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Cavity flow control using a rod in cross flow.

机译:使用横流中的杆进行腔体流量控制。

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摘要

For a variety of aerodynamic conditions and geometric configurations fluid structure interactions give rise to a reverberant field. This phenomenon, referred to as resonant acoustics, has practical importance due to its undesirable effects such as noise, structural loading, and unsteady flow field. Several flow control technologies exist but they lose efficacy at off-design conditions. With the focus on expanding their operating envelope, the present work investigates the physics of the flow control using a combination of detailed experimental measurements and theoretical analysis. The model resonant acoustic flow problem that we chose for our study is cavity tones, i.e., the high intensity acoustic tones produced by high speed air moving over rectangular cavity. The flow control actuator is a rod in cross flow, i.e., a thin horizontal rod placed upstream of the cavity.;In the present work, a detailed experimental study has been undertaken to characterize the acoustics, mean velocity field as well as the pressure perturbation field both inside and outside of the cavity. Control cases with contrasting suppression results are chosen to illustrate important aspects of the mean flow field. To investigate whether the cylinder, through its wake, changes the stability characteristics of the shear layer that develops over the cavity, stability analysis of the shear layer is undertaken. First, stability of artificial velocity profiles that are prototypical of the experimentally measured velocity profiles is investigated; in order to determine what parameters of the velocity profiles influence the stability of the shear layer the most. Next stability of experimentally measured velocity profiles is evaluated to calculate integrated growth rates along the length of the cavity. Mean velocity data is also used to elucidate the shear layer lift off mechanism of the rod. Both integrated growth range and shear layer lift off data are compared with the acoustic suppression results. Based on the trends it appears that shear layer lift off, which interferes with the acoustic interaction between the shear layer and the trailing edge of the cavity, is the dominant mechanism by which the rod controls flow over the cavity.
机译:对于各种空气动力学条件和几何构型,流体结构相互作用产生了回响场。这种现象被称为共振声学,由于其不良影响,例如噪声,结构载荷和不稳定的流场,因此具有实际意义。存在几种流量控制技术,但是它们在非设计条件下会失去功效。着眼于扩大其工作范围,本工作结合详细的实验测量和理论分析,研究了流量控制的物理原理。我们为研究选择的模型共振声流问题是空腔音,即高速空气在矩形空腔上移动所产生的高强度声音。流量控制执行器是横流的杆,即位于空腔上游的细水平杆。在当前工作中,已进行了详细的实验研究,以表征声学,平均速度场以及压力扰动腔内外的磁场。选择具有相反抑制结果的控制案例来说明平均流场的重要方面。为了研究圆柱体是否通过其尾流改变了在型腔上形成的剪切层的稳定性特征,对剪切层进行了稳定性分析。首先,研究与实验测得的速度分布图典型的人工速度分布图的稳定性。为了确定速度曲线的哪些参数对剪切层的稳定性影响最大。评估实验测得的速度分布曲线的下一个稳定性,以计算沿腔体长度的整体增长率。平均速度数据也用于阐明杆的剪切层剥离机理。将完整的生长范围和剪切层剥离数据与声学抑制结果进行了比较。基于趋势,似乎剪切层剥离会干扰剪切层与腔体后缘之间的声学​​相互作用,这是控制杆在腔体上流动的主要机制。

著录项

  • 作者

    Sarpotdar, Shekhar.;

  • 作者单位

    Illinois Institute of Technology.;

  • 授予单位 Illinois Institute of Technology.;
  • 学科 Engineering Aerospace.;Physics Acoustics.
  • 学位 Ph.D.
  • 年度 2010
  • 页码 178 p.
  • 总页数 178
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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