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Analytical Prediction of Aeroacoustic Cavity Oscillations

机译:气凝修腔振荡的分析预测

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High-speed flow over cavities in vehicle surfaces can produce intense tonal pressure fluctuations. This problem has been of concern for decades, especially for aircraft, but the underlying physical mechanisms have not been well understood. A fairly simple analytical model has been developed that improves understanding of the oscillation mechanisms in shallow rectangular cavities. The model describes the phenomenon, and gives reasonable agreement with experimental data. The analysis is constructed from waves that exist in a system having a finite thickness shear layer dividing two acoustic media, one at rest and one in motion. The wave types can be interpreted in physical terms. The shear layer thickness has an important effect on the speed of convective waves. Only two convective waves and three acoustic waves suffice to represent the basic phenomenon. Mass addition and removal at the rear bulkhead due to shear layer oscillation plays an important role in the process. Conditions on energetics and shear layer motion at the rear of the cavity must be satisfied simultaneously for the oscillation to occur.
机译:车辆表面的高速流动空腔可以产生强调的色调压力波动。这一问题对于几十年来说,特别是飞机,但潜在的物理机制尚未得到很好的理解。已经开发了一个相当简单的分析模型,从而提高了对浅矩形腔中振荡机制的理解。该模型描述了现象,并与实验数据提供合理的协议。该分析由存在于具有分割两个声学介质的有限厚度剪切层的系统中存在的波构成,一个在静止和一个运动中。波类型可以在物理术语中解释。剪切层厚度对对流波的速度具有重要影响。只有两个对流波和三个声波足以代表基本现象。由于剪切层振荡导致的后舱壁在后舱壁上的肿块在过程中起重要作用。必须同时满足在腔后部的能量和剪切层运动的条件,以便发生振荡。

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