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Numerical Investigation of Thermal-Hydraulic Performance of Channel with Protrusions by Turbulent Cross Flow Jet

机译:湍流交叉流动射流与突出通道热液压性能的数值研究

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In this two dimensional numerical investigation, small rectangular channel with right angled triangular protrusions in the bottom wall of test section is considered. A slot nozzle is placed at the middle of top wall of channel which impinges air normal to the protruded surface. A duct flow and nozzle flow combined to form cross flow which is investigated for heat transfer enhancement of protruded channel. The governing equations for continuity, momentum, energy along with SST k-ω turbulence model are solved with finite volume based Computational fluid dynamics code ANSYS FLUENT 14.0. The range of duct Reynolds number considered for this analysis is 8357 to 51760.The ratios of pitch of protrusion to height of duct considered are 0.5, 0.64 and 0.82. The ratios of height of protrusion to height of duct considered are 0.14, 0.23 and 0.29. The effect of duct Reynolds number, pitch and height of protrusion on thermal-hydraulic performance is studied under cross flow condition. It is found that heat transfer rate is more at relatively larger pitch and small pressure drop is found in case of low height of protrusion.
机译:在这两种尺寸数值调查中,考虑了在试验部分的底壁中具有正确成角度的三角形突起的小矩形通道。槽喷嘴放置在通道顶部壁的中间,其将垂直于突出表面的空气撞击。管道流量和喷嘴流量结合形成交叉流动,该横流被研究用于传热增强突出的通道。用于连续性,动量,能量以及SST k-Ω湍流模型的控制方程被求助于有限的基于体积的计算流体动力学代码ANSYS流畅的14.0。考虑该分析的管道雷诺数的范围是8357至51760.突出的突出距离对所考虑的管道高度为0.5,0.64和0.82。所考虑的管道高度高度的比率为0.14,0.23和0.29。在交叉流动条件下,研究了导管雷诺数,螺距和突起高度对热液压性能的影响。结果发现,在突起高度的情况下,在突起高度的情况下,发现传热速率更大。

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