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On removing the near-field coherent structures in a jet and its impact on the radiated sound

机译:在移除喷射器中的近场相干结构及其对辐射声音的影响

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Sound radiation from a subsonic turbulent jet is examined after a hypothetical removal of near-field coherent structures in the low azimuthal components of the velocity fluctuations. With the help of a well-validated database of large-eddy simulation, the near-field coherent structures are extracted using discrete wavelet transform (DWT), and their spatial structures are examined using proper orthogonal decomposition (POD). The acoustic far field is calculated using Lighthill's acoustic analogy. It is shown that the coherent part extracted by DWT accounts for most of the fluctuation energy of axial velocity, whereas the incoherent part, assumed to have a Gaussian probability distribution, has little energy. After the coherent part is removed, the axisymmetric component of the sound is found to be significantly reduced by around 7 dB in the overall sound pressure level at 30 degrees with respect to the jet axis. The reduction is mostly at low Strouhal numbers (St < 0.4, based on the speed of sound and the nozzle exit diameter). The first few POD modes of the near-field coherent part, which capture most of the fluctuation energy, are found to be characterised by large-scale wavy structures. After these POD modes are removed, the axisymmetric component of the sound pressure level is also reduced considerably, by around 5 dB/St at St = 0.2. When velocity components in the first and second helical azimuthal modes are removed, the overall sound pressure levels are reduced for a wide range of polar angles. The results also show that axial velocity fluctuations in the second helical mode are closely associated with sound radiation at high polar angles. Far-field azimuthal decomposition indicates that the sound reduction takes place in multiple azimuthal modes. The results suggest that there is a causal link between the axisymmetric components of the near-field coherent fluctuations and far-field low-angle jet noise. On the other hand, velocity components in near-field helical azimuthal modes are coupled for sound radiation in helical azimuthal modes. It is also suggested that not only the large-scale wavy structures in low POD modes, but also the smaller-scale coherent structures in higher POD modes need to be included for jet noise modelling, because they are both shown to be efficient at sound radiation.
机译:在速度波动的低方位角分量中假设近场相干结构假设之后,检查来自亚音速湍流射流的声音辐射。与大涡模拟的充分验证的数据库的帮助下,近场相干结构使用离散小波变换(DWT)萃取,并用适当的正交分解(POD)进行检查它们的空间结构。声学远场使用Lighthill的声学类比计算。结果表明,由DWT提取的相干部件用于轴向速度的大部分波动能量,而假设具有高斯概率分布的不连贯部分具有很小的能量。在去除相干部分之后,发现声音的轴对称分量在相对于喷射轴上以30度在30度的整体声压级中显着降低约7dB。减少主要是在低斯特鲁姆数(ST <0.4,基于声音的速度和喷嘴出口直径)。捕获大部分波动能量的近几个POD模式的近几个荚模式被发现由大规模的波浪结构的特征在于。除了去除这些POD模式之后,ST = 0.2的声压水平的轴对称组件也显着降低了大约5dB / s。当移除第一和第二螺旋方形方形模式中的速度分量时,对于宽范围的极性角度,整体声压水平降低。结果还表明,第二螺旋模式中的轴向速度波动与高极性角度的声辐射密切相关。远场方位角分解表明声音减少在多种方位角模式下进行。结果表明,近场相干波动和远场低角度射流的轴对称组分之间存在因果关系。另一方面,近场螺旋方位角模式中的速度分量耦合以用于螺旋方位角模式的声辐射。还建议不仅需要在低豆荚模式中的大规模波浪结构,而且需要更高豆荚模式中的较小刻度相干结构,因为喷射噪声建模,因为它们都显示在声辐射时有效。

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