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Contrastive experimental study on heat transfer and friction characteristics in steam cooled and air cooled rectangular channels with rib turbulators

机译:带肋湍流的蒸汽冷却和风冷矩形通道传热和摩擦特性的对比实验研究

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摘要

The present experiment compares the heat transfer and friction characteristics in steam cooled and air cooled rectangular channels (simulating a gas turbine blade cooling passage) with two opposite rib-roughened walls. The Reynolds number (Re) whose length scale is the hydraulic diameter of the passage is set within the range of 10000-60000. The channel length is 1000 mm. The pitch-to-rib height ratio, the channel aspect ratio and the channel blockage ratio is 10, 0.5 and 0.047, respectively. It is found that the average Nu, the average friction coefficient, and the heat transfer performance of both steam and air in the ribbed channels show almost the same change trend with the increase of Re. Under the same test conditions, the average Nu of steam is 30.2% higher than that of air, the average friction coefficient is 18.4% higher, and the heat transfer performances of steam on the ribbed and the smooth walls are 8.4% and 7.3% higher than those of air, respectively. In addition, semi-empirical correlations for the two test channels are developed, which can predict the Nu under the given test condition. The correlations can be used in the design of the internal cooling passage of new generation steam-cooled gas turbine blade/vane.
机译:本实验比较了蒸汽冷却和空气冷却的矩形通道(模拟燃气轮机叶片冷却通道)中的热传递和摩擦特性,该矩形通道具有两个相对的肋形粗糙壁。长度比例为通道的水力直径的雷诺数(Re)设置在10000-60000的范围内。通道长度为1000毫米。螺距与肋的高度比,通道纵横比和通道堵塞比分别为10、0.5和0.047。研究发现,肋骨通道中蒸汽的平均Nu,平均摩擦系数以及蒸汽和空气的传热性能随着Re的增加呈现出几乎相同的变化趋势。在相同的试验条件下,蒸汽的平均Nu比空气高30.2%,平均摩擦系数高18.4%,蒸汽在肋状壁和光滑壁上的传热性能分别高8.4%和7.3%比空气的分别另外,开发了两个测试通道的半经验相关性,可以在给定测试条件下预测Nu。该相关性可用于新一代蒸汽冷却燃气涡轮叶片/叶片的内部冷却通道的设计中。

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