A study of fully developed plane turbulent channel flow subject to spanwisesystem rotation through direct numerical simulations is presented. In order tostudy both the influence of the Reynolds number and spanwise rotation onchannel flow, the Reynolds number $Re = U_b h/\nu$ is varied from a low 3000 toa moderate $31\,600$ and the rotation number $Ro = 2 \Omega h/U_b$ is variedfrom 0 to 2.7, where $U_b$ is the mean bulk velocity, $h$ the channel half gapand $\Omega$ the system rotation rate. The mean streamwise velocity profiledisplays also at higher $Re$ the characteristic linear part with a slope nearto $2 \Omega$ and a corresponding linear part in the profiles of the productionand dissipation rate of turbulent kinetic energy appears. With increasing $Ro$a distinct unstable side with large spanwise and wall-normal Reynolds stressesand a stable side with much weaker turbulence develops in the channel. The flowstarts to relaminarize on the stable side of the channel and persistingturbulent-laminar patterns appear at higher $Re$. If $Ro$ is further increasedthe flow on the stable side becomes laminar-like while at yet higher $Ro$ thewhole flow relaminarizes, although the calm periods might be disrupted byrepeating bursts of turbulence, as explained by Brethouwer (2016). Theinfluence of the Reynolds number is considerable, in particular on the stableside of the channel where velocity fluctuations are stronger and the flowrelaminarizes less quickly at higher $Re$. Visualizations and statistics showthat at $Ro=0.15$ and 0.45 large-scale structures and large counter rotatingstreamwise roll cells develop on the unstable side. These become lessnoticeable and eventually vanish when $Ro$ raises, especially at higher $Re$.At high $Ro$, the largest energetic structures are larger at lower $Re$.
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机译:通过直接数值模拟研究了完全展展的平面湍流通道流在翼展方向系统旋转下的研究。为了研究雷诺数和翼展方向旋转对通道流量的影响,雷诺数$ Re = U_b h / \ nu $从低到3000到中等的$ 31 \,600 $和旋转数$ Ro = 2 \ ωh / U_b $在0到2.7之间变化,其中$ U_b $是平均体积速度,$ h $是通道的半间隙,而$ \ Omega $是系统旋转速度。平均流速分布也显示出较高的$ Re $特征线性部分,其斜率接近$ 2 \ Omega $,并且在动能的产生和耗散速率的分布图中出现了相应的线性部分。随着Ro的增加,在通道中会产生较大的翼展方向和壁法向雷诺应力的明显不稳定面,并且湍流弱得多的稳定面会发展。流量在通道的稳定侧开始重新分层,并且在更高的$ Re $处出现持续的湍流分层模式。如果进一步增加$ Ro $,则稳定侧的流量会变成层流状,而如果$ Ro $更高,则整个流量会重新分层,尽管如Brethouwer(2016)所述,反复的湍流爆发可能会扰乱平静期。雷诺数的影响相当大,尤其是在通道的稳定侧,在该侧上速度波动较大,并且在较高的$ Re $时,流量相对较慢。可视化和统计数据表明,在$ Ro = 0.15 $和0.45的情况下,大型结构和大型逆向旋转滚动单元在不稳定的一侧发展。当Ro $升高时(尤其是在Re $较高时),这些变得不那么明显,最终消失.Ro $高时,$ Re $较低时最大的能量结构较大。
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