空气外掠圆孔翅片管的流动与换热数值模拟

Numerically Simulation of Flowing and Heat Transfer with Airflow Over Holes Fins Tube

摘要:

以矩形平翅片作为比较对象，采用数值模拟方法研究了空气外掠三对称大直径圆孔翅片表面的流动与传热性能，获得了不同Re(雷诺)数时矩形平翅片和三对称大直径圆孔翅片表面的速度场、温度场和Nu(努塞尔)数分布.平翅片的模拟结果与实验数据的最大误差小于10%，证明了该模拟方法的正确性.研究结果表明：当气流Re=1 610~6 440时，三对称大直径圆孔翅片的表面传热系数比平翅片提高25%以上.证明该圆孔翅片是一种适用于翅片管式制冷换热器且传热效果优越的片型.

Abstract:

The performance of the flowing and heat transfer with airflow over the three symmetrical bigholes fins tube are studied by the numerical simulation in comparison with the plane fines.The distributions of the velocity,temperature and Nu(Nuselt number) on the surfaces of the plane fins and the three symmetrical bigholes fins at different Re numbers are obtained.The maximal error between the modeling result and experiment bats of the plane fins is less than 10%,which verifies the simulation method.The simulation results prove that when the air flow Re number changes from 1 610 to 6 440,the surface heat transfer of the three symmetrical bigholes fin is higher by over 25 percent in comparison with the plane fin.This kind of fin is applicable to the fintube cooling heat exchanger and the effect of heat transfer is perfect.