THE FLUCTUATING VELOCITY FIELD ABOVE THE FREE END OF A SURFACEMOUNTED FINITE-HEIGHT SQUARE PRISM

R. Chakravarty, N. Rostamy, D. Bergstrom, D. Sumner
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Abstract

This study investigates the features of the fluctuating velocity field above the free end of a surface-mounted finite-height square prism, at a Reynolds number of Re = 4.2×10, using two state-of-the-art post-processing methodologies, namely Proper Orthogonal Decomposition (POD) and the swirling strength criterion. Instantaneous velocity measurements were obtained from Particle Image Velocimetry (PIV) experiments conducted in a low-speed wind tunnel for the flow over finite square prisms of aspect ratios AR = 9, 7, 5 and 3 (AR = H/D where H is the prism height and D is the prism width). The prisms were immersed in a thin, turbulent boundary layer with a dimensionless thickness of δ/D = 1.6. The Reynolds number based on the freestream velocity U∞ was Re = 4.2×10. POD modes were used to extract the dominant flow features, which revealed a pair of shear sub-layers above the free end, flow entrainment from the freestream above, as well as several vortex structures in the mean shear flow region. At lower aspect ratios, the shear layers become more pronounced. Combined with the swirling strength results, this represents evidence of Kelvin-Helmholtz instabilities within the shear layer region. These instabilities increase moving away from the vertical symmetry plane. Some structures in the near wake above and behind the prism trailing edge are also seen due to the interactions of the reverse flow downstream with the downwash flow.
面装有限高方棱镜自由端上的波动速度场
在雷诺数Re = 4.2×10的条件下,采用两种最先进的后处理方法,即适当正交分解(POD)和旋流强度准则,研究了表面安装的有限高度方形棱镜自由端上方波动速度场的特征。通过在低速风洞中进行的粒子图像测速(PIV)实验,获得了长径比为AR = 9,7,5和3 (AR = H/D,其中H为棱镜高度,D为棱镜宽度)的有限方棱镜上的瞬时速度。棱镜浸泡在无量纲厚度为δ/D = 1.6的薄湍流边界层中。基于自由流速度U∞的雷诺数Re = 4.2×10。利用POD模态提取优势流动特征,发现自由端上方存在一对剪切子层,自由端上方有自由流夹带,平均剪切流区存在多个涡旋结构。在较低的纵横比下,剪切层变得更加明显。结合旋流强度结果,这代表了剪切层区域内开尔文-亥姆霍兹不稳定性的证据。远离垂直对称面,这些不稳定性会增加。由于下游逆流与下洗流的相互作用,在棱镜尾缘前后的近尾迹中也可以看到一些结构。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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