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HEAT TRANSFER IN TRAILING EDGE WEDGE-SHAPED PIN-FIN CHANNELS WITH SLOT EJECTION UNDER HIGH ROTATION NUMBERS

机译:高旋转数下带槽的拖曳式楔形楔形翅片通道的传热

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摘要

The heat transfer characteristics of a rotating pin-fin roughened wedge shaped channel have been studied. The model incorporates ejection through slots machined on the narrower end of the wedge, simulating a rotor blade trailing edge. The copperplate regional average method is used to determine the heat transfer coefficient; pressure taps have been used to estimate the flow discharged through each slot. Tests have been conducted at high rotation (≈ 1 ) and buoyancy (≈ 2) numbers, in a pressurized rotating rig. Reynolds Numbers investigated range from 10,000 to 40,000 and rotational speeds range from 0-400rpm. Pin-fins studied are made of copper as well as non-conducting garolite. Results show high heat transfer coefficients in the proximity of the slot. A significant enhancement in heat transfer due to the pin-fins, compared with a smooth channel is observed. Even the non-conducting pin-fins, indicative of heat transfer on the end-wall show a significant enhancement in the heat transfer coefficient. Results also show a strong rotation effect, increasing significantly the heat transfer coefficient on the trailing surface - and reducing the heat transfer on the leading surface.
机译:研究了旋转销翅片粗糙楔形通道的传热特性。该模型结合了通过楔形体较窄端上加工的狭槽的弹出来模拟转子叶片的后缘。用铜板区域平均法确定传热系数。压力抽头已用于估算通过每个缝隙排出的流量。在加压旋转钻机上以高转数(≈1)和浮力(≈2)进行了测试。研究的雷诺数范围为10,000至40,000,转速范围为0-400rpm。所研究的鳍片是由铜以及不导电的方铅矿制成的。结果表明,在缝隙附近有很高的传热系数。与平滑通道相比,观察到由于针状翅片导致的传热显着增强。甚至指示端壁上的热传递的不导电的针状翅片也显示出热传递系数的显着提高。结果还显示出强大的旋转效果,显着增加了后表面上的传热系数,并减少了前表面上的传热。

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