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Large-eddy simulation of separation and reattachment of a flat plate turbulent boundary layer

机译:平板湍流边界层分离与重新附着的大涡模拟

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摘要

© 2015 Cambridge University Press. We present large-eddy simulations (LES) of separation and reattachment of a flat-plate turbulent boundary-layer flow. Instead of resolving the near wall region, we develop a two-dimensional virtual wall model which can calculate the time- and space-dependent skin-friction vector field at the wall, at the resolved scale. By combining the virtual-wall model with the stretched-vortex subgrid-scale (SGS) model, we construct a self-consistent framework for the LES of separating and reattaching turbulent wall-bounded flows at large Reynolds numbers. The present LES methodology is applied to two different experimental flows designed to produce separation/reattachment of a flat-plate turbulent boundary layer at medium Reynolds number Reθ based on the momentum boundary-layer thickness θ. Comparison with data from the first case at demonstrates the present capability for accurate calculation of the variation, with the streamwise co-ordinate up to separation, of the skin friction coefficient, Reθ, the boundary-layer shape factor and a non-dimensional pressure-gradient parameter. Additionally the main large-scale features of the separation bubble, including the mean streamwise velocity profiles, show good agreement with experiment. At the larger Reθ = 11000 of the second case, the LES provides good postdiction of the measured skin-friction variation along the whole streamwise extent of the experiment, consisting of a very strong adverse pressure gradient leading to separation within the separation bubble itself, and in the recovering or reattachment region of strongly-favourable pressure gradient. Overall, the present two-dimensional wall model used in LES appears to be capable of capturing the quantitative features of a separation-reattachment turbulent boundary-layer flow at low to moderately large Reynolds numbers.
机译:©2015剑桥大学出版社。我们提出了平板湍流边界层流分离和重新附着的大涡模拟(LES)。而不是解析近壁区域,我们开发了一个二维虚拟壁模型,该模型可以以已解决的比例计算壁上时间和空间相关的皮肤摩擦矢量场。通过将虚拟壁模型与拉伸涡流子网格规模(SGS)模型相结合,我们为大雷诺数的分离和重新附着湍流壁流的LES构建了一个自洽框架。本LES方法应用于两个不同的实验流程,这些流程旨在基于动量边界层厚度θ在中等雷诺数Reθ的条件下产生平板湍流边界层的分离/重新附着。与第一种情况下的数据进行比较后,我们证明了当前的准确计算能力的能力,其中沿流坐标直至分离,皮肤摩擦系数,Reθ,边界层形状因子和无量纲压力-梯度参数。此外,分离气泡的主要大规模特征(包括平均流速分布)与实验结果吻合良好。在第二种情况下,较大的Reθ= 11000时,LES提供了对整个实验整个流向范围内测得的皮肤摩擦变化的良好预测,其中包括非常强的不利压力梯度,导致了分离气泡本身的分离,并且在压力梯度非常有利的恢复或重新连接区域中。总的来说,在LES中使用的当前二维壁模型似乎能够在低到中等大的雷诺数下捕获分离-重新附着湍流边界层流的定量特征。

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