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Vortex Dynamics and Sound Emission in an Excited High-Speed Jet

机译:高速喷气机中的涡旋动力学和声发射

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This work aims to study the dynamics of, and noise generated by, the large-scale structures in a Mach 0.9 turbulent jet using simultaneous pressure and velocity measurements alongside plasma-based excitation and advanced analyses to produce either individual or periodic coherent ring-vortices in the shear layer. The dynamics of the large-scale structures were investigated by stochastically-estimating time-resolved velocity fields from planar velocity snapshots and time-resolved near-field pressure traces using a feedforward neural network. Then, using Ribner's dilatation-based acoustic analogy, the aeroacous-tic source terms were computed using the time-resolved velocity field. Results indicated that the ring-vortices underwent a rapid disintegration beginning just upstream of the (time-averaged) end of the potential core; additionally, under certain excitation frequencies merging or multiple merging events of the generated ring-vortices occurred. Analysis of the computed source fields found that the coherent structures produced a convected wavepacket-like event, centered on the jet lipline though reaching into the potential core. Rapid modulation of this wavepacket amplitude and extent occurred in regions of structure merging or disintegration, which resulted in noise emission to the far-field.
机译:这项工作旨在通过同时进行压力和速度测量以及基于等离子体的激励和高级分析来研究Mach 0.9湍流中大型结构的动力学和产生的噪声,从而产生单个或周期性相干环涡。剪切层。通过使用前馈神经网络从平面速度快照和时间分辨的近场压力迹线中随机估计时间分辨的速度场,研究了大型结构的动力学。然后,使用Ribner基于膨胀的声学类比,使用时间分辨速度场来计算航空声源项。结果表明,环形涡旋从势核(时间平均)末端的上游开始迅速崩解。另外,在某些激发频率下,发生了所产生的环形涡旋的合并或多次合并事件。对计算出的源场的分析发现,相干结构产生了一个对流的波包状事件,虽然到达了潜在的核,但以射流唇线为中心。这种波包幅度和幅度的快速调制发生在结构合并或分解的区域,这导致向远场的噪声发射。

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