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Heat Transfer in Smooth and Ribbed Rectangular Two-Pass Channels with a Developing Flow Entrance at High Rotation Numbers

机译:在具有高旋转数的流动入口不断发展的光滑且带肋的矩形两通通道中的传热

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摘要

Cooling channels with a developing flow entrance condition and aspect ratios of1:4 and 2:1 were studied. The range of the rotation number and buoyancy parameter forthe selected AR channels was extended. The maximum Ro and Bo for the 1:4 channelwas 0.67 and 1.9, respectively. For the 2:1 channel, these values were 0.45 and 0.85,respectively.The effect of rib spacing and rib height on heat transfer in the 1:4 channel isinvestigated. Three rib spacing configurations were considered: P/e=2.5, 5, 10 with aconstant e/Dh ratio of 0.078. To investigate the effect of rib height, a rib configurationwith an e/Dh ratio of 0.156 and P/e ratio of 10 was considered. For the 2:1 channel, asmooth channel surface condition was studied. For each channel aspect ratio and surfacecondition, five Reynolds numbers were studied up to 40K. At each Re, five rotationalspeeds are considered up to 400 rpm.The results of this research work indicate that rotation can cause a significantincrease in heat transfer on the first pass trailing surface of both aspect ratio channels. The leading surface in ribbed channels has shown a dramatic decrease in heat transferwith rotation in the first pass. Reductions in heat transfer by as much as 50% wereobserved. In the second pass, the leading and trailing surfaces with ribs showed verysimilar effects of rotation. Also, the effect of rotation seems to vary with the rib spacing.The strength of rotation showed to be greater in the tight rib spacing of P/e=2.5. The ribheight in the 1:4 channel had minimal impact due to the large distance between theleading and trailing surfaces. The tip cap heat transfer for both channels showed largeincreases with rotation. This is very beneficial since tip cooling is an important part ofmaintaining the life a turbine blade. Finally, the buoyancy parameter proved to be veryuseful in predicting heat transfer in rotating conditions. The correlations developedshowed very acceptable accuracy when compared to the experimental data.
机译:研究了流动通道进入条件和长宽比分别为1:4和2:1的冷却通道。扩展了所选AR通道的转数和浮力参数的范围。 1:4通道的最大Ro和Bo分别为0.67和1.9。对于2:1通道,这些值分别为0.45和0.85。研究了肋间距和肋高对1:4通道传热的影响。考虑了三种肋骨间距配置:P / e = 2.5、5、10,恒定e / Dh比为0.078。为了研究肋骨高度的影响,考虑了e / Dh比为0.156和P / e比为10的肋骨结构。对于2:1通道,研究了光滑通道的表面状况。对于每个通道的纵横比和表面条件,研究了40K以下的五个雷诺数。在每个Re处,五个旋转速度被认为高达400 rpm。这项研究工作的结果表明,旋转会导致两个长宽比通道的第一遍尾随表面的传热显着增加。带肋通道中的前导表面在第一遍中显示出随着旋转的传热显着减少。观察到传热减少了多达50%。在第二遍中,带有肋的前,后表面显示出非常相似的旋转效果。同样,旋转的影响似乎随肋骨间距而变化。在P / e = 2.5的紧密肋骨间距中,旋转强度显示出更大的强度。由于前后表面之间的距离较大,因此1:4通道中的肋高影响最小。两个通道的顶盖传热均显示旋转增加。这是非常有益的,因为尖端冷却是维持涡轮机叶片寿命的重要部分。最后,浮力参数被证明对于预测旋转条件下的传热非常有用。与实验数据相比,相关性显示出非常可接受的准确性。

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    Huh Michael;

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  • 年度 2010
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