Department of General Engineering, University of Wisconsin, Platteville, 1 University Plaza, Platteville, Wisconsin 53818, USA.
Chaos. 2010 Mar;20(1):017506. doi: 10.1063/1.3276062.
The effect of spatial and temporal resolutions and random errors on identification of Lagrangian coherent structures (LCSs) from Eulerian velocity fields is evaluated using two canonical flows: a two-dimensional vortex pair and a vortex ring formed by transient ejection of a jet from a tube. The flow field for the vortex pair case was steady and obtained analytically while the transient vortex ring flow was simulated using computational fluid dynamics. To evaluate resolution and random error effects, the flow fields were degraded by locally smoothing the flow and sampling it on a sparser grid to reduce spatial resolution, adding Gaussian distributed random noise to provide random errors, and/or subsampling the time series of vector fields to reduce the temporal resolution (the latter applying only for the vortex ring case). The degradation methods were meant to emulate distortions and errors introduced in common flow measurement methods such as digital particle image velocimetry. Comparing the LCS corresponding to the vortex boundary (separatrix) obtained from the degraded velocity fields with the true separatrix (obtained analytically for the vortex pair case or from high resolution, noise-free velocity fields for the vortex ring case) showed that noise levels as low as 5%-10% of the vortex velocity can cause the separatrix to significantly deviate from its true location in a random fashion, but the "mean" location still remained close to the true location. Temporal and spatial resolution degradations were found to primarily affect transient portions of the flow with strong spatial gradients. Significant deviations in the location of the separatrix were observed even for spatial resolutions as high as 2% of the jet diameter for the vortex ring case.
评估了时空分辨率和随机误差对从欧拉速度场识别拉格朗日相干结构(LCS)的影响,使用了两种典型流:二维涡对和通过管中射流瞬态喷射形成的涡环。涡对情况的流场是稳定的,并且通过解析获得,而瞬态涡环流则通过计算流体动力学进行模拟。为了评估分辨率和随机误差的影响,通过局部平滑流并在更稀疏的网格上对其进行采样来降低空间分辨率,添加高斯分布的随机噪声以提供随机误差,以及/或对矢量场的时间序列进行子采样来降低时间分辨率(后者仅适用于涡环情况)来降低流场。退化方法旨在模拟数字粒子图像测速等常见流动测量方法中引入的失真和误差。将从退化速度场获得的对应于涡边界(分隔线)的 LCS 与真实分隔线(对于涡对情况是通过解析获得的,对于涡环情况是从高分辨率、无噪声速度场获得的)进行比较,结果表明,噪声水平低至涡速度的 5%-10%可能会导致分隔线以随机方式严重偏离其真实位置,但“平均”位置仍接近真实位置。发现时空分辨率的降低主要影响具有强空间梯度的流动的瞬态部分。即使对于涡环情况,空间分辨率高达射流直径的 2%,也观察到分隔线位置的明显偏差。