...
首页> 外文期刊>Applied thermal engineering: Design, processes, equipment, economics >Effect of longitudinal vortex generator on heat transfer in rectangular channels
【24h】

Effect of longitudinal vortex generator on heat transfer in rectangular channels

机译:纵向涡流发生器对矩形通道传热的影响

获取原文
获取原文并翻译 | 示例

摘要

Average convective heat transfer on the top and bottom surfaces of a plain plate and four plates with a pair of delta winglet longitudinal vortex generator punched directly from the plates at attack angles of 15°, 30°, 45° and 60° respectively, is experimentally and numerically studied in the present paper. The plate fixed horizontally in the center of the tested channel is designed to simulate the forced heat transfer on the both surfaces of a single piece of fin in a fin-tube heat exchanger. Experimental results show that the average Nusselt number on the surfaces of plate increases with the increase of the attack angle of delta winglet pair compared with that of plain plate without delta winglet pair in the test range. The average Nusselt number of the plate with attack angle of 60° is slightly higher than that of plate with attack angle of 45°, yet may bring larger pressure drop. Strong longitudinal vortices are visualized when air flow across the leading-edges of the winglet pair. And a portion of air stream flows into the lower channel through the punched holes on the plates after rushing at the frontal face of delta winglet, and disturbs the flow field of the lower channel further. The heat transfer in the tested channel of five cases is also numerically investigated. Variance of average Nusselt number between the numerical results and experimental results for the five cases are all less than 10%, validating the present models and methods used for the simulation of fin channel flow with punched vortex generators feasible and reliable. The computed velocity and temperature fields are analyzed to understand the details of fin channel flow with longitudinal vortex generator. The experimental and numerical results reveal that the transverse flow of air stream through the punched holes disturbs the air flow in the lower channel, enhancing the heat transfer on the under surface of fin.
机译:实验研究了在普通平板的顶部和底部以及四个平板上分别用一对三角翼小翼纵向涡流发生器分别以15°,30°,45°和60°的攻角直接冲孔的平均对流传热。并在本文中进行了数值研究。水平固定在测试通道中心的板设计为模拟在翅片管热交换器中单片翅片的两个表面上的强制传热。实验结果表明,在测试范围内,与不带小翼对的平板相比,平板表面的平均努塞尔数随对角小翼的迎角的增加而增加。迎角为60°的平板的平均Nusselt数略高于迎角为45°的平板的Nusselt数,但可能带来更大的压降。当空气流过小翼对的前缘时,可以看到强烈的纵向涡流。并且一部分气流冲入三角翼小翼的正面后,通过板上的穿孔流入下部通道,进一步扰乱下部通道的流场。还对5种情况下测试通道中的传热进行了数值研究。这五种情况的数值结果与实验结果之间的平均努塞尔数方差均小于10%,验证了目前用于冲孔涡流发生器模拟翅片通道流动的模型和方法的可行性和可靠性。分析计算的速度和温度场,以了解纵向涡流发生器产生的翅片通道流的细节。实验和数值结果表明,通过冲孔的横向气流扰动了下部通道中的气流,从而增强了散热片下表面的热传递。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号