TRACKING COHERENT STRUCTURES IN MASSIVELY-SEPARATED AND TURBULENT FLOWS

Matthew Rockwood, Yangzi Huang, Melissa A. Green
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引用次数: 14

Abstract

Coherent vortex structures are tracked in simulations of massively-separated and turbulent flows. Topological Lagrangian saddle points are found using intersections of the positive and negative finite-time Lyapunov exponent (FTLE) ridges, and these points are then followed in order to track individual coherent structure motion in both a complex interacting three-dimensional flow (turbulent channel) and during vortex formation (two-dimensional bluff body shedding). For a simulation of wall-bounded turbulence in a channel flow, tracking Lagrangian saddles shows that the average structure convection speed exhibits a similar trend as a previously published result based on velocity and pressure correlations, giving validity to the method. When this tracking method is applied in a study of a circular cylinder in cross-flow it shows that Lagrangian saddles rapidly accelerate away from the cylinder surface as the vortex sheds. This saddle behavior is compared with the time-resolved static pressure distribution on the circular cylinder, yielding locations on a cylinder surface where common sensors could detect this phenomenon, which is not available from force measurements or vortex circulation calculations. The current method of tracking coherent structures yields insight into the behavior of the coherent structures in both of the diverse flows presented, highlighting the breadth of its potential application.
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在大规模分离和湍流中跟踪相干结构
在大规模分离和湍流的模拟中跟踪了相干涡结构。拓扑拉格朗日鞍点是利用有限时间李雅普诺夫指数(FTLE)正负脊的交点找到的,然后跟踪这些点,以便在复杂的相互作用的三维流动(湍流通道)和涡旋形成(二维bluff体脱落)期间跟踪单个相干结构的运动。对于通道流动中壁面湍流的模拟,跟踪拉格朗日鞍表明,平均结构对流速度与先前发表的基于速度和压力相关性的结果具有相似的趋势,证明了该方法的有效性。将该跟踪方法应用于横流圆柱体的研究,结果表明,随着涡流的脱落,拉格朗日鞍迅速加速离开圆柱体表面。将这种鞍形行为与圆柱体上的时间分辨静压分布进行比较,在圆柱体表面的屈服位置,普通传感器可以检测到这种现象,这是无法从力测量或涡循环计算中获得的。目前跟踪相干结构的方法可以深入了解所呈现的两种不同流中相干结构的行为,突出了其潜在应用的广度。
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TRACKING COHERENT STRUCTURES IN MASSIVELY-SEPARATED AND TURBULENT FLOWS INNER-OUTER INTERACTIONS IN A TURBULENT BOUNDARY LAYER OVERLYING COMPLEX ROUGHNESS SKIN-FRICTION DRAG REDUCTION USING THE METHOD OF SPANWISE MEAN VELOCITY GRADIENT PLANE TURBULENT COUETTE FLOW: DNS, LARGE SCALE STRUCTURES AND SYMMETRY INDUCED SCALING LAWS SMALL-SCALE PHASE ORGANIZATION THROUGH LARGE-SCALE INPUTS IN A TURBULENT BOUNDARY LAYER
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