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Acoustic Resonance in a Cavity under a Subsonic Flow

机译:亚音速流下腔体中的声共振

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摘要

Acoustic resonances leading to high unsteady pressure levels may occur in flow past cavities. The resonance involves a coupling between the downstream-propagating instability wave on the shear layer spanning the open face of the cavity, and acoustic waves propagating within and external to the cavity. These elements of the disturbance field are coupled by the scattering processes that occur at the upstream and downstream ends of the cavity. We develop a theoretical prediction method that combines propagation models in the central region of the cavity with scattering models for the end regions. In our analyses of the scattering processes at the cavity ends, the square-corner geometry is treated exactly, by a method employing the Wiener--Hopf technique. The shear layer is approximated as a vortex sheet in the edge scattering analyses, but finite shear-layer thickness is accounted for in analyzing the propagation of the waves along the length of the cavity. The global analysis leads to a prediction for the resonant frequencies which has a form similar to the Rossiter formula, but contains no empirical constants. In addition to prediction of the frequency, our theory determines the temporal growth or decay rate of each mode. Finally, our theory also predicts the influence of secondary feedback loops involving other components of the unsteady field. Comparisons of the predictions with existing experimental data are made.
机译:导致高不稳定压力水平的声共振可能发生在经过腔体的流动中。共振涉及跨越腔的敞开面的剪切层上的下游传播的不稳定性波与在腔内部和外部传播的声波之间的耦合。干扰场的这些元素通过在腔体的上游和下游端发生的散射过程耦合在一起。我们开发了一种理论预测方法,该方法将空腔中心区域的传播模型与末端区域的散射模型结合在一起。在我们对腔体末端散射过程的分析中,采用维纳-霍普夫(Wiener-Hopf)技术的方法可以精确地处理方形角的几何形状。在边缘散射分析中,剪切层近似为涡旋片,但是在分析沿腔的长度方向上的波的传播时,剪切层的厚度是有限的。整体分析导致对谐振频率的预测,该预测具有类似于Rossiter公式的形式,但不包含经验常数。除了预测频率外,我们的理论还确定每种模式的时间增长率或衰减率。最后,我们的理论还预测了涉及非稳态磁场其他分量的次级反馈回路的影响。将预测结果与现有实验数据进行比较。

著录项

  • 作者

    Alvarez Jose Oliverio;

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  • 年度 2005
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  • 原文格式 PDF
  • 正文语种 EN
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