Convective heat transfer coefficient prediction of pin-fin channel based on neural network
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摘要:
针对扰流柱通道结构的流动传热过程进行了仿真研究,构建了该结构内部表面传热系数的快速预测模型。该预测模型首先构建了若干流阻元件用于冷气质量流量预测,之后根据质量流量预测结果计算通道内的流动雷诺数。将雷诺数与几何结构参数组合并输入基于遗传算法优化的反向传播神经网络,分别预测通道内不同结构的平均表面传热系数。最后建立基于肋化传热模型的扰流柱导热等效表面传热系数换算方法,以便将预测模型应用于实际双层壁涡轮叶片的冷效预测。经数值仿真验证,该模型对通道内冷气质量流量和表面传热系数进行组合预测,相对误差控制在5%以内。
Abstract:The heat transfer process of pin-fin channel was studied by simulation, and a prediction model of the internal convective heat transfer coefficient was constructed. Firstly, several flow resistance elements were constructed to predict the cooling air flow rate, and then the Reynolds number in the channel was calculated according to the flow rate. Secondly, the Reynolds number and geometric parameters were combined and fed into a genetic algorithm and back propagation neural network to predict the average convective heat transfer coefficient of elements in the pin-fin channel respectively. Finally, a conversion method of equivalent heat transfer coefficient of pin-fin heat conduction was established based on ribbed heat transfer model, so as to apply the model to the cooling effect prediction of actual double-wall turbine blades. Numerical simulation results showed that the model can predict the flow rate of cool air and the convective heat transfer coefficient in the channel, and the relative error was controlled within 5%.
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表 1 数据集参数方案
Table 1. Parameter scheme of dataset
参数 取值 雷诺数/103 2,5,10,15,20,25 高径比 0.8,1.0,1.2 无量纲流向间距 3,4,5 无量纲横向间距 3,4,5 表 2 质量流量预测效果测试
Table 2. Mass flow prediction test
结构 质量流量/(kg/s) 相对误差/% 预测结果 仿真结果 气膜孔出口 0.005197 0.005143 1.04 劈缝出口 0.05243 0.05201 0.81 表 3 表面传热系数预测效果测试
Table 3. Convective heat transfer coefficient prediction test
Re/104 表面传热系数/(W/(m2·K)) 相对误差/% 预测结果 仿真结果 1.1 3451 3596 4.2 1.9 6170 6466 4.8 -
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