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首页> 外文期刊>Journal of turbomachinery >Flowfield and Pressure Measurements in a Rotating Two-Pass Duct With Staggered Rounded Ribs Skewed 45 Degrees to the Flow
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Flowfield and Pressure Measurements in a Rotating Two-Pass Duct With Staggered Rounded Ribs Skewed 45 Degrees to the Flow

机译:旋转的两通管道中的流场和压力测量,其中交错的圆形肋与流量成45度角

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摘要

Laser-Doppler velocimetry and pressure measurements are presented of the local velocity and wall pressure distributions in a rotating two-pass square duct with staggered ribs placed on the leading and trailing walls at an angle of 45 deg to the main stream. The ribs were square in cross section with the radii of rounds and fillets to rib height ratios of 0.33. The rib-height/duct-height ratio and the pitch/rib-height ratio were 0.136 and 10, respectively. The duct Reynolds number was 1×10{sup}4 and rotation number Ro ranged from 0 to 0.2. Results are documented in terms of the evolutions of both main flow and cross-stream secondary flow, the distributions of the pressure coefficient, and the variation of friction factor with Ro. For CFD reference, the periodic fully developed flow condition is absent for the present length of the rotating passage roughened with staggered 45 deg ribs. In addition, the relationships between the regional averaged Nusselt number, transverse and convective mean velocity component, and turbulent kinetic energy are addressed. Using these relationships the general superiority of heat transfer enhancement of the staggered 45 deg ribs arrangement over the in-line one can be reasonably illustrated. Simple expressions are obtained to correlate the friction factor with Ro, which are lacking in the published literature for passages ribbed with staggered 45 deg ribs. The staggered 45 deg ribs are found to reduce the friction loss to about 88%±1% of the in-line 45 deg ribs for the rotating passage under the same operating conditions. The respective contributions of the angled ribs and passage rotation on the passage friction loss are identified.
机译:激光多普勒测速和压力测量结果显示了旋转的两遍方管中的局部速度和壁面压力分布,方管与主壁成45度角,在前壁和后壁上有交错的肋骨。肋的横截面为正方形,圆角和圆角与肋的高度比为0.33。肋骨高度/导管高度比和间距/肋骨高度比分别为0.136和10。管道雷诺数为1×10 {sup} 4,旋转数Ro在0至0.2的范围内。根据主流和横流次级流的演变,压力系数的分布以及摩擦系数随Ro的变化来记录结果。对于CFD参考,对于目前的交错交错的45度肋粗糙化的旋转通道,目前没有周期性的充分发展的流动条件。另外,解决了区域平均努塞尔数,横向和对流平均速度分量以及湍动能之间的关系。使用这些关系,可以合理地说明交错的45度肋排布置比直排布置的传热增强的总体优势。获得简单的表达式以将摩擦系数与Ro关联起来,而在已发表的文献中对于带有交错的45度肋肋的通道则缺乏这种表达式。发现在相同的操作条件下,交错的45度肋将旋转通道的直列45度肋的摩擦损失降低至大约88%±1%。确定了成角度的肋和通道旋转对通道摩擦损失的各自贡献。

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