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Computation of heat transfer in turbine rotor blade cooling channels with angled rib turbulators

机译:带有角肋湍流器的涡轮转子叶片冷却通道中的传热计算

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摘要

The effects of rotation and Reynolds number on heat transfer in rotating two-pass square and rectangular channels with smooth walls and walls with 45 degree angled and V-shaped rib turbulators were investigated numerically using an unstructured, incompressible, Reynolds-averaged Navier-Stokes flow solver. The influence of 45 degree angled ribs and channel orientation on the local Nusselt number ratios for leading and trailing surfaces in a two-pass square channel (AR=1) are compared to experimental data for Reynolds numbers from 5,000 to 25,000 and dimensionless rotation numbers from 0.0 to 0.118. The influence of V-shaped ribs and channel orientation on the local Nusselt number ratios for leading and trailing surfaces in a two-pass rectangular channel (AR=2) are compared to experimental data for Reynolds numbers from 5,000 to 40,000 and rotation numbers from 0.0 to 0.210. It is concluded that rotation causes significant changes to the local Nusselt number ratio distribution relative to stationary conditions. Generally, the first pass trailing and second pass leading surfaces have increased local Nusselt number ratios due to the secondary ow impingement induced by rotation. Alternatively, the first pass leading and second pass trailing surface Nusselt number ratios tend to decrease with increased rotation.
机译:使用非结构化,不可压缩,雷诺数均值的Navier-Stokes流,数值研究了旋转和雷诺数对旋转的两通道方形和矩形通道(具有光滑壁和带有45度角的V型肋湍流器)的传热的影响。解算器。将45度成角度的肋骨和通道方向对两通道方通道(AR = 1)中前后表面局部Nusselt数比的影响与5,000至25,000的雷诺数和5,000的无因次旋转数的实验数据进行了比较0.0至0.118。将V型肋和通道方向对两遍矩形通道(AR = 2)中前后表面局部Nusselt数比的影响与5,000至40,000的雷诺数和0.0的旋转数的实验数据进行了比较到0.210。可以得出结论,相对于静止状态,旋转会导致局部Nusselt数比分布发生显着变化。通常,由于旋转引起的二次流冲击,第一遍尾随表面和第二遍前导表面具有增加的局部努塞尔特数比。可替代地,第一遍前导表面和第二遍后表面努塞尔数比率倾向于随着旋转的增加而减小。

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    Flynt Guy Austin;

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  • 年度 2013
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  • 正文语种 English
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