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Numerical simulation of acoustic scattering by a plane turbulent shear layer: Spectral broadening study

机译:平面湍流剪切层的声散射数值模拟:谱展宽研究

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摘要

The scattering of an acoustic wave by a 3D spatially-developing plane turbulent mixing layer is investigated by means of a Large Eddy Simulation (LES). First, a plane turbulent mixing layer of initial Reynolds number Re-omega,Re- 0 approximate to 1200 and convective Mach number M-c approximate to 0.12 is computed and its characteristics are validated by comparisons to experimental and numerical studies. Then, an acoustic source is introduced in the computational domain and the LES of both the turbulent mixing layer and the acoustic field is carried out, allowing the direct computation of the scattered pressure field. Computational Aero Acoustics (CAA) methods have been implemented to minimize spurious pressure fluctuations created while the turbulent structures leave the computational domain. The side-lobes of the scattered pressure power spectral density are recovered and a parametric study, involving the convection velocity of the large turbulent structures, the amplitude and the tonal frequency of the source is carried out. The part of scattered energy, the frequency shift of the side-lobes and the spectra decrease are found to be correctly estimated. Analysis of directivity at the side-lobes frequencies show a progressive re-distribution of the acoustic energy, as the acoustic wave propagates through the turbulent shear layer. (C) 2016 Elsevier Ltd. All rights reserved.
机译:利用大涡模拟(LES)研究了3D空间展开的平面湍流混合层对声波的散射。首先,计算了初始雷诺数Re-omega,Re-0接近1200和对流马赫数M-c接近0.12的平面湍流混合层,并通过与实验和数值研究的比较验证了其特性。然后,在计算域中引入声源,并进行湍流混合层和声场的LES,从而可以直接计算散射压力场。已经实施了计算航空声学(CAA)方法,以最大程度地减小湍流结构离开计算域时产生的假压力波动。恢复了散射压力功率谱密度的旁瓣,并进行了参数研究,其中涉及大型湍流结构的对流速度,震源的振幅和音调频率。发现散射能量的一部分,旁瓣的频移和频谱的减少是正确估计的。在旁瓣频率处的指向性分析表明,随着声波传播通过湍流剪切层,声能会逐渐重新分布。 (C)2016 Elsevier Ltd.保留所有权利。

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