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Vortex Formation and Shedding in the Wake of Surface-Mounted Finite Aspect-Ratio Square Cylinders.

机译:表面安装的有限长宽比方形圆柱的尾流中涡的形成和脱落。

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摘要

Bluff-body vortex shedding with focus on the turbulent wake of finite surface-mounted square cylinders at moderate Reynolds numbers is studied experimentally using particle image velocimetry (PIV) and hotwire anemometry (HWA). Emphasis is put on understanding the formation and growth process of vortices, their interaction and separation from the feeding shear layer.;The conventionally described vortex shedding process is reassessed. It is concluded that contrary to the traditionally proposed mechanism, the mutual interaction between counter-rotating vortices is not the cause for the limit to vortex growth. Rather, the vortex growth is naturally limited and the feedback from the shed vortices serves to lock-in the shedding frequency. Furthermore, based on observation of the shedding of an isolated two-dimensional vortex, a length scale defined as the distance between the shear-layer edge and vortex center at the streamwise location of maximum vortex circulation is shown to result in a collapse of nondimensional circulation. On the ground of scaling principles, this scale is shown to also result in a collapse of the shedding frequency.;This work also resolves an apparent discrepancy in the literature with respect to the existence of symmetric and anti-symmetric shedding regimes. Using spatial cross-correlation, instantaneous phase relationships, and phase-averaged velocity data obtained from PIV and HWA, it is shown that the shedding in the wake of surface-mounted finite square cylinders is predominantly anti-symmetric and thus consistent with the von Karman process. What had been interpreted as symmetric shedding appears to be a distortion of the regular shedding process. During periods of low-amplitude fluctuations, two counter-rotating vortices exist concurrently in the base region. However, counter-rotating vortices are still shed alternately.
机译:使用粒子图像测速仪(PIV)和热线风速仪(HWA),通过实验研究了在中等雷诺数下集中于有限表面安装方形圆柱体的湍流尾流的钝体涡旋脱落。重点在于理解涡流的形成和生长过程,它们与进料剪切层的相互作用和分离。;重新评估了常规描述的涡流脱落过程。可以得出结论,与传统机制相反,反向旋转涡流之间的相互影响并不是限制涡流增长的原因。而是,涡流的增长自然受到限制,而来自脱落涡流的反馈可用于锁定脱落频率。此外,基于对孤立的二维涡旋脱落的观察,长度尺度定义为最大涡旋流的流向位置处的剪切层边缘与涡旋中心之间的距离,从而导致无量纲环流崩溃。根据比例缩放原理,该比例也显示出导致脱落频率的下降。这项工作还解决了文献中关于对称和反对称脱落机制存在的明显差异。使用空间互相关,瞬时相位关系以及从PIV和HWA获得的相位平均速度数据,表明表面安装的有限方形圆柱体的尾流主要是反对称的,因此与von Karman一致处理。被解释为对称脱落的现象似乎是对常规脱落过程的一种扭曲。在低幅度波动期间,基本区域中同时存在两个反向旋转的涡流。但是,反向旋转的涡流仍然交替出现。

著录项

  • 作者

    Sattari, Pooria.;

  • 作者单位

    University of Calgary (Canada).;

  • 授予单位 University of Calgary (Canada).;
  • 学科 Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 2013
  • 页码 207 p.
  • 总页数 207
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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