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首页> 外文期刊>Journal of Fluid Mechanics >Turbulent flow over a backward-facing step. Part 1. Effects of anti-cyclonic system rotation
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Turbulent flow over a backward-facing step. Part 1. Effects of anti-cyclonic system rotation

机译:朝后的台阶上有湍流。第1部分。反气旋系统旋转的影响

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The effects of rotation on turbulent flow with separation and reattachment are investigated by means of direct numerical simulations. The backward-facing step configuration is rotated about a spanwise axis such that the sudden expansion of the channel is on the pressure side. The upstream flow is a fully developed plane Poiseuille flow subjected to orthogonal-mode rotation, which subsequently detaches from the step corner and eventually reattaches further downstream. The size of the resulting separation bubble with recirculating flow diminishes monotonically with increasing rotation rates and the reattachment distance is reduced from about 7 to 3 step heights. This is ascribed to the augmentation of the cross-stream turbulence intensity in the anti-cyclonic shear layer formed between the bulk flow and the recirculating eddy due to the destabilizing influence of the Coriolis force. The spanwise-oriented vortex cells or roller eddies found in non-rotating shear layers were disrupted by the enhanced turbulence. The flow along the planar wall is subjected to an adverse pressure gradient induced by the sudden expansion. The stabilizing influence of the system rotation in this cyclonic shear layer tends to damp the turbulence, the flow becomes susceptible to flow separation, and a substantial cyclonic recirculation bubble is observed at the highest rotation rates. The resulting meandering of the bulk flow is associated with interactions between the anti-cyclonic shear layer at the stepped side and the cyclonic shear flow along the planar surface. These give rise to enhanced turbulence levels at the cyclonic side in spite of the otherwise stabilizing influence of the Coriolis force. Exceptionally high velocity fluctuations in the spanwise direction are observed in the vicinity of flow reattachment behind the step and ascribed to longitudinal Taylor-Grtler-like roll cells which extend into the backflow region. These roll cells arise from a centrifugal instability mechanism associated with the convex streamline curvature in the reattachment zone.
机译:通过直接数值模拟研究了旋转对分离和重新附着的湍流的影响。朝后的阶梯结构围绕翼展方向轴旋转,以使通道的突然膨胀在压力侧。上游流是经过正交模式旋转的完全展开的平面Poiseuille流,该流随后从台阶角分离并最终重新附着在下游。随着转速的增加,所产生的带有再循环流的分离气泡的尺寸单调减小,并且重新连接距离从大约7到3步高减小。这归因于由于科里奥利力的不稳定影响,在整体流和再循环涡流之间形成的反气旋剪切层中横流湍流强度的增加。在非旋转剪切层中发现的沿翼展方向的涡流单元或滚子涡流被增强的湍流破坏。沿平面壁的流动受到突然膨胀引起的不利压力梯度的影响。在该旋风剪切层中系统旋转的稳定影响趋向于减弱湍流,使流动易于分流,并且在最高旋转速率下观察到大量的旋风再循环气泡。整体流动的最终曲折与阶梯状侧的反气旋剪切层和沿着平面的气旋剪切流之间的相互作用有关。尽管科里奥利力有其他稳定的影响,但它们在旋风分离器的一侧产生了增加的湍流水平。在台阶后面的流动重新连接附近,在翼展方向上观察到异常高的速度波动,这归因于延伸到回流区域的纵向泰勒-格特勒式辊腔。这些滚动单元是由离心不稳定机制引起的,该机制与重新连接区域中的凸形流线曲率有关。

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