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    表面冲孔影响燃料组件热工水力特性的数值模拟

    Numerical Simulation of Thermal and Hydraulic Characteristics of Fuel Assembly Affected by Surface Punching

    • 摘要: 利用数值模拟方法计算不同雷诺数工况下棒束通道内特别是在定位格架下游的热工水力参数,从沿程压降、努塞尔数、综合局部换热因子等方面分析了不同冲孔模型对定位格架下游段速度和湍流强度的影响,并计算了不同雷诺数范围内的最佳冲孔面积。结果表明:当雷诺数不小于5 871时,相比于未冲孔模型,冲孔模型均能起到降低下游段压降的效果;雷诺数大于6 605时,在搅浑叶片表面冲孔会降低叶片出口处的纵向涡量,进而会导致下游流场远场段的努塞尔数降低;当雷诺数小于7 339时,冲孔面积比为15%时综合换热因子的提升最大,但雷诺数大于7 339时,下游远场的局部综合换热系数会随着冲孔面积的增大而逐步降低。

       

      Abstract: Using numerical simulation methods, the thermodynamic and hydraulic parameters in the fuel bundle channel, especially downstream of the positioning grid, were calculated under different Reynolds number conditions. The effects of different punching models on the velocity and turbulence intensity in the downstream of the positioning grid were analyzed from the aspects of pressure drop, Nusselt number and comprehensive local heat transfer factor, and the optimal punching area within different Reynolds number ranges was calculated. Results show that when the Reynolds number is not less than 5 871, compared with the unperforated model, the perforated model can effectively reduce the pressure drop in the downstream section. When the Reynolds number is greater than 6 605, punching holes on the surface of the turbulent blade can reduce the longitudinal vorticity at the blade outlet, which leads to a decrease in the Nusselt number in the far field of the downstream flow field. When the Reynolds number is less than 7 339, the comprehensive heat transfer factor increases the most when the punching area ratio is 15%. However, when the Reynolds number is greater than 7 339, the local comprehensive heat transfer coefficient in the downstream far-field will gradually decrease with the increase of punching area.

       

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