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零压力梯度湍流边界层渐近状态的研究方法。

Approach to an asymptotic state for zero pressure gradient turbulent boundary layers.

作者信息

Nagib Hassan M, Chauhan Kapil A, Monkewitz Peter A

机构信息

Illinois Institute of Technology, 10 W 32nd Street, Chicago, IL 60616, USA.

出版信息

Philos Trans A Math Phys Eng Sci. 2007 Mar 15;365(1852):755-70. doi: 10.1098/rsta.2006.1948.

Abstract

Flat plate turbulent boundary layers under zero pressure gradient at high Reynolds numbers are studied to reveal appropriate scale relations and asymptotic behaviour. Careful examination of the skin-friction coefficient results confirms the necessity for direct and independent measurement of wall shear stress. We find that many of the previously proposed empirical relations accurately describe the local Cf behaviour when modified and underpinned by the same experimental data. The variation of the integral parameter, H, shows consistent agreement between the experimental data and the relation from classical theory. In accordance with the classical theory, the ratio of Delta and delta asymptotes to a constant. Then, the usefulness of the ratio of appropriately defined mean and turbulent time-scales to define and diagnose equilibrium flow is established. Next, the description of mean velocity profiles is revisited, and the validity of the logarithmic law is re-established using both the mean velocity profile and its diagnostic function. The wake parameter, Pi, is shown to reach an asymptotic value at the highest available experimental Reynolds numbers if correct values of logarithmic-law constants and an appropriate skin-friction estimate are used. The paper closes with a discussion of the Reynolds number trends of the outer velocity defect which are important to establish a consistent similarity theory and appropriate scaling.

摘要

研究了高雷诺数下零压力梯度的平板湍流边界层,以揭示合适的尺度关系和渐近行为。对表面摩擦系数结果的仔细研究证实了直接和独立测量壁面剪应力的必要性。我们发现,许多先前提出的经验关系在经过相同实验数据修正和支撑后,能准确描述局部摩擦系数行为。积分参数H的变化表明实验数据与经典理论关系之间存在一致的一致性。根据经典理论,δ和δ渐近线的比值为常数。然后,确定了适当定义的平均时间尺度与湍流时间尺度的比值用于定义和诊断平衡流的有用性。接下来,重新审视了平均速度剖面的描述,并使用平均速度剖面及其诊断函数重新建立了对数定律的有效性。如果使用对数定律常数的正确值和适当的表面摩擦估计值,尾流参数Pi在最高可用实验雷诺数下会达到一个渐近值。本文最后讨论了外部速度缺陷的雷诺数趋势,这对于建立一致的相似性理论和适当的标度很重要。

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