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Drag and Flutter Characteristics of Loop Membranes

机译:环膜的阻力和颤动特性

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摘要

We present the results of experimental investigations on the aerodynamic characteristics of high-drag devices with flexible membranes joined at their short ends (loops). The loops were placed in a low-speed wind tunnel and tested at speeds up to 19 m/s. The range of Reynolds numbers was Re = 2 x 10~5 - 2 x 10~6. The loops were tested for a variety of aspect ratios, from 3.3 to 30, three planform areas, and two mounting methods. Results are presented for the drag coefficient and for the flutter characteristics. We prove that with a low aspect ratio the loops form a teardrop shape and their flutter mode is a sinusoidal-like oscillation. Furthermore, the drag coefficient decreases with the increasing wind speed, but it depends strongly on the aspect ratio and the planform area. Empirical correlations for the drag coefficient are polynomial equations.
机译:我们提出了对高阻力装置的空气动力学特性进行实验研究的结果,该装置在其短端(环)处连接有柔性膜。将环路放置在低速风洞中,并以高达19 m / s的速度进行测试。雷诺数的范围为Re = 2 x 10〜5-2 x 10〜6。对环进行了各种宽高比测试,范围从3.3到30,三个平面区域和两种安装方法。给出了阻力系数和颤振特性的结果。我们证明了,长宽比低时,环路会形成泪珠状,其颤动模式是正弦波状的振荡。此外,阻力系数随着风速的增加而减小,但是在很大程度上取决于纵横比和平面面积。阻力系数的经验相关性是多项式方程。

著录项

  • 来源
    《Journal of Aircraft》 |2007年第1期|p.317-322|共6页
  • 作者单位

    Flight Group, Department of Zoology, University of Oxford, South Parks Road, Oxford, OX1 3PS England, United Kingdom;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空;
  • 关键词

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