首页> 外文期刊>International Journal of Heat and Fluid Flow >Identification and analysis of the meandering of a fin-tip vortex using Proper Orthogonal Decomposition (POD)
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Identification and analysis of the meandering of a fin-tip vortex using Proper Orthogonal Decomposition (POD)

机译:使用适当的正交分解(POD)识别和分析鳍尖涡翅片涡流的曲折

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The meandering of a vortex exists in a broad range of engineering applications and can lead to flow instability and other undesirable characteristics. Compared to a static vortex, measurement of a meandering vortex can result in a 'smeared' mean-flow field and increased levels of turbulence at the centre of the vortex. A case study was performed here on the meandering nature of a fin-tip vortex generated by a manoeuvring submarine. From stereoscopic particle image velocimetry (SPIV) measurements, it is possible to remove the meandering by shifting each instantaneous velocity field so as to produce a common centre for the vortex. In this paper, a snapshot Proper Orthogonal Decomposition (POD) technique is used to capture the dominant large-scale coherent structures (from inspection of eigenvalue or energy distributions) and to improve vortex centre identification. The POD reconstructed velocity field using only the most energetic modes enabled the coherent structures of the flow to be clearly visualised, providing improved identification of the vortex centre and subsequent evaluation of the meandering effect on the turbulent statistics. The present findings suggest that the vortex meandering only has a small impact on the ensemble-averaged resultant velocity, while contributing up to a maximum of 28% for the fluctuating component. The meandering correction also leads to an overall decrease of turbulence intensity in the peak fluctuating region of the vortex core.
机译:涡旋的曲折存在于广泛的工程应用中,并且可以导致流动不稳定性和其他不良特征。与静态涡旋相比,曲折涡流的测量可以导致“涂抹的”平均流场和涡旋中心的湍流水平增加。这里对由机动潜艇产生的翅片涡旋的蜿蜒性质进行了案例研究。通过立体粒子图像速度测量(SPIV)测量,可以通过使每个瞬时速度场移位以便产生涡流的公共中心来除去曲折。在本文中,使用快照适当的正交分解(POD)技术来捕获显着的大规模相干结构(从考验到特征值或能量分布)并改善涡旋中心识别。仅使用最有能量模式的POD重建速度场使得能够清楚地看到流动的相干结构,从而提供了改进的涡流中心的识别和随后对湍流统计的曲折效应的评估。本研究结果表明,涡旋曲折仅对合奏平均结果速度产生小的影响,同时波动组分的最大达到最多28%。曲折校正还导致涡旋芯的峰值波动区域中的湍流强度的总体减小。

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