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Numerical Simulations of Three-Dimensional Instabilities in Cavity Flows.

机译:空腔流动中三维不稳定性的数值模拟。

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摘要

Direct numerical simulations are performed to investigate the stability of compressible flow over three-dimensional open cavities for future control applications.;First, the typical self-sustained oscillations, commonly referred as shear-layer (Rossiter) modes, are characterized for two-dimensional cavities over a range of flow conditions. A linear stability analysis is then conducted to search for three-dimensional global instabilities of the 2D mean flow for cavities that are homogeneous in the spanwise direction. The presence of such instabilities is reported for a range of cavity configurations. For cavities of aspect ratio (length to depth) of 2 and 4, the three-dimensional mode has a spanwise wavelength of approximately 1 cavity depth and oscillates with a frequency about an order-of-magnitude lower than two-dimensional Rossiter (flow/acoustics) instabilities. A steady mode of smaller spanwise wavelength is also identified for square cavities. The linear results indicate that the instability is hydrodynamic (rather than acoustic) in nature and arises from a generic centrifugal instability mechanism associated with the mean recirculating vortical flow in the downstream part of the cavity. These three-dimensional instabilities are related to centrifugal instabilities reported in flows over backward-facing steps, lid-driven cavity flows, and Couette flows.;Results from three-dimensional simulations of the nonlinear compressible Navier-Stokes equations are also reported. The formation of oscillating (and, in some cases, steady) spanwise structures is observed inside the cavity. The spanwise wavelength and oscillation frequency of these structures agree with the linear analysis predictions. When present, the shear-layer (Rossiter) oscillations experience a low-frequency modulation that arises from nonlinear interactions with the three-dimensional mode. These results are consistent with observations of low-frequency modulations and spanwise structures in previous experimental and numerical studies on open cavity flows.
机译:进行直接数值模拟以研究可用于未来控制应用的三维开放腔上的可压缩流的稳定性。首先,典型的二维自保持振荡(通常称为剪切层(Rossiter)模式)是二维的。各种流动条件下的腔体。然后进行线性稳定性分析,以搜索二维平均流的三维全局不稳定性,以查找在翼展方向上均匀的腔体。据报道,这种不稳定性的存在是由于一系列腔体的配置引起的。对于纵横比(长度与深度)为2和4的腔,三维模式的展向波长约为腔深度的1,并且其振荡频率低于二维Rossiter(流量/声学)不稳定。对于方腔,还确定了较小的展向波长的稳定模式。线性结果表明,这种不稳定性本质上是流体动力学的(而不是声学的),并且是由与腔体下游部分中的平均循环涡流相关的一般离心不稳定性机理引起的。这些三维不稳定性与向后台阶流动,盖驱动腔流和库埃特流中报告的离心不稳定性有关;还报告了非线性可压缩Navier-Stokes方程的三维模拟结果。在腔体内观察到振荡的(有时是稳定的)翼展结构的形成。这些结构的翼展方向波长和振荡频率与线性分析预测一致。当存在时,剪切层(Rossiter)振荡会经历低频调制,该低频调制是由与三维模式的非线性相互作用引起的。这些结果与先前对开放腔流动的实验和数值研究中的低频调制和展向结构的观察结果一致。

著录项

  • 作者

    Bres, Guillaume A.;

  • 作者单位

    California Institute of Technology.;

  • 授予单位 California Institute of Technology.;
  • 学科 Mechanical engineering.;Acoustics.;Aerospace engineering.
  • 学位 Ph.D.
  • 年度 2007
  • 页码 149 p.
  • 总页数 149
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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