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The turbulent wake of a submarine model in pitch and yaw.

机译:潜艇模型在俯仰和偏航中的湍流尾流。

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This thesis aims to further our understanding of high Reynolds number wakes of submarine-like bodies of revolution. These wake measurements are preceded by an investigation of the limitations of the hot wire anemometry technique that is extensively used in this thesis to measure the velocity field.;To study spatial filtering, measurements of the turbulence statistics and spectra downstream of a grid were performed using hot-wires of varying length and compared to the results from a new nano-scale thermal anemometry probe. The effect of spatial filtering on the streamwise spectrum function is observed to extend to almost all wavenumbers, even those significantly lower than the length of the hot wire itself. A criterion is found that must be satisfied in order to avoid the effects of spatial filtering on the turbulence statistics as well as on the spectrum. End conduction effects are investigated numerically and validated experimentally using grid turbulence. A new end-conduction parameter takes into account the effects due to hot wire material, overheat ratio and Reynolds number. We suggest a numerical criterion for the new end-conduction parameter that is necessary to avoid any attenuation in the turbulent fluctuations.;Detailed velocity measurements were then performed using hot wire anemometry and stereoscopic particle image velocimetry in the wake of a body of revolution shape (DARPA SUBOFF) at a Reynolds number of Re L = 2.4 x 106, for pitch and yaw angles up to 12°. These measurements reveal the formation of a pair of streamwise vortices in pitch and yaw that are asymmetric in strength, an unexpected result. In pitch the vortices rotate around each other as they evolve downstream, and they lose their strength by diffusion relatively quickly. In yaw the asymmetry is even more pronounced due to the influence of the sail. The weaker vortex quickly diffuses, and in the absence of further diffusion the stronger vortex maintains its strength even at the furthest downstream location. It appears that small asymmetries in the flow near the nose can result in strong asymmetries in the wake, a result previously only seen for sharp-nosed bodies at high angles of attack.
机译:本论文旨在进一步了解类似海底的旋转体的雷诺数高。在进行这些尾流测量之前,首先要研究热线风速测量技术的局限性,该技术在本文中被广泛用于测量速度场。为了研究空间滤波,使用了网格下游的湍流统计数据和光谱进行了测量。各种长度的热线,并与新型纳米级热风速计探针的结果进行比较。观察到空间滤波对沿流频谱函数的影响扩展到几乎所有波数,甚至那些远低于热线本身长度的波数。找到了必须满足的标准,以避免空间滤波对湍流统计数据和频谱的影响。对末端传导效应进行了数值研究,并使用网格湍流进行了实验验证。新的终端传导参数考虑了热线材料,过热率和雷诺数的影响。我们建议使用新的最终传导参数的数值标准,该数值标准是避免湍流波动中任何衰减所必需的;然后在旋转体之后使用热线风速仪和立体粒子图像测速仪进行了详细的速度测量(雷诺数Re L = 2.4 x 106时的DARPA SUBOFF),俯仰角和偏航角最大为12°。这些测量结果揭示了在螺距和偏航方向上形成了一对强度不对称的沿流方向的涡流,这是出乎意料的结果。在螺距中,涡旋随着它们向下游发展而绕彼此旋转,并且它们由于扩散而相对较快地失去了强度。在偏航中,由于风帆的影响,不对称性更加明显。较弱的涡旋迅速扩散,并且在没有进一步扩散的情况下,较强的涡旋即使在最远的下游位置也能保持其强度。看起来,鼻子附近流中的较小不对称性可能会导致尾流中出现强烈的不对称性,这种结果以前仅在高攻角的尖锐物体上可见。

著录项

  • 作者

    Ashok, Anand.;

  • 作者单位

    Princeton University.;

  • 授予单位 Princeton University.;
  • 学科 Mechanical engineering.;Aerospace engineering.
  • 学位 Ph.D.
  • 年度 2014
  • 页码 187 p.
  • 总页数 187
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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