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首页> 外文期刊>International Journal of Heat and Mass Transfer >Flow structure identification and analysis in fin arrays produced by cold spray additive manufacturing
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Flow structure identification and analysis in fin arrays produced by cold spray additive manufacturing

机译:冷喷涂增材制造的翅片阵列的流动结构识别与分析

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摘要

The focus of this work is the identification and analysis of the flow structures found in pyramidal pin fin arrays produced using the Masked Cold Gas Dynamic Spraying (MCGDS) additive manufacturing process. The observed flow structures are described, with classic double recirculation patterns being identified. The turbulence intensity levels of the flow in the axial flow channels was measured and it was found that although the flow rates considered in this work correspond to low Reynolds numbers (500-3000), significant turbulence intensity levels are found. Furthermore, these levels increase as the flow progresses downstream, even though the large scale flow structures are well established after a few rows (as little as two in this case). A slight misalignment of the axial and transverse flow channels resulting from imperfections in the masks caused a bypass flow structure to arise in the wake of the pin fins, replacing the double recirculation pattern observed when there is no such misalignment. A CFD model was used to investigate the effect of these misalignments on heat transfer efficiency and predicted that there would be no significant effect in the configurations studied. Finally, this work shows the importance of not only considering the flow structures in the fin's wake, but also the effect of these structures on the turbulence levels of the axial flow channels, which could significantly affect the thermal and hydrodynamic performance.
机译:这项工作的重点是识别和分析在使用屏蔽冷气动态喷涂(MCGDS)增材制造工艺生产的金字塔形针翅阵列中发现的流动结构。描述了观察到的流动结构,并确定了经典的双重再循环模式。测量了轴向流动通道中流动的湍流强度水平,发现尽管此工作中考虑的流速对应于较低的雷诺数(500-3000),但发现了显着的湍流强度水平。此外,这些水平随着流向下游的进行而增加,即使在几行之后(在这种情况下只有两行)就可以很好地建立大规模的流结构。由面罩的缺陷引起的轴向和横向流动通道的轻微错位会在针状翅片的尾流中产生旁路流动结构,从而在没有这种错位的情况下取代了观察到的双重再循环模式。 CFD模型用于研究这些未对准对传热效率的影响,并预测在所研究的构型中不会有显着影响。最后,这项工作表明,不仅要考虑翅片尾流中的流动结构,而且还要考虑这些结构对轴向流动通道湍流水平的影响,这可能会显着影响热力和流体动力性能,这一点很重要。

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