Exploration of the effects of fin geometry and material properties on thermal performance of convective-radiative moving fins

G. Sobamowo, O. Kamiyo, M. Salami, A. Yinusa
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引用次数: 1

Abstract

The performance of fins, commonly used as heat enhancement devices are greatly affected by both the geometry and material properties. These consideration in fin design has stimulated an extensive research interest in the recent time. In this study, investigation on the thermal responses of moving irregular porous fins with trapezoidal, concave and convex profiles of copper, aluminium, silicon nitrides and stainless steel materials is examined. The developed thermal model is solved using differential transform method (DTM). On the verification of result obtained with numerical method using Runge-Kutta, a good agreement with the solution of approximate method is achieved. In the parametric studies carried out, the effect of physical parameters such as convective-conductive, convective-radiative term, internal heat generation, porosity, surface emissivity, power index of heat transfer coefficient, Peclet number and Darcy number on the thermal behaviour of fins are examined and discussed. The comparative analysis carried out on the effect of materials on non-dimensional temperature distribution reveals that copper obtains the highest temperature while the stainless steel gets the lowest. More-so, the fins with concave geometry gives the highest volume adjusted efficiency with increase in Peclet number while that with convex profile has the least. These result output are essential and would be useful in the future design of fins with optimum size reduction and high efficiency.
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翅片几何形状和材料特性对对流辐射运动翅片热性能影响的探讨
翅片通常用作热增强装置,其性能在很大程度上受到几何形状和材料性能的影响。近年来,翅片设计中的这些考虑激发了广泛的研究兴趣。在本研究中,研究了铜、铝、氮化硅和不锈钢材料的梯形、凹形和凸形移动不规则多孔翅片的热响应。利用差分变换方法(DTM)对所建立的热模型进行求解。用龙格-库塔方法对数值方法的结果进行了验证,与近似方法的解有很好的一致性。在参数研究中,考察和讨论了对流传导、对流辐射项、内部发热、孔隙率、表面发射率、传热系数功率指数、Peclet数和Darcy数等物理参数对翅片热性能的影响。对材料对无量纲温度分布的影响进行了对比分析,结果表明:铜的温度最高,不锈钢的温度最低。更重要的是,随着Peclet数的增加,具有凹几何形状的翅片具有最高的体积调节效率,而具有凸轮廓的翅片具有最低的体积调节率。这些结果输出是必不可少的,并且将在具有最佳尺寸减小和高效率的翅片的未来设计中有用。
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