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High-frequency wavepackets in turbulent jets

机译:湍流喷气机中的高频波丝囊

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摘要

Wavepackets obtained as solutions of the flow equations linearised around the mean flow have been shown in recent work to yield good agreement, in terms of amplitude and phase, with those educed from turbulent jets. Compelling agreement has been demonstrated, for the axisymmetric and first helical mode, up to Strouhal numbers close to unity. We here extend the range of validity of wavepacket models to Strouhal number St = 4.0 and azimuthal wavenumber m = 4 by comparing solutions of the parabolised stability equations with a well-validated large-eddy simulation of a Mach 0.9 turbulent jet. The results show that the near-nozzle dynamics can be correctly described by the homogeneous linear model, the initial growth rates being accurately predicted for the entire range of frequencies and azimuthal wavenumbers considered. Similarly to the lower-frequency wavepackets reported prior to this work, the high-frequency linear waves deviate from the data downstream of their stabilisation locations, which move progressively upstream as the frequency increases.
机译:在近期工作中显示了作为线性围绕平均流动的流动方程的溶解的波波皮克在幅度和相位上产生良好的一致性,从湍流喷射器中引导的那些。令人信服的协议已经证明了轴对称和第一螺旋模式,直到靠近Unity的Strouhal数字。我们通过比较抛光稳定方程的解与Mach 0.9湍流射流的良好验证的大涡流模拟来扩展WaveHaket模型的有效性ST = 4.0和方位角波数M = 4的有效性。结果表明,邻近喷嘴动力学可以通过均匀的线性模型正确描述,所考虑的整个频率范围和方位角波数的准确预测初始增长率。类似于在该工作之前报告的较低频率的波波皮上,高频线性波偏离其稳定位置下游的数据,随着频率的增加而逐渐移动。

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