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OPTIMIZATION OF LONGITUDINAL RECTANGULAR FINS WITH ASYMMETRICAL BOUNDARY CONDITIONS

机译:不对称边界条件优化纵向矩形翅片

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Longitudinal rectangular fins with asymmetrical boundary conditions and different temperatures at each base were been studied and optimized using relative inverse thermal admittance as performance coefficient. A Neutral Line was defined and determined for different temperature ratios at the bases. Using the network method for the numerical simulation, the optimization problem was solved in a classical way: starting with the fin volume, heat transfer coefficient and thermal conductivity, the optimal geometry or aspect ratio (length/thickness ratio) for dissipating maximum heat from the fin surface was determined. The results are illustrated through tables and universal graphics made with optimal points, which, are independent from the temperature ratio at the bases. Besides the optimal thickness the graphics also provide, the fin effectiveness and the transversal Biot number. Finally, the location of the Neutral Line is represented for the optimal geometry and temperature ratios. To illustrate the optimization process practical examples are shown.
机译:使用相对逆热导入作为性能系数,研究并优化了具有不对称边界条件的纵向矩形和每个碱的不同温度。定义中性线并确定碱基的不同温度比。使用网络方法进行数值模拟,优化问题以经典的方式解决:从鳍体积,传热系数和导热率开始,最佳几何或纵横比(长/厚度比),用于消散来自的最大热量确定翅片表面。结果通过具有最佳点制造的表和通用图形来说明,这些表格与基部的温度比无关。除了最佳厚度之外,图形还提供,鳍效果和横向生物编号。最后,为最佳几何和温度比表示中性线的位置。为了说明优化过程,示出了实际示例。

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