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

机译:涡旋动力学和兴奋高速射流的声音

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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:这项工作旨在研究的动力学,以及由噪声生成的,采用同时的压力和速度测量沿着基于等离子体的激发和高级分析,以产生任一单独的或周期性的连贯环形涡流在大型结构的马赫0.9湍性射流剪切层。通过使用前馈神经网络随着平面速度快照和时间分辨的近场压力迹线来调查大规模结构的动态。然后,使用Ribner的基于扩张的声学类比,使用时间分辨的速度场计算出气化源术语。结果表明,环形涡流在潜在核心(时间平均)结束的上游开始的快速崩解;另外,在某些激励频率下,发生生成的环形涡流的合并或多个合并事件发生。对计算的源字段的分析发现,相干结构产生了与置于喷射Lipline的对象类似的波动相同的事件,尽管达到潜在核心。在结构合并或崩解的区域中,在结构合并或崩解的区域中快速调制,这导致了远场的噪声发射。

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