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POD Analysis in the Wake of Wall-Mounted Cylinders

机译:壁挂式气缸唤醒后的POD分析

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The flow patterns over a finite square cylinder of aspect ratio H/d = 3 were analyzed experimentally. The measurements were carried out in a subsonic wind tunnel using the technique of Time Resolved Particle Image Velocimetry (TR-PIV). The near wake flow structures and vortex shedding characteristics were investigated using instant velocity maps and proper orthogonal decomposition (POD). Tests were performed at a speed of 20m/s, resulting in Re - 65300, with the cylinder facing the flow at 90°. For the wind tunnel tests, the cylinders were fixed on flat plate, creating a boundary layer which interacted with the cylinder wake. The 2D PIV measurements were conducted at three horizontal planes (z/H = 0.3, z/H = 0.5, z/H = 1) and the symmetry x-z plane. Due to the complexity of the phenomena, the flow was characterized both in terms of average behavior and time-resolved velocity fields. Both symmetrical and anti-symmetrical vortices structures occur in the cylinder wake, which can be identified based on the coefficients of the first four POD modes. The results indicated that the alternating Karman vortex structures are dominant, described by the two first POD modes. However, this structure is sometimes suppressed, leading to periods of symmetrical vortex shedding.
机译:实验分析了纵横比为H / d = 3的有限方圆柱体上的流动模式。使用时间分辨粒子图像测速技术(TR-PIV)在亚音速风洞中进行测量。使用即时速度图和适当的正交分解(POD)研究了近尾流的结构和涡旋脱落特性。以20m / s的速度进行测试,得到Re-65300,圆柱体面向流动方向为90°。对于风洞测试,将气瓶固定在平板上,形成与气瓶尾流相互作用的边界层。在三个水平面(z / H = 0.3,z / H = 0.5,z / H = 1)和对称x-z平面上进行2D PIV测量。由于现象的复杂性,在平均行为和时间分辨速度场方面都对流动进行了表征。对称涡流结构和反对称涡流结构都出现在圆柱尾流中,可以根据前四个POD模式的系数进行识别。结果表明,交替的卡曼涡旋结构是主要的,由两个第一个POD模式描述。但是,这种结构有时会受到抑制,从而导致对称涡旋脱落的时期。

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