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Study of heat transfer performance of tube-fin heat exchanger with interrupted annular groove fin

机译:环形槽翅片管翅式换热器传热性能研究

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The numerical analysis on convective heat transfer behavior and pressure drop characteristics of staggered circular tube bank fin heat exchanger with smooth fin and with interrupted half annular groove fin is carried out under the conditions of different tube rows (1,2,3,4,5), different fin spans (1.5mm, 2mm, 2.5mm) and different annular angles of interrupted half annular groove(30°,50°,70°), in addition, the velocity fields and the temperature fields of the structures are obtained. The results show that the ability of heat transfer could be enhanced by increasing tube rows, fin spans and annular angle of interrupted half annular groove in certain range, and the Nu number increases with the increase of Re number, whereas the resistance coefficient decreases with the increase of Re number in the heat exchangers both for the smooth fins and the interrupted half annular groove fins. The features of flow and heat transfer for heat exchanger with interrupted half annular groove fin are obtained by analysis of the formation, development and influence area of the vortices generated by interrupted half annular grooves.
机译:在不同排管数(1,2,3,4,5)的条件下,对光滑翅片和半环形槽翅片错开的交错式圆管排翅片换热器的对流传热行为和压降特性进行了数值分析。 ),获得不同的翅片跨度(1.5mm,2mm,2.5mm)和间断的半环形凹槽的不同环形角(30°,50°,70°),此外,还获得了结构的速度场和温度场。结果表明,在一定范围内,通过增加管排,翅片跨度和间断半环形槽的环形角度,可以提高传热能力,Nu数随Re数的增加而增加,而电阻系数随Re数的增加而减小。光滑翅片和间断的半环形槽翅片在热交换器中的Re数量增加。通过对半环形凹槽翅片的换热器的流动和传热特性进行分析,得到了半环形凹槽翅片产生的涡流的形成,发展和影响面积。

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