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Computation of Heat Transfer in Turbine Rotor Blade Cooling Channels with Angled Rib Turbulators

机译:涡轮转子叶片冷却通道中传热的计算与成角度肋湍流器

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The effects of rotation and Reynolds number on heat transfer in rotating two-pass square and rectangular channels with angled rib turbulators were investigated numerically using an incompressible, Reynolds-averaged Navier-Stokes flow solver. The influence of 45° angled ribs and channel orientation on local Nusselt number ratios in a two-pass square channel (AR=1) are compared to experimental data for Reynolds numbers from 5,000 to 25,000 and rotation numbers from 0.0 to 0.118. The influence of Ⅴ-shaped ribs and channel orientation on local Nusselt number ratios in a two-pass rectangular channel (AR=2) are investigated for Reynolds numbers from 10,000 to 40,000 and rotation numbers from 0.0 to 0.105. 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 flow 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:旋转和雷诺数的传热在旋转的影响具有成角度的肋湍流器进行了数值使用不可压缩的,雷诺平均纳维 - 斯托克斯求解流动调查两遍正方形和长方形通道。 45°角的肋和通道的取向对本地努塞尔数比率的影响的两遍平方信道(AR = 1)进行比较,以从5000至25000的实验数据为雷诺数和转数从0.0至0.118。 Ⅴ型肋和通道的取向对本地努塞尔数的比率在两通矩形通道的影响(AR = 2)研究了雷诺数为10,000至40,000转数从0.0至0.105。可以得出结论,旋转导致局部努塞尔数比分布相对于固定条件显著变化。通常,第一通后缘和第二遍前表面具有增加的本地努塞尔数的比率由于旋转所引起的二次流冲击。可替代地,第一遍导致和第二遍后表面努塞尔数的比率倾向于具有增加的旋转降低。

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