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Acoustic field associated with parabolized stability equation models in turbulent jets

机译:湍流喷射器中与抛抛稳定性方程模型相关的声场

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Wavepackets are large-scale turbulent structures that are correlated and advected over distances that are large compared to the integral scales of turbulence, and have been shown to be responsible for the peak noise radiated at aft angles to the jet axis. The present paper discusses linear models of these wavepackets for supersonic turbulent jets based on Parabolized Stability Equations (PSE). In the past, results of this approach were shown to be in excellent agreement with coherent structures extracted from experimental near-field pressure and velocity data in subsonic jets. Here, we make use of a Large Eddy Simulation (LES) database for an isothermal and a moderately heated Mach 1.5 turbulent jets. Careful comparisons of the PSE models with near-field pressure fields from LES, filtered by means of Proper Orthogonal Decomposition (POD), demonstrate acceptable fidelity of the model. Finally, the acoustic far-field associated with the PSE wavepackets is computed using a Kirchhoff surface method, capturing reasonably well the far-field pressure at angles close to the peak.
机译:波拔丝是大规模湍流结构,其与与湍流的整体刻度相比大的距离相比,并且已被示出负责以沿射线轴处的AFT角度辐射的峰值噪声。本文讨论了基于抛物杠稳定性方程(PSE)的超声波湍流喷射器的这些波波皮的线性模型。在过去,该方法的结果显示出与从实验近场压力和亚音速喷射中的速度数据提取的相干结构的良好一致。在这里,我们利用大型涡流模拟(LES)数据库,用于等温和一个适度加热的Mach 1.5湍流喷射器。仔细比较PSE模型与LES的近场压力场,通过适当的正交分解(POD)过滤,展示了模型的可接受的保真度。最后,使用Kirchhoff表面方法计算与PSE波袋相关联的声学远场,在接近峰值的角度处捕获相当好的远场压力。

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