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Investigation on laminar convection heat transfer in fin-and-tube heat exchanger in aligned arrangement with longitudinal vortex generator from the viewpoint of field synergy principle

机译:基于场协同原理的翅片管式换热器与纵向涡流对准布置的层流对流换热研究

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摘要

3-D numerical simulation results are presented for laminar flow heat transfer of the fin-and-tube surface with vortex generators. The effects of Reynolds number (from 800 to 2000), the attack angle (30° and 45°) of delta winglet vortex generator are examined. The numerical results are analyzed from the viewpoint of field synergy principle. It is found that the inherent mechanism of heat transfer enhancement by longitudinal vortex can be explained by the field synergy principle, the second flow generated by the vortex generators results in the reduction of the intersection angle between the velocity and fluid temperature gradient. In addition, the heat transfer enhancement of delta winglet with the attack angle of 45° is larger than that of 30°, while the delta winglet with the attack angle of 45° results in an increase of the pressure drop, however, the delta winglet with the attack angle of 30° results in a slight decrease.
机译:提出了利用涡流发生器对翅片管表面进行层流传热的3-D数值模拟结果。研究了三角翼小涡旋发生器雷诺数(从800到2000),迎角(30°和45°)的影响。从场协同原理的角度分析了数值结果。研究发现,纵向涡流增强传热的内在机理可以用场协同原理来解释,涡流发生器产生的第二股流导致速度与流体温度梯度之间的相交角减小。另外,攻角为45°的三角翼小翼的传热增强大于30°,而攻角为45°的三角翼小翼的传热增强导致压降增大,但是三角翼小翼的传热增强。迎角为30°时会稍微降低。

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