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EXPERIMENTAL AND NUMERICAL STUDY ON THE CONVECTIVE HEAT TRANSFER AND PRESSURE LOSS IN RECTANGULAR DUCTS WITH INCLINED PIN-FIN ON A WAVY ENDWALL

机译:波浪形尾壁上带有倾斜销的矩形管道的对流换热和压力损失的实验和数值研究

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Local endwall heat transfer characteristics and overall pressure loss of normal and inclined pin fins arrayed in rectangular ducts with flat and wavy endwalls have been investigated to improve the cooling efficiency of jet engine combustor liners. The detailed time-mean local Nusselt number profiles were measured using a naphthalene sublimation method based on the heat/mass transfer analogy. Four kinds of angled pin fins (-45, 0, and +45 degrees with a flat endwall, and -45 degrees with a wavy endwall) were tested and compared with each other. As a result, the average heat transfer coefficient on the flat endwall of normal pin fins was higher than that of the angled pin fins. The average heat transfer coefficient of-45-degree inclined pin fins with a wavy endwall is the same or a little higher than the heat transfer coefficient of those with a flat endwall; however, the pressure loss of the -45-degree inclined pin fins with a wavy endwall is less than the pressure loss of those with a flat endwall. Corresponding numerical simulations using Large Eddy Simulation (LES) with the Mixed Time Scale (MTS) model have been also conducted at Re_d = 1000 for fully developed regions, and the results have shown good quantitative agreement with mass transfer experiments. It can be concluded that wavy endwalls can realize better heat transfer with less pressure loss as long as the aim consists in enhancing endwall heat transfer in inclined pin-fin channels.
机译:为了提高喷气发动机燃烧室衬套的冷却效率,已经研究了排列在矩形管道中的正常和倾斜的针状翅片的局部端壁传热特性和总压力损失,以改善喷气发动机燃烧器衬套的冷却效率。使用基于热/质量传递类比的萘升华方法测量详细的平均时间局部努塞尔数分布。测试了四种成角度的针状翅片(端壁平坦时为-45度,0和+45度,而端壁为波浪状时为-45度)并进行了比较。结果,普通销翅片的平坦端壁上的平均传热系数高于成角度的销翅片的平均传热系数。端壁呈波浪形的-45度倾斜销翅片的平均传热系数与端壁平坦的翅片的平均传热系数相同或略高;但是,具有波浪形端壁的-45度倾斜销翅片的压力损失要小于具有平坦端壁的倾斜翅片的压力损失。对于充分发达的地区,也已在Re_d = 1000处使用大涡模拟(LES)和混合时间标度(MTS)模型进行了相应的数值模拟,结果表明与传质实验具有良好的定量一致性。可以得出结论,波浪形的端壁可以以较小的压力损失实现更好的传热,只要目的在于增强倾斜的针翅式通道中的端壁传热即可。

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