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Bio-Inspired Control of Roughness and Trailing Edge Noise

机译:生物启发性的粗糙度和后缘噪声控制

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摘要

Noise from fluid flow over rough surfaces is an important consideration in the design and performance of certain vehicles with high surface-area-to-perimeter ratios. A new method of noise control based on the anatomy of owls is developed and consists of fabric or fibrous canopies suspended above the surface. The method is tested experimentally and is found to reduce the total far-field noise emitted by the surface. The treatment also is found to reduce the magnitude of pressure fluctuations felt by the underlying surface by up to three orders of magnitude. Experimental investigations into the effects of geometric parameters of the canopies lead to an optimized design which maximizes noise reduction.;The results obtained during the canopy experiment inspired a separate new device for the reduction of trailing edge noise. This type of noise is generated by flow past the wing of an aircraft or the blades of a wind turbine, and is a source of annoyance for those in surrounding communities. The newly developed treatment consists of small fins, or "finlets," placed near the trailing edge of an airfoil. The treatment is tested experimentally at near-full-scale conditions and is found to reduce the magnitude of far-field noise by up to 10 dB. Geometric parameters of the finlets are tested to determine the optimal size and spacing of the finlets to maximize noise reduction. Follow-up computational and experimental studies reveal the fluid mechanics behind the noise reduction by showing that the finlets produce a velocity deficit in the flow near the trailing edge and limit the magnitude and spanwise correlation lengthscale of turbulence near the trailing edge, factors which determine the magnitude of far-field noise.;In a final experiment, the finlets are applied to a marine propeller and are found to reduce not only trailing edge noise, but also noise caused by the bluntness of the trailing edge. The results of this experiment show the potential usefulness of finlets to reduce noise from rotating systems, such as fans or propellers, as well as from structures which feature blunt trailing edges.
机译:在某些具有高表面积与周长比的车辆的设计和性能中,来自流体流经粗糙表面的噪声是重要的考虑因素。开发了一种基于猫头鹰解剖学的噪声控制新方法,该方法由悬浮在表面上方的织物或纤维蓬蓬组成。该方法经过实验测试,发现可以减少表面发出的总远场噪声。还发现该处理将下层表面感觉到的压力波动的幅度减小了三个数量级。通过对顶篷几何参数的影响进行实验研究,得出了一种优化设计,该设计可以最大程度地降低噪声。在顶篷实验过程中获得的结果启发了一种单独的新设备来降低后缘噪声。这种噪声是由流过飞机机翼或风力涡轮机叶片的气流产生的,并且是周围社区居民的烦恼之源。新开发的处理方法是在翼型后缘附近放置小鳍或“鳍”。该处理在接近满量程的条件下进行了实验测试,发现可以将远场噪声的大小降低多达10 dB。测试散热片的几何参数,以确定散热片的最佳尺寸和间距,以最大程度地降低噪音。后续的计算和实验研究表明,翼片在后缘附近产生了速度缺陷,并限制了后缘附近湍流的大小和展向相关长度尺度,从而揭示了降噪背后的流体力学。在最后的实验中,将小片应用于船用螺旋桨,不仅降低了后缘噪声,而且还降低了由后缘钝性引起的噪声。该实验的结果表明,小片对减少旋转系统(例如风扇或螺旋桨)以及后钝角结构产生的噪声的潜在实用性。

著录项

  • 作者

    Clark, Ian Andrew.;

  • 作者单位

    Virginia Polytechnic Institute and State University.;

  • 授予单位 Virginia Polytechnic Institute and State University.;
  • 学科 Aerospace engineering.
  • 学位 Ph.D.
  • 年度 2017
  • 页码 135 p.
  • 总页数 135
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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