论文标题

最佳的涡流粘度,用于湍流喷气机中相干结构模型的最佳粘度

Optimal eddy viscosity for resolvent-based models of coherent structures in turbulent jets

论文作者

Pickering, Ethan, Rigas, Georgios, Schmidt, Oliver T., Sipp, Denis, Colonius, Tim

论文摘要

通过湍流平均流场的线性分辨分析计算得出的响应模式已显示出在壁结合和游离剪切流中观察到的湍流相干结构的定性特征。为了使这种解析模型预测性,必须关闭非线性强迫项。这样做的策略包括施加自洽的三元相互作用集,提出各种源模型或通过湍流建模。对于后者,一些研究人员提出了使用在波动场上线性作用的平均场涡流粘度。在这项研究中,采用数据驱动的方法来定量地改善线性共振模型,通过推断出最佳的涡流粘度场,该模型最大程度地利用了使用光谱适当的正交分解(SPOD)对高而菲德利元素的数据进行频谱正交分解(SPOD)教育的主要分解模式的投影。我们在亚音速,跨语音和超音速条件下使用大型型模拟数据库进行圆形等热射流,并表明最佳的涡质粘度大大改善了分辨率和SPOD模式之间的比对,在那些频率上达到了90%以上的对齐,在喷气式飞机表现出较低的速度响应。然后,我们考虑了涡流粘度的固定模型,并表明通过单个常数的校准,结果通常接近最佳。特别是,使用标准的雷诺平均 - 长 - 长 - 长烟(RANS)具有单个系数的涡流效率分辨率模型,为三个湍流喷气机以及跨越最有能力的波数和频率的Spod和Resolvent模式之间的实质性一致。

Response modes computed via linear resolvent analysis of a turbulent mean-flow field have been shown to qualitatively capture characteristics of the observed turbulent coherent structures in both wall-bounded and free shear flows. To make such resolvent models predictive, the nonlinear forcing term must be closed. Strategies to do so include imposing self-consistent sets of triadic interactions, proposing various source models, or through turbulence modelling. For the latter, several investigators have proposed using the mean-field eddy viscosity acting linearly on the fluctuation field. In this study, a data-driven approach is taken to quantitatively improve linear resolvent models by deducing an optimal eddy-viscosity field that maximizes the projection of the dominant resolvent mode to the energy-optimal coherent structure educed using spectral proper orthogonal decomposition (SPOD) of data from high-fidelity simulations. We use large-eddy simulation databases for round isothermal jets at subsonic, transonic, and supersonic conditions and show that the optimal eddy viscosity substantially improves the alignment between resolvent and SPOD modes, reaching over 90% alignment at those frequencies where the jet exhibits a low-rank response. We then consider a fixed model for the eddy viscosity and show that with the calibration of a single constant, the results are generally close to the optimal one. In particular, the use of a standard Reynolds-Averaged-Navier-Stokes (RANS) eddy-viscosity resolvent model, with a single coefficient, provides substantial agreement between SPOD and resolvent modes for three turbulent jets and across the most energetic wavenumbers and frequencies.

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