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Normal and cross-flow Reynolds stresses: differences between confined and semi-confined flows

机译:正向和横流雷诺应力:密闭和半密闭流之间的差异

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摘要

Understanding turbulent wall-bounded flows remains an elusive goal. Most turbulent phenomena are non-linear, complex and have broad range of scales that are difficult to completely resolve. Progress is made only in minute steps and enlightening models are rare. Herein, we undertake the effort to bundle several experimental and numerical databases to overcome some of these difficulties and to learn more about the kinematics of turbulent wall-bounded flows. The general scope of the present work is to quantify the characteristics of wall-normal and spanwise Reynolds stresses, which might be different for confined (e.g., pipe) and semi-confined (e.g., boundary layer) flows. In particular, the peak position of wall-normal stress and a shoulder in spanwise stress never described in detail before are investigated using select experimental and direct numerical simulation databases available in the open literature. It is found that the positions of the -peak in confined and semi-confined flow differ significantly above δ + ≈ 600. A similar behavior is found for the position of the -peak. The upper end of the logarithmic region seems to be closely related to the position of the -peak. The -shoulder is found to be twice as far from the wall than the -peak. It covers a significantly large portion of the typical zero-pressure-gradient turbulent boundary layer.
机译:了解湍流边界流仍然是一个遥不可及的目标。大多数湍流现象是非线性的,复杂的,并且具有范围广泛的尺度,很难完全解决。进步只有一步之遥,而启发性的模型却很少。在此,我们致力于将几个实验和数值数据库捆绑在一起,以克服其中的一些困难,并进一步了解湍流边界流的运动学。本工作的总体范围是对壁法向应力和跨向雷诺应力的特征进行量化,这对于密闭(例如管道)和半密闭(例如边界层)流可能会有所不同。特别是,使用公开文献中提供的精选实验和直接数值模拟数据库研究了以前从未详细描述的壁法向应力和肩向应力的峰值位置。发现在δ + ≈600以上时,限制和半限制流中-peak的位置存在显着差异。对于-peak的位置也发现了类似的行为。对数区域的上端似乎与-peak的位置紧密相关。发现-shoulder距墙壁的距离是-peak的两倍。它覆盖了典型的零压力梯度湍流边界层的很大一部分。

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