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REGENERATION MECHANISMS OF NEAR-WALL TURBULENCE STRUCTURES

机译:近壁湍流结构的再生机理

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摘要

Direct numerical simulations of a highly constrained plane Couette flow are employed to study the dynamics of the structures found in the near-wall region of turbulent flows. Starting from a fully developed turbulent flow, the dimensions of the computational domain are reduced to near the minimum values which will sustain turbulence. A remarkably well-defined, quasi-cyclic and spatially organized process of regeneration of near-wall structures is observed. This process is composed of three distinct phases: formation of streaks by streamwise vortices, breakdown of the streaks, and regeneration of the streamwise vortices. Each phase sets the stage for the next, and these processes are analysed in detail. The most novel results concern vortex regeneration, which is found to be a direct result of the breakdown of streaks that were originally formed by the vortices, and particular emphasis is placed on this process. The spanwise width of the computational domain corresponds closely to the typically observed spanwise spacing of near-wall streaks. When the width of the domain is further reduced, turbulence is no longer sustained. It is suggested that the observed spacing arises because the time scales of streak formation, breakdown and vortex regeneration become mismatched when the streak spacing is too small, and the regeneration cycle at that scale is broken. [References: 24]
机译:对高度受限的平面Couette流进行直接数值模拟,以研究在湍流近壁区域中发现的结构动力学。从充分发展的湍流开始,计算域的尺寸减小到接近将维持湍流的最小值。观察到近壁结构再生的明确定义的,准循环和空间组织的过程。该过程由三个不同的阶段组成:流向涡流形成条纹,条纹破裂以及流向涡流的再生。每个阶段都为下一个阶段奠定了基础,并对这些过程进行了详细分析。最新颖的结果与涡流再生有关,涡流再生是涡流最初由涡流形成的破裂的直接结果,因此特别强调了这一过程。计算域的翼展方向宽度非常接近通常观察到的近壁条纹的翼展方向间距。当畴的宽度进一步减小时,湍流将不再持续。建议观察到的间距是由于条纹间距太小而导致条纹形成,击穿和涡旋再生的时间尺度不匹配,并且破坏了该尺度下的再生周期而产生的。 [参考:24]

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