Effect of Spacer Grid Model on Sub-Channel Analysis Code
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摘要: 子通道分析程序只能进行简单的定位格架模型分析,对格架的考虑仅以形阻系数表示,仅能反映轴向的平均阻力效应,难以反映格架上不同角度和排布的交混翼对流场及温度场的影响,不能准确反映格架中的交混翼对局部参数的影响。本文通过选用适当的阻力经验关系式,引入交混翼几何尺寸及交混翼角度,将交混翼对流体产生的力定量地表示出来,添加至动量方程中,建立了新的交混翼分布式阻力模型,并将其耦合到ATHAS子通道分析程序中。程序经过对5×5棒束组件在不同结构下的计算,对比有交混翼和无交混翼子通道内的流场,研究不同形状、角度、排列方式的交混翼产生的效应。Abstract: The sub-channel analysis codes merely conduct the analysis on the simple spacer grid, and represent the spacer as the profile drag coefficient, which can only reflect the average effect of the fluid resistance generated by the axial position and can not accurately reflect the effect of mixing vanes on their local field. In this paper, we choose the empirical correlation appropriately and introduce the geometric dimensions of mixing vanes. The term of mixing vane resistance is expressed quantitatively in the axial and lateral momentum equations of sub-channel analysis. Therefore, we establish the distributed resistance of the mixing vanes model. The improved model is applied to sub-channel analysis code, ATHAS. The effect of different shapes, angles or arrangement of mixing vanes of 5×5 bundle assembly is calculated with and without the improved model. Then the thermal hydraulic performance is analyzed accurately, especially the flow and temperature field.
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Key words:
- Spacer grid model /
- Mixing vanes /
- Distributed resistance method /
- Sub-channel analysis
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