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Numerical and experimental study of flow distribution in tubular space of fin-and-tube heat exchanger with modified inlet manifold

机译:改进进气歧管的翅片管式换热器管腔内流量分布的数值和实验研究

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This paper presents the experimental and numerical investigation of flow distribution in the tubular space of cross-flow fin-and-tube heat exchanger. The tube bundle with two rows arranged in staggered formation is considered. A modified heat exchanged manifold, with inlet nozzle pipe located asymmetrically is considered. The outlet nozzle pipe is located in the middle of the outlet manifold, with a standard shape. An experimental stand allows one to investigate the volumetric flow rate in heat exchanger tubular space using the ultrasonic flowmeters. Various inlet mass flow rate i.e. 3 m~(3)/h, 4 m~(3)/h and 5 m~(3)/h are considered. The experimental results are compared with CFD simulation performed in ANSYS CFX program using the SSG Reynolds Stress turbulence model. A relatively good agreement is found for tube Re numbers varied from 1800 to 3100.
机译:本文提出了横流翅片管式换热器管腔内流动分布的实验和数值研究。考虑两排交错排列的管束。考虑一种改进的热交换歧管,其中进气管不对称。出口喷嘴管位于出口歧管的中间,呈标准形状。实验台允许使用超声波流量计研究换热器管状空间中的体积流量。考虑各种入口质量流量,即3 m〜(3)/ h,4 m〜(3)/ h和5 m〜(3)/ h。将实验结果与使用SSG雷诺应力湍流模型在ANSYS CFX程序中执行的CFD仿真进行了比较。对于从1800到3100的Re数管,找到了相对较好的协议。

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