首页> 外文期刊>Frontiers in Heat and Mass Transfer >3D NUMERICAL ANALYSIS ON FLOW CONFIGURATIONS AND HEAT TRANSFER CHARACTERISTICS FOR FIN-AND-OVAL-TUBE HEAT EXCHANGER WITH V-DOWNSTREAM DELTA WINGLET VORTEX GENERATORS
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3D NUMERICAL ANALYSIS ON FLOW CONFIGURATIONS AND HEAT TRANSFER CHARACTERISTICS FOR FIN-AND-OVAL-TUBE HEAT EXCHANGER WITH V-DOWNSTREAM DELTA WINGLET VORTEX GENERATORS

机译:带V降三角洲小翼涡流发生器的翅片和椭圆管换热器的流动结构和传热特性的3D数值分析

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3D numerical investigations for heat transfer characteristics and flow configurations in a fin–and-oval-tube heat exchanger with V-tip pointing downstream delta winglet pairs (DDWP) are examined. The DDWPs are placed on the fin surface with pointing downstream and the oval tube row number is set at three in a staggered arrangement. The flow attack angles (α = 15o, 30o, 45o and 60o) and the distance from V-tip to the oval tube center in transverse axis (a = 3.77, 4.77 and 5.77 mm) are investigated for Reynolds number based on hydraulic diameter, Re = 500 – 2500. The numerical results are compared with the previous experimental results and the validations of the grid system on both heat transfer and friction factor are also reported. As the results, it is found that the use of the DDWP performs higher heat transfer rate and the friction factor over than the smooth fin with no DDWP for all cases. The vortex flows and the impinging jet of the flows over the oval-tube walls lead to the increase in heat transfer rate, but also increase in pressure loss. The augmentations are maximum around 1.59 and 4.4 times higher than the smooth fin for heat transfer and friction factor, respectively. In addition, the optimum thermal enhancement factor, TEF is around 1.09 at Re = 2500, a = 5.77 mm and α = 15o. 
机译:对翅片和卵形管式换热器的VD尖端指向下游的三角翼小翼对(DDWP)的传热特性和流动配置进行了3D数值研究。 DDWP放置在翅片表面上,指向下游,椭圆形管的行数交错排列设置为3。根据水力直径,研究了雷诺数的流动迎角(α= 15o,30o,45o和60o)以及从V-tip到横轴到椭圆形管中心的距离(a = 3.77、4.77和5.77 mm), Re = 500 –2500。数值结果与先前的实验结果进行了比较,并且还报告了网格系统在传热和摩擦系数方面的验证。结果,发现在所有情况下,与没有DDWP的光滑翅片相比,使用DDWP的导热率和摩擦系数更高。在椭圆形管壁上的涡流和撞击的射流导致传热速率增加,但压力损失也增加。对于传热和摩擦系数而言,最大增加量分别比光滑翅片高约1.59和4.4倍。此外,最佳热增强因子TEF在Re = 2500,a = 5.77 mm和α= 15o时约为1.09。

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