首页> 外文期刊>International Journal of Heat and Mass Transfer >Influence of channel aspect ratio on heat transfer in rotating rectangular ducts with skewed ribs at high rotation numbers
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Influence of channel aspect ratio on heat transfer in rotating rectangular ducts with skewed ribs at high rotation numbers

机译:高旋转数时通道长宽比对带斜肋的旋转矩形管传热的影响。

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摘要

Centerline heat transfer measurements along two opposite ribbed walls in three rotating rectangular ducts roughened by 45° staggered ribs with channel aspect ratios (AR)of 1:1, 2:1 and 4:1 are performed at Reynolds (Re), rotation (Ro) and buoyancy (Bu) numbers in the ranges of 5000-30,000, 0-2, and 0.005-8.879, respectively. These channel geometries are in common use as the internal cooling passages of a gas turbine rotor blade and the tested Ro and Bu ranges are considerably extended from the previous experiences. This study focuses on the heat transfer characteristics in response to the change of AR under the parameter ranges examined. With zero-rotation (Ro = 0), the local Nusselt numbers (Nu_0) along the cen-terlines of two opposite ribbed walls increase as AR increases due to the increased rib-height to channel-height ratio. The Bu impact on heat transfer appears to be AR dependent, i.e. the increase of Bu elevates Nusselt number ratios NujNu_o in the square channel but impairs heat transfer in the rectangular channels of AR = 2 and 4. Acting by the Coriolis effect alone, all the leading edge Nu values in the present Ro range are lower than the zero-rotation references but started to recover as Ro increases from 0.1 in the channels of AR= 1, 2 and from 0.3 in the channel of AR=4. The trailing edge Nu/Nu_0 ratios increase consistently from unity as Ro increases but their responses toward the increase of AR are less systematic than those found along the leading edge. The above findings, with the aids of extended Ro and Bu ranges achieved by this study, serve as the original contributions for this technical community. The Nu/Nuo ratios in the rotating channels of AR= 1, 2, and 4 fall in the ranges of 0.6-2.2, 0.5-2.7, and 0.5-2.1, respectively. A set of heat transfer correlations is derived to represent all the heat transfer data in the periodically developed flow regions of three rotating ducts.
机译:在雷诺兹(Re),旋转(Ro)下,在三个旋转的矩形管道中沿两个相对的肋壁进行中心线传热测量,这些矩形管道通过45°交错肋进行粗化,通道纵横比(AR)为1:1、2:1和4:1 )和浮力(Bu)数分别在5000-30,000、0-2和0.005-8.879之间。这些通道的几何形状通常用作燃气轮机转子叶片的内部冷却通道,并且经过测试的Ro和Bu范围从以前的经验中得到了大大扩展。这项研究的重点是在所检查的参数范围内响应AR变化的传热特性。零旋转(Ro = 0)时,由于肋高与通道高之比的增加,沿两个相对肋壁中心线的局部Nusselt数(Nu_0)随着AR的增加而增加。 Bu对传热的影响似乎与AR有关,即Bu的增加会提高方形通道中的Nusselt比值NujNu_o,但会削弱AR = 2和4的矩形通道中的传热。仅靠科里奥利效应,所有当前Ro范围内的前沿Nu值低于零旋转参考值,但随着Ro从AR = 1、2的通道中的0.1和AR = 4的通道中的0.3开始增加而开始恢复。后沿的Nu / Nu_0比率随着Ro的增加而从单位一致地增加,但是它们对AR的增加的响应不如沿前沿的响应那么系统。通过本研究获得的扩展的Ro和Bu范围,以上发现为该技术界做出了最初的贡献。 AR = 1、2和4的旋转通道中的Nu / Nuo比分别落在0.6-2.2、0.5-2.7和0.5-2.1的范围内。导出一组传热相关性,以表示三个旋转管道的周期性展开的流动区域中的所有传热数据。

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