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Numerical Study on Flow and Heat Transfer Characteristics of Jet Impingement Cooling

机译:射流冲击冷却流动与传热特性的数值研究

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Three-dimensional numerical study is conducted to investigate the heat transfer characteristics for the flow impingement cooling in the narrow passage based on cooling technology of turbine blade.The effects of the jet Reynolds number, impingement distance and initial cross-flow on heat transfer characteristic are investigated.Results show that when other parameters remain unchanged local heat transfer coefficient increases with increase of jet Reynolds number; overall heat transfer effect is reduced by initial cross-flow; there is an optimal distance to the best effect of heat transfer.
机译:基于涡轮叶片的冷却技术,进行了三维数值研究,研究了窄通道内流动冲击冷却的传热特性,射流雷诺数,冲击距离和初始错流对传热特性的影响如下:结果表明,当其他参数保持不变时,局部传热系数随射流雷诺数的增加而增加;当射流雷诺数增加时,局部传热系数增大。最初的横流降低了整体传热效果;与最佳传热效果之间存在最佳距离。

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