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CONJUGATE HEAT TRANSFER ANALYSIS OF A RECTANGULAR COOLING CHANNEL WITH 45-DEG RIBS

机译:45度肋矩形冷却通道的共轭传热分析

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A conjugate heat transfer simulation of air in a rectangular cooling channel with 45-deg ribs is presented in this paper. The test channel length is 400mm and the ratio of width to height is 1. The hydraulic diameter of the channel is 40mm and the thickness of channel wall is 3mm. The rib height is 1.9mm and the distance between nearby ribs is 19mm. The flow field and the temperature field in the solid channel are obtained by using ANSYS CFX. An energy source is added in the solid domain to simulate the Low-Voltage High-Current heating method in the experiment. The GGI method is adopted for the mesh connection between the fluid domain and solid domain. The SST turbulence model and automatic wall function in ANSYS CFX are used to simulate the flow and heat transfer in near-wall region. The numerical results show great agreement with the experimental data. The temperature distribution on the channel outer wall is shown and analyzed. The Nusselt number field on the channel wall is shown and illustrated by the flow field shown by the Vortex Core Technology. There are four secondary flow vortex cores between ribs in near wall region and a strong secondary flow can be seen in main flow region. The angled ribs leads to the unbalanced temperature and Nusselt number field on the outer wall and the inner wall of the channel respectively. The distribution law of the Nusselt number on inner wall is not similar with the one of temperature on the outer wall. But the overall distribution of outer wall temperature field is more homogeneous compared with that of the inner wall Nusselt number. Some recommendations for optimization are given based on the flow field and Nusselt number distribution.
机译:本文提出了具有45度肋肋的矩形冷却通道中空气的共轭传热模拟。测试通道的长度为400mm,宽高比为1。通道的水力直径为40mm,通道壁的厚度为3mm。肋骨高度为1.9mm,相邻肋骨之间的距离为19mm。固体通道中的流场和温度场是通过使用ANSYS CFX获得的。在固态域中添加了一个能源,以模拟实验中的低压大电流加热方法。流体域和固体域之间的网格连接采用GGI方法。 ANSYS CFX中的SST湍流模型和自动壁功能用于模拟近壁区域的流动和传热。数值结果与实验数据吻合良好。显示并分析了通道外壁上的温度分布。通道壁上的Nusselt数字段由Vortex Core Technology显示的流场显示和说明。在壁附近区域的肋之间有四个次级流动涡流核,并且在主要流动区域中可以看到强烈的次级流动。倾斜的肋条分别导致通道外壁和内壁的温度和Nusselt数场不平衡。内壁上的努塞尔数分布规律与外壁上的温度分布规律不相似。但是,外壁温度场的整体分布与内壁努塞尔数相比更均匀。根据流场和Nusselt数分布给出了一些优化建议。

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