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Large eddy simulation of the near wake of a circular cylinder at sub-critical Reynolds number

机译:亚临界雷诺数下圆柱近尾迹的大涡模拟

摘要

This paper investigates the unsteady, near wake of a circular cylinder in cross flow at a Reynolds number of 5.5 x 10(3) using Large Eddy Simulation (LES). The near and intermediate wake velocity fields and unsteady aerodynamic forces compare well against available experimental data. Flow visualisation results show the presence of intermittent Kelvin Helmholtz (KH) instabilities in the very near wake. An empirical relation is presented for the spanwise length scales associated with KH instability that compares favourably with LES data. A wavelet analysis technique is used to investigate the frequency content of near wake. This analysis shows the existence of vortex pairing and breakdown in the near wake, providing further evidence that the near wake shear layer behaves in a similar manner to a mixing layer.
机译:本文使用大涡模拟(LES)来研究横流中圆柱的非稳态,近尾流,其雷诺数为5.5 x 10(3)。接近和中等的尾流速度场以及不稳定的空气动力与现有的实验数据进行了很好的比较。流动可视化结果表明,在非常近的尾流中存在间歇性的Kelvin Helmholtz(KH)不稳定性。提出了与KH不稳定性相关的跨度长度尺度的经验关系,该关系与LES数据具有可比性。小波分析技术用于研究近尾波的频率含量。该分析显示了近尾流中存在涡流对和分解,进一步证明了近尾流剪切层的行为与混合层相似。

著录项

  • 作者

    Doolan C.;

  • 作者单位
  • 年度 2010
  • 总页数
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类

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