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首页> 外文期刊>International Communications in Heat and Mass Transfer >Surface modification of transversely twisted-turbulator using perforations and winglets: An extended study
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Surface modification of transversely twisted-turbulator using perforations and winglets: An extended study

机译:横向扭曲湍流用过的表面改造使用穿孔和小翼:扩展研究

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摘要

Twisted-turbulators are effective passive techniques for enhancing the thermal performance of heat exchangers. Although numerous studies have been conducted on longitudinal forms, there are very scarce studies on transverse forms. In this study, particular attention is paid on the effects of perforation, winglet, and a combination of both, as modifications, on the performance of transversely twisted-turbulators (TTTS) through a rectangular channel. Firstly, experimental tests are performed on the TTTS with three different twist-angles of 0°, 90°, and 180° for the Reynolds number range from 1643 to 4929. Then, numerical simulations are carried out on these models. It is found that the effects of perforations and winglets depend on the twist-angle of TTTs. In the case of 0° TTTs, introducing both perforations and winglets leads to lower values of h and △p. The results show that the solid model is more effective in fluid dispersion towards the hot walls and generate stronger vortices inside the channel. Based on the experimental data, for the case of 0° TTTs, the average reduction of h and △p between the solid model and other models are as follows, 9.8% and 16.4% for the perforated model, 16.2% and 16.9% for the winged model, and 23.6% and 41.8% for the combined model. However, in the cases of 90° and 180° TTTs, creating winglets enhances these parameters, leading to better overall performance. The highest overall performance indexes of 1.55, 1.66, and 1.65 are recorded for the solid 0° TTT, winged 90° TTT, and winged 180° TTT models at the Reynolds number of 1643.
机译:双绞动机是用于增强热交换器的热性能的有效无源技术。虽然纵向形式进行了许多研究,但对横向形式进行了非常稀缺的研究。在这项研究中,特别注意穿孔,小翼和两者的组合,作为修改,对横向扭曲湍流器(TTTS)的性能通过矩形通道的影响。首先,在具有0°,90°和180°的三种不同的扭曲角度的TTT上进行实验测试,对于雷诺数范围为1643至4929.然后,在这些模型上进行数值模拟。发现穿孔和小翼的影响取决于TTT的扭曲角度。在0°TTT的情况下,引入穿孔和小翼导致H和△P的较低值。结果表明,固体模型在流体分散朝向热壁上更有效,并在通道内产生更强的涡流。基于实验数据,对于0°TTT的情况,固体模型和其他模型之间的H和△P的平均降低如下,穿孔模型的9.8%和16.4%,16.2%和16.9%翼型模型,组合模型的23.6%和41.8%。然而,在90°和180°TTT的情况下,创建小翼增强这些参数,导致更好的整体性能。 1.55,1.66和1.65的最高总体性能指标被记录为固体0°TTT,翅膀的90°TTT,并在雷诺数1643的曲线上有180°TTT模型。

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