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Mass/Heat Transfer in a Ribbed Passage With Cylindrical Vortex Generators: The Effect of Generator-Rib Spacing

机译:圆柱涡流发生器在肋状通道中传质/传热:发生器-肋间距的影响

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摘要

The effect of vortex generators on the heat transfer from internally ribbed passages is studied experimentally using a mass transfer technique. Cylindrical vortex generators placed directly above the ribs have been used in this study. Results are reported on the effect of the spacing between the vortex generator and the ribs. Detailed distributions of the Sherwood number contours and the centerline Sherwood number distributions are presented. Reynolds number values of 5000, 10,000, and 30,000 are studied and three generator-rib-spacing-rib-height (s/e) values of 0.55, 1, and 1.5 are considered. It is shown that at small generator-rib spacings (s/e=0.55), the two act as a single element, and lead to a retardation of the shear layer development past the reattachment point. This is generally associated with lower heat transfer. At a larger generator-rib spacing (s/e =1.5), the generator wake and the rib shear layer interact with each other to promote mixing and heat transfer.
机译:使用传质技术实验研究了涡流发生器对内部肋状通道传热的影响。直接在肋骨上方放置的圆柱形涡流发生器已用于本研究中。报告了涡流发生器和肋之间的间距的影响的结果。给出了舍伍德数轮廓和中心线舍伍德数分布的详细分布。研究了雷诺数的值分别为5000、10,000和30,000,并考虑了三个发电机-肋-间隔-肋-高度(s / e)值为0.55、1和1.5。结果表明,在较小的发电机-肋骨间距(s / e = 0.55)下,两者作为一个单元起作用,并导致剪力层发展滞后于重新连接点。这通常与较低的热传递有关。在较大的发电机肋间距(s / e = 1.5)下,发电机尾流和肋骨剪切层相互影响,以促进混合和传热。

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