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Effect of fin thickness on the air-side performance of wavy fin-and-tube heat exchangers under dehumidifying conditions

机译:翅片厚度对除湿条件下波浪形翅片管换热器空气侧性能的影响

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摘要

This study investigated the effect of fin thickness on the air-side performance of wavy fin-and-tube heat exchangers under dehumidifying conditions. A total of 10 samples were tested with associated fin thickness (δ_f) of 0.115 mm and 0.25 mm, respectively. For a heat exchanger with two rows (N=2) and fin pitch F_p of 1.41 mm, the effect of fin thickness on the heat transfer coefficient is more pronounced. The heat transfer coefficients for δ_f = 0.25 mm is about 5-50% higher than those for δ_f = 0.115 mm whereas the pressure drop for δ_f = 0.25 mm is about 5-20% higher. The unexpected difference in heat transfer coefficient subject to fin thickness is attributable to better interactions between the directed main flow and the swirled flow caused by the condensate droplet for δ_f = 0.25 mm. The maximum difference in heat transfer coefficients for N = 2 and F_p = 2.54 mm subject to the influence of fin thickness is reduced to about 20%, and there is no difference in heat transfer coefficient when the frontal velocity is above 3 m/s. For N ≥ 4 and F_p = 2.54 mm, the influence of fin thickness on the heat transfer coefficients diminishes considerably. This is because of the presence of tube row, and the unsteady/ vortex shedding feature at the down stream of wavy channel. Based on the present test results, a correlation is proposed to describe the air-side performance for wavy fin configurations, the mean deviations of the proposed heat transfer and friction correlations are 7.9% and 7.7%, respectively.
机译:这项研究研究了除湿条件下翅片厚度对波浪形翅片管换热器空气侧性能的影响。总共测试了10个样品,其相关的翅片厚度(δ_f)分别为0.115 mm和0.25 mm。对于具有两排(N = 2)且翅片间距F_p为1.41mm的热交换器,翅片厚度对传热系数的影响更加明显。 δ_f= 0.25 mm的传热系数比δ_f= 0.115 mm的传热系数高约5-50%,而δ_f= 0.25 mm的压降约高5-20%。受翅片厚度影响的传热系数的出乎意料的差异可归因于由δ_f= 0.25 mm的冷凝液滴引起的定向主流与涡旋流之间更好的相互作用。 N = 2和F_p = 2.54 mm时,受翅片厚度的影响,传热系数的最大差异减小到约20%,并且当正面速度高于3 m / s时,传热系数没有差异。当N≥4且F_p = 2.54 mm时,翅片厚度对传热系数的影响将大大减小。这是因为存在管排,并且在波浪通道的下游存在不稳定/涡旋脱落的特征。基于当前的测试结果,提出了一种相关关系来描述波浪状翅片构型的空气侧性能,所提出的热传递和摩擦相关性的平均偏差分别为7.9%和7.7%。

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