicted the measured turbulence intensity at the downstream region of the split-vane spacer grid. The predicted velocities, however, were in good agreement with the measurements downstream of spacers. Crown Copyright (C) 2016 Published by Elsevier Ltd. All rights reserved.
机译:在这项调查中,对OECD / NEA-KAERI MATiS-H基准进行基准后评估,以预测分流叶片隔栅下游的湍流强度和速度变化。使用三维计算流体动力学(CFD)工具(STAR-CCM +)来模拟通过带有裂片式隔栅的冷5乘5杆束的单相流。评估了分流叶片隔栅上游区域的长度和分流叶片隔栅区域处的网格分辨率对它们对间隔环下游湍流强度预计衰减的影响。多面体与壁附近的棱柱形单元一起用于离散化计算域,其总体网格计数范围从25 M到64 M单元体积。测试了可实现的k-ε,k-ΩSST和雷诺应力模型,以评估它们预测湍流强度和实验中测得的速度的能力。发现计算的湍流强度取决于所使用的湍流模型的选择,间隔件上的网格密度以及间隔件上游的畴长。 CFD仿真低估了分流叶片隔栅下游区域测得的湍流强度。但是,预测的速度与间隔器下游的测量结果非常吻合。 Crown版权所有(C)2016,由Elsevier Ltd.发行。保留所有权利。

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