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TA Computational Investigation of Flow Structure Within a Sinuous Duct

机译:弯管内流动结构的TA计算研究

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In the present investigation the distribution of mean velocity are experimentally studied on three constant area rectangular curved ducts with an aspect ratio of 2.4. First one is C-shape, second one is S-shape and third one is a DS-shape duct. The experiment is carried out at mass averaged mean velocity of 40m/s for all the ducts. The velocity distribution shows for C-duct, the bulk flow shifting from outer wall to the inner wall along the flow passage and for S-duct, the bulk flow shifting from outer wall to the inner wall in the first half and from inner wall to the outer wall in the second half along the flow passage of curved ducts are very instinct. Due to the imbalance of centrifugal force and radial pressure gradient, secondary motions in the forms of counter rotating vortices have been generated within both the curved duct. For DS-duct the velocity distributions shows the Bulk of flow shifting from inner watt to outer wall in the first bend and third bend of the duct and outer wall to inner wall in the second bend and forth bend of the duct along the flow passage is very instinct. Flow at end of the DS-duct is purely uniform in nature due to non existence of secondary motion. The experimental results then were numerically validated with the help of Fluent, which shows a good agreement between the experimental and predicted results for all the ducts
机译:在本研究中,通过实验研究了三个长宽比为2.4的恒定面积矩形弯曲管道的平均速度分布。第一个是C形,第二个是S形,第三个是DS形风管。对于所有管道,均以质量平均速度40m / s进行实验。速度分布表明,对于C型管道,总流量沿流动通道从外壁向内壁转移;对于S型管道,总流量在上半部分从外壁向内壁转移,从内壁向后半部分的外壁沿弯曲管道的流动通道非常直觉。由于离心力和径向压力梯度的不平衡,两个弯曲管道内都产生了反向旋转涡流形式的次级运动。对于DS-管道,速度分布表明,在管道的第一弯和第三弯中,大流量从内瓦向外壁转移,在第二弯和第二弯时,外壁向内壁沿流动通道转移。非常本能。由于不存在次级运动,DS管道末端的流动本质上是纯均匀的。然后在Fluent的帮助下对实验结果进行了数值验证,这表明所有管道的实验结果与预测结果之间都具有很好的一致性

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