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Laminar flow heat transfer studies in a twisted square duct for constant wall heat flux boundary condition

机译:恒定壁热通量边界条件下在扭曲方管中的层流传热研究

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The problem of fluid flow and heat transfer was studied for flow inside twisted duct of square cross-section. Three-dimensional numerical solutions were obtained for steady fully developed laminar flow and for uniform wall heat flux boundary conditions using commercially available software. Reynolds number range considered was 100-3000. Twist ratio used are 2.5, 5, 10 and 20. Fluids considered are in Prandtl number range of 0.7-20. Product of friction factor and Reynolds number is found to be a function of Reynolds number and maximum values are observed for a twist ratio of 2.5 and Reynolds number of 3000. Maximum Nusselt number is observed for the same values along with Prandtl number of 20. Correlations for friction factor and Nusselt number are developed involving swirl parameter. Local distribution of friction factor ratio and Nusselt number across a cross-section is presented. Based on constant pumping power criteria, enhancement factor is defined to compare twisted ducts with straight ducts. Selection of twisted square duct is presented in terms of enhancement factor. It is found that twisted duct performs well in the laminar region for range of parameters studied. Heat transfer enhancement for Reynolds number of 3000 and Prandtl number of 0.7 for twist ratio of 2.5, 5, 10, and 20 is 20%, 17.8%, 16.1% and 13.7%, respectively. The results are significant because it will contribute to development of energy efficient compact size heat exchangers.
机译:研究了方形截面扭曲管道内部的流体流动和传热问题。使用可商购的软件获得了稳定的完全展开的层流和均匀的壁热通量边界条件的三维数值解。雷诺数范围为100-3000。所使用的扭曲比为2.5、5、10和20。所考虑的流体的Prandtl数范围为0.7-20。发现摩擦系数和雷诺数的乘积是雷诺数的函数,并且在2.5的扭曲比和3000的雷诺数下观察到最大值。对于相同的值和20的普朗特数,观察到最大努塞尔数。涉及旋涡参数的摩擦因数和努塞尔数被开发出来。给出了横截面的摩擦系数比和Nusselt数的局部分布。基于恒定的抽气功率标准,定义了增强因子,以将扭曲的风道与直的风道进行比较。根据增强因子介绍了扭曲方管的选择。发现在所研究的参数范围内,扭曲的导管在层流区域中表现良好。对于2.5、5、10和20的扭曲比,雷诺数3000和普朗特数0.7的传热增强分别为20%,17.8%,16.1%和13.7%。结果非常重要,因为它将有助于开发节能紧凑型热交换器。

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