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首页> 外文期刊>Journal of Heat Transfer >Thermal Characteristics in a Curved Rectangular Channel With Variable Cross-Sectional Area
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Thermal Characteristics in a Curved Rectangular Channel With Variable Cross-Sectional Area

机译:变截面面积的矩形矩形通道中的热特性

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摘要

Heat transfer due to steady, laminar airflow through a curved rectangular channel with a variable cross-sectional (c/s) area is investigated computationally. Such a flow passage is formed between two fin walls of a curved fin heat sink with a 90 deg bend, used in avionics cooling. Simulations are carried out for two different configurations: (a) a variable c/s area curved channel with inlet and outlet sections (entry and exit lengths) that are straight and constant c/s area-termed as the long channel and (b) a variable c/s area curved channel with no entry and exit lengths-termed as the short channel. Multiple secondary flow patterns develop in the curved section of the channel, which in conjunction with the bulk axial flow, lead to the formation of multiple vortices and separation bubbles. The complex 3-D flow structures, as well as the variable c/s area of the curved channel (diverging-converging) significantly alter the heat transfer characteristics, compared to the straight fin heat sink. Secondary flow strengthens with increasing axial (bulk) flow velocity, or Dean number in dimensionless form. This in turn improves heat transfer from all walls, particularly, the outer curvature (concave) wall and the heat sink base. At the highest Dean number condition, the local heat transfer coefficient at certain locations of the outer curvature wall is augmented by as much as 3.5 times, compared to the straight fin walls. The overall channel average heat transfer coefficient is improved by about 40% for the long channels, and about 10% for the short ones. However, the heat transfer enhancement is associated with a penalty of higher pressure drop, compared to the straight channels. To quantify the effectiveness of thermal performance enhancement a system Figure of Merit (FOM) is defined. A greater than unity FOM value is observed for all curved channel geometries and flow rate conditions. This indicates that heat transfer enhancement in the variable c/s area curved channel outweighs the penalty of additional pressure drop, compared to a straight channel of similar length.
机译:通过稳定的层流气流通过具有可变横截面(c / s)面积的弯曲矩形通道,进行了计算研究。这样的流动通道形成在具有90度弯曲的弯曲翅片散热器的两个翅片壁之间,用于航空电子冷却。针对两种不同的配置进行了仿真:(a)可变c / s面积的弯曲通道,其入口和出口部分(入口和出口的长度)是直的且恒定的c / s面积,称为长通道;(b)一个没有入口和出口长度的可变c / s面积弯曲通道,称为短通道。在通道的弯曲部分中形成了多个次级流型态,这些次级流型态与整体轴向流相结合,导致形成多个涡旋和分离气泡。与直翅片散热器相比,复杂的3-D流动结构以及弯曲通道的可变c / s面积(发散-会聚)显着改变了传热特性。二次流随着轴向(体)流速的增加而增强,或无量纲形式的Dean数增加。这进而改善了从所有壁,特别是外曲率(凹面)壁和散热器基座的传热。在最高迪恩数条件下,与直翅片壁相比,外曲率壁某些位置的局部传热系数增加了3.5倍。长通道的总通道平均传热系数提高了约40%,短通道的总传热系数提高了约10%。然而,与直通道相比,传热的增强伴随着更高的压降的损失。为了量化热性能增强的有效性,定义了系统品质因数(FOM)。对于所有弯曲的通道几何形状和流速条件,观察到的FOM值均大于1。这表明,与类似长度的直通道相比,在可变c / s面积的弯曲通道中传热的增强超过了额外压降的损失。

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