Optimization of louver fin geometries for miniature microchannel condenser by Taguchi and CFD method

S Satheesh Kumar, G Kumaraguruparan, T S Senthilkumar
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Abstract

In this work, optimization of louver fin geometries is performed to obtain better thermal hydraulic performance of multilouvered microchannel heat exchanger by CFD method. Five louver fin geometries are considered in this work namely fin pitch, fin height, louver pitch, louver angle and louver length. The air side performance is analyzed with the help of airside heat transfer coefficient and pressure drop. These parameters are determined using Colburn-j factor and f factor for Reynolds numbers range of 100–600. In this work, two factors are studied for the effect of individual and combined louver fin geometries. It is observed from the literature study that increase in Reynold number, increases the Colburn-j factor and hence increases the rate of heat transfer favorably. At the same time, increase in Reynold number, increase f factor in term increase the pressure drop which is not desirable. Hence, it is challenging to increase the heat transfer without increase the pressure drop characteristics for heat exchanger design. So, aim of this work is to maximize the heat transfer and minimize the pressure drop. To account for these two contradicting objectives, dimensionless number (JF factor) is considered to determine the thermal hydraulic performance for the heat exchanger and it accounts both Colburn-j factor and f factor simultaneously. Orthogonal array-based Taguchi analysis is performed to obtain optimized louver fin geometries. Taguchi-CFD analysis revealed that fin pitch is the most influencing parameter, that alone accounts for 94.33% of contribution ratio on JF factor. Taguchi-confirmation test showed that the enhancement of JF factor for optimal louver fin is 5.97% higher than that of the initial design parameter. Finally, CFD analysis is performed to compare the performance of optimal louver fin geometry with that of the default louver fin geometry. From this analysis, Colburn-j and JF factor of optimum fin geometry are found to be 24.42% and 18.23% higher than those of default fin geometry. Regression models are developed for optimum fin geometry to predict the Colburn-j, f and JF factor for the Reynolds numbers range of 100–850, whose adj. R2 value is 99.05%.

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利用田口和 CFD 方法优化微型微通道冷凝器的百叶窗翅片几何形状
在这项工作中,通过 CFD 方法对百叶窗翅片几何形状进行了优化,以获得多层微通道热交换器更好的热液压性能。本研究考虑了五种百叶窗翅片几何形状,即翅片间距、翅片高度、百叶窗间距、百叶窗角度和百叶窗长度。借助空气侧传热系数和压降分析了空气侧的性能。这些参数是使用 Colburn-j 因子和 f 因子确定的,雷诺数范围为 100-600。在这项工作中,研究了单个百叶鳍片和组合百叶鳍片几何形状的两个影响因素。从文献研究中可以看出,雷诺数的增加会提高 Colburn-j 因子,从而有利地提高传热速率。与此同时,雷诺数的增加会增加 f 因子,从而增加压降,这是不可取的。因此,在设计热交换器时,如何在不增加压降特性的情况下增加传热是一项挑战。因此,这项工作的目标是最大限度地提高传热效率,同时最大限度地降低压降。为了考虑这两个相互矛盾的目标,我们采用了无量纲数(JF 因子)来确定热交换器的热液压性能,它同时考虑了 Colburn-j 因子和 f 因子。通过基于正交阵列的田口分析,获得了优化的百叶窗翅片几何形状。Taguchi-CFD 分析表明,翅片间距是影响最大的参数,仅此一项就占 JF 因子贡献率的 94.33%。Taguchi-confirmation 试验表明,最佳百叶鳍片的 JF 因子比初始设计参数高出 5.97%。最后,还进行了 CFD 分析,以比较最佳百叶窗翅片几何形状与默认百叶窗翅片几何形状的性能。分析发现,最佳翅片几何形状的 Colburn-j 和 JF 因子比默认翅片几何形状分别高 24.42% 和 18.23%。针对最佳翅片几何形状建立了回归模型,以预测雷诺数范围为 100-850 的 Colburn-j、f 和 JF 因数,其辅助 R2 值为 99.05%。
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