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Cavitation and wake structure of unsteady tip vortex flows.

机译:不稳定涡旋流的空化和尾流结构。

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摘要

nsteady flows are prevalent in virtually every fluid application yet, because of their intrinsic complexity, few attempts have been made to measure them or explain their behavior. This thesis presents an experimental study of one of the simplest unsteady flow induced effects, the periodic change in angle of attack of a lifting surface. Of particular interest is the influence this effect has on the tip vortex structure of a finite aspect ratio hydrofoil and the part it plays in the inception of cavitation.;An aspect ratio 2.3 hydrofoil was reflection-plane mounted to the test section floor of the Caltech Low Turbulence Water Tunnel and harmonically oscillated in pitch near its center of pressure. Observations of the growth and collapse of surface and tip vortex cavitation were made along with detailed observations of the interaction of the tip vortex formation with the spanwise wake structure. Measurements of the cavitation inception number for surface cavitation and tip vortex cavitation were made relative to the phase of the hydrofoil and the reduced frequency, k =
机译:不稳定的流动几乎在每个流体应用中都很普遍,但是由于其固有的复杂性,很少尝试测量它们或解释其行为。本文提出了一种最简单的非稳态流动诱发效应的实验研究,即提升面的迎角周期性变化。特别令人感兴趣的是,这种影响对有限长宽比水翼的尖端涡旋结构及其在空化开始时所起的作用的影响。长宽比2.3水翼被安装在加州理工学院测试断面的反射平面上低湍流水洞,在其压力中心附近以螺距谐调振动。观察了表面和尖端涡流空化的生长和坍塌,并详细观察了尖端涡流形成与翼展方向尾流结构的相互作用。相对于水翼的相位和降低的频率,测量了表面空化和尖端涡旋空化的空化起始数。

著录项

  • 作者

    Hart, Douglas Payton.;

  • 作者单位

    California Institute of Technology.;

  • 授予单位 California Institute of Technology.;
  • 学科 Ocean engineering.;Plasma physics.;Aerospace engineering.
  • 学位 Ph.D.
  • 年度 1993
  • 页码 250 p.
  • 总页数 250
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

  • 入库时间 2022-08-17 11:50:00

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