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Influence of aspect ratio on the mean flow field of a surface-mounted finite-height square prism

机译:长宽比对表面安装有限高方棱镜平均流场的影响

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摘要

The flow around surface-mounted, finite-height square prisms at a Reynolds number of Re=4.2 x 10(4) was investigated experimentally in a low-speed wind tunnel using particle image velocimetry. The thickness of the boundary layer on the ground plane relative to the width of the prism was delta/D = 1.5. Four prism aspect ratios were tested, AR = 9, 7, 5, and 3, to study how the aspect ratio influences the flow field close to the prism. Upstream of the prism, lowering the aspect ratio from AR = 9 to AR = 3 causes the stagnation point on the upstream face to move closer to the free end, but there is no influence on the location and strength of the horseshoe vortex. Lowering the aspect ratio from AR = 9 to AR = 3 causes the cross-stream vortices in the upper and lower halves of the wake to move downstream and upstream, respectively; the latter vortex is absent for AR = 3, suggesting this prism sits below the critical aspect ratio. Above the free end of the prism, within the region of separated flow, lowering the aspect ratio from AR = 9 to AR = 3 shifts the location of the cross-stream vortex farther downstream. For the prism of AR = 3, reverse flow above the free end is stronger yet more unsteady compared to the more slender prisms, while the streamwise edge vortices are smaller and weaker. (C) 2017 Elsevier Inc. All rights reserved.
机译:雷诺数为Re = 4.2 x 10(4)时,表面安装的有限高度方形棱镜周围的流动是在低速风洞中使用粒子图像测速技术进行实验研究的。相对于棱镜的宽度,地平面上边界层的厚度为Δ/ D = 1.5。测试了四个棱镜长宽比,AR = 9、7、5和3,以研究长宽比如何影响靠近棱镜的流场。在棱镜的上游,将纵横比从AR = 9降低到AR = 3会导致上游面上的停滞点移近自由端,但对马蹄涡旋的位置和强度没有影响。将宽高比从AR = 9降低到AR = 3会导致尾流的上半部和下半部的横流涡流分别向下游和上游移动; AR = 3时不存在后一个涡旋,这表明该棱镜位于临界纵横比以下。在棱镜的自由端上方,在分流区域内,将宽高比从AR = 9降低到AR = 3,可将横流涡流的位置向更下游移动。对于AR = 3的棱镜,与细长的棱镜相比,自由端上方的逆流更强,但不稳定,而沿流方向的涡旋更小且更弱。 (C)2017 Elsevier Inc.保留所有权利。

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