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Heat transfer augmentation in a wedge-ribbed channel using winglet vortex generators

机译:使用小翼涡发生器在楔肋通道中增加传热

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Experimental investigations have been carried out to study the effect of combined wedge ribs and winglet type vortex generators (WVGs) on heat transfer and friction loss behaviors for turbulent airflow through a constant heat flux channel. To create a reverse flow in the channel, two types of wedge (right-triangle) ribs are introduced: wedge ribs pointing downstream and pointing upstream. The arrangements of both rib types placed inside the opposite channel walls are in-line and staggered arrays. To generate longitudinal vortex flows through the tested section, two pairs of the WVGs with the attack angle of 60° are mounted on the test channel entrance. The test channel has an aspect ratio, AR = 10 and height, H = 30 mm with a rib height, e/H = 0.2 and rib pitch, P/H = 1.33. The flow rate in terms of Reynolds numbers is based on the inlet hydraulic diameter of the channel ranging from 5000 to 22,000. The presence of the combined ribs and the WVGs shows the significant increase in heat transfer rate and friction loss over the smooth channel. The Nusselt number and friction factor values obtained from combined the ribs and the WVGs are found to be much higher than those from the ribs/ WVGs alone. In conjunction with the WVGs, the in-line wedge pointing downstream provides the highest increase in both the heat transfer rate and the friction factor while the staggered wedge pointing upstream yields the best thermal performance.
机译:已经进行了实验研究以研究组合楔形肋和小翼型涡流发生器(WVG)对湍流通过恒定热通量通道的传热和摩擦损失行为的影响。为了在通道中产生反向流动,引入了两种类型的楔形(直角三角形)肋:指向下游和指向上游的楔形肋。布置在相对的通道壁内的两种肋类型的布置是直列和交错的阵列。为了在测试部分产生纵向涡流,在测试通道入口安装了两对迎角为60°的WVG。测试通道的长宽比为AR = 10,高度为H = 30 mm,肋骨高度为e / H = 0.2,肋骨间距为P / H = 1.33。以雷诺数表示的流量基于通道的入口液压直径,范围为5000至22,000。结合的肋条和WVG的存在表明,在光滑通道上的传热速率和摩擦损失显着增加。发现从肋骨和WVG的组合获得的Nusselt数和摩擦系数值比单独从肋骨/ WVG的Nusselt数和摩擦系数值高得多。与WVG结合使用时,下游的直列楔形物在传热速率和摩擦系数方面都提供了最大的增长,而交错的楔形物指向上游则产生了最佳的热性能。

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