首页> 外文学位 >Jet noise of high aspect-ratio rectangular nozzles with application to pneumatic high-lift devices.
【24h】

Jet noise of high aspect-ratio rectangular nozzles with application to pneumatic high-lift devices.

机译:高纵横比矩形喷嘴的喷射噪声应用于气动高升力设备。

获取原文
获取原文并翻译 | 示例

摘要

Circulation control wings are a type of pneumatic high-lift device that have been extensively researched as to their aerodynamic benefits. However, there has been little research into the possible airframe noise reduction benefits.{09}The key element of noise is the jet noise associated with the jet sheet emitted from the blowing slot. This jet sheet is essentially a high aspect-ratio rectangular jet.; This study directly compared far-field noise emissions from a state-of-the-art circulation control wing high lift configuration, and a conventional wing also configured for high lift. Results indicated that a circulation control wing had a significant acoustic advantage over a conventional wing for identical lift performance. A high aspect-ratio nozzle was fabricated to study the general characteristics of high aspect-ratio jets with aspect ratios from 100 to 3000. The results of this study provided the basic elements in understanding how to reduce the noise from a circulation control wing.; High aspect-ratio nozzle results showed that the jet noise of this type of jet was proportional to the 8th power of the jet velocity. It was also found that the jet noise was proportional to the slot height to the 3/2 power and slot width to the 1/2 power. Fluid dynamic experiments were also performed on the high aspect-ratio nozzle. Single hot-wire experiments indicated that the jet exhaust from the high aspect-ratio nozzle was similar to a 2-d turbulent jet. Two-wire space-correlation experiments were performed to attempt to find a relationship between the slot height of the jet and the length-scale of the flow noise generating turbulence structure. The turbulent eddy convection velocity was also calculated, and was found to vary with the local centerline velocity, and also as a function of the frequency of the eddy.
机译:循环控制机翼是一种气动高升力装置,已对其空气动力学优势进行了广泛研究。但是,几乎没有关于降低机身噪音的好处的研究。{09}噪音的关键因素是与从吹气槽中喷出的喷气片相关的喷气噪声。该射流片实质上是高纵横比的矩形射流。这项研究直接比较了最先进的循环控制机翼高升力配置和常规机翼也配置为高升力的远场噪声排放。结果表明,对于相同的升力性能,循环控制机翼比常规机翼具有明显的声学优势。制造高纵横比喷嘴以研究纵横比从100到3000的高纵横比射流的一般特性。这项研究的结果为理解如何减少循环控制机翼的噪声提供了基本要素。高长宽比喷嘴结果表明,这种类型的射流的射流噪声与射流速度的八次幂成正比。还发现喷射噪声与缝隙高度与3/2幂成正比,与缝隙宽度与1/2幂成正比。在高纵横比喷嘴上也进行了流体动力学实验。单个热线实验表明,高纵横比喷嘴的喷射流与二维湍流喷射流相似。进行了两线空间相关性实验,以试图找到射流的狭缝高度与产生流动噪声的湍流结构的长度尺度之间的关系。还计算了湍流涡流对流速度,发现该湍流对流速度随局部中心线速度变化,并且还随涡流频率而变化。

著录项

  • 作者

    Munro, Scott Edward.;

  • 作者单位

    Georgia Institute of Technology.;

  • 授予单位 Georgia Institute of Technology.;
  • 学科 Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 2002
  • 页码 360 p.
  • 总页数 360
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空、航天技术的研究与探索;
  • 关键词

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号