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Large-Eddy Simulation of local heat transfer in plate and pin fin heat exchangers confined in a pipe flow

机译:大涡模拟局限在管流中的板翅式换热器中的局部传热

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Large-Eddy Simulation of heat transfer in plate and pin fin heat exchangers is carried out under constant surface temperature assumption while resolving the surface heat flux by a dense mesh of 28 M cells. The heat exchangers are mounted inside a pipe in a highly constrained space. The heat transfer takes place by forced convection at Re-D = 20000. The numerical simulations are validated by comparison of velocity profiles against experimental flow measurements on 3D-printed aluminium heat exchangers. Both the experiments and simulations indicate higher rate of heat transfer on the outer fins. The numerical findings indicate that, for the plate heat exchanger, the average Nusselt number of the outermost fins is approximately 50% larger than at the inner fins (Nu = 7.54). For the pin fin heat exchanger, we observe a 20% increase in the Nusselt number between the inner and the outer fins. A strongly localized vortex shedding region is observed for the pin fin heat exchanger increasing the local heat transfer by a factor of two. In contrast, for the planar fins, the flow appears steady and laminar in the interior. In addition to strong flow diversion observed for both geometries, we show that for the pin fin array, almost 50% of the flow that enters the heat exchanger leaks to the clearances through the side and tip gaps. For the planar fins, the respective leakage is only 30%. Numerical evidence is also provided on the relevance of variety of flow phenomena including recirculation zones, vortex shedding, flow laminarization as well as flow separation and reattachment, all affecting the local heat transfer. (C) 2019 Elsevier Ltd. All rights reserved.
机译:在恒定的表面温度假设下,同时通过28 M单元的密集网格解决表面热通量,对板翅式和翅片式翅片换热器中的传热进行大涡模拟。热交换器安装在高度受限的空间内的管道内。传热通过强迫对流在Re-D = 20000处进行。通过将速度曲线与3D打印的铝制热交换器上的实验流量测量值进行比较,可以验证数值模拟。实验和模拟均表明外翅片上的传热速率更高。数值结果表明,对于板式换热器,最外侧散热片的平均努塞尔数大约比内侧散热片的平均努塞尔数大(Nu = 7.54)。对于针翅式换热器,我们观察到内翅片和外翅片之间的努塞尔数增加了20%。对于针翅式换热器,观察到强烈的局部涡旋脱落区域,使局部传热增加了两倍。相反,对于平面散热片,内部的流动似乎稳定且呈层状。除了在两种几何结构中均观察到强力的分流以外,我们还显示出,对于针翅阵列,进入热交换器的流量几乎有50%通过侧面和尖端间隙泄漏到间隙中。对于平面散热片,各自的泄漏仅为30%。还提供了各种流动现象的相关性的数字证据,包括再循环区,涡旋脱落,流动层流以及流动分离和重新附着,这些都影响了局部传热。 (C)2019 Elsevier Ltd.保留所有权利。

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