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Skin-friction drag reduction in turbulent channel flow based on streamwise shear control

机译:基于流向剪切控制的湍流通道中皮肤摩擦阻力的减小

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It is known that stretching and intensification of a hairpin vortex by mean shear play an important role to create a hairpin vortex packet, which generates the large Reynolds shear stress associated with skin friction drag in wall-bounded turbulent flows. In order to suppress the mean shear at the wall for high efficient drag reduction (DR), in the present study, we explore an active flow control concept using stream wise shear control (SSC) at the wall. The longitudinal control surface is periodically spanwise-arranged with no-control surface while varying the structural spacing, and an amplitude parameter for imposing the strength of the actuating streamwise velocity at the wall is introduced to further enhance the skin friction DR. Significant DR is observed with an increase in the two parameters with an accompanying reduction of the Reynolds stresses and vorticity fluctuations, although a further increase in the parameters amplifies the turbulence activity in the near-wall region. In order to study the direct relationship between turbulent vortical structures and DR under the SSC, temporal evolution with initial eddies extracted by conditional averages for Reynolds-stress-maximizing Q2 events are examined. It is shown that the generation of new vortices is dramatically inhibited with an increase in the parameters throughout the flow, causing fewer vortices to be generated under the control. However, when the structural spacing is sufficiently large, the generation of new vortex is not suppressed over the no-control surface in the near-wall region, resulting in an increase of the second-and fourth-quadrant Reynolds shear stresses. Although strong actuating velocity intensifies the near-wall turbulence, the increase in the turbulence activity is attributed to the generation of counter-clockwise near-wall vortices by the increased vortex transport. (C) 2016 Elsevier Inc. All rights reserved.
机译:众所周知,通过平均剪切对发夹涡的拉伸和强化在产生发夹涡包中起着重要作用,发夹涡包会产生很大的雷诺剪切应力,这些应力与壁边界湍流中的皮肤摩擦阻力有关。为了抑制壁上的平均剪切力以实现高效减阻(DR),在本研究中,我们探索了使用壁上的流向剪切控制(SSC)的主动流控制概念。在改变结构间隔的同时,纵向控制表面与非控制表面周期性地沿翼展方向布置,并且引入用于在壁处施加致动流速度的强度的振幅参数,以进一步增强皮肤摩擦DR。随两个参数的增加,伴随雷诺应力和涡度波动的减少,DR显着增加,尽管参数的进一步增加会放大近壁区域的湍流活动。为了研究SSC下湍流涡旋结构与DR之间的直接关系,研究了雷诺应力最大化Q2事件的条件平均提取的初始涡流的时间演化。结果表明,随着整个流动过程中参数的增加,新涡旋的产生得到了显着的抑制,从而在控制下产生了更少的涡旋。但是,当结构间隔足够大时,在近壁区域的无控制表面上没有抑制新涡旋的产生,导致第二象限和第四象限雷诺剪切应力增加。尽管很强的驱动速度会加剧近壁湍流,但湍流活动的增加归因于涡流传输的增加导致了逆时针近壁涡流的产生。 (C)2016 Elsevier Inc.保留所有权利。

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