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Effects of adverse pressure gradient on quasi-coherent structures in turbulent boundary layer

机译:逆压梯度对湍流边界层准相干结构的影响

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Statistical and kinematic characteristics of turbulent boundary layer flwos subjected to adverse pressure gradients are found to differ significnatly from those of zero-pressure-gradient ordinary boundary layers. The turbulent energy and shear stress transport vu~2 and vuv occurs in the directio ntoward the wall from the regions away fro mthe wall, as the pressure gradient paramete P~+ increases. This event is completely opposite to that in zero-pressure-gradient cases. The instataneous waveforms of third-order moments are markedly altered in the near-wall region. The quadrant splitting and trajectory analyses reveal the obvious changes do occur in large-amplitude sweep motions (Q4) and outward itneractiosn (Q1). On the other hand, the contributions from other coherent motions, especially the ejectio nmotions (Q2), significantly decrease and their duratiosn become logner, i.e., these motions are dull and less active. Moreover, multi-point simultaneous measuremtns with five X-probes are made to depict the kinematic pictures of hte effects of the adverse pressure gradient on the eddy strucutres.
机译:发现受到不利压力梯度的湍流边界层流体的统计和运动学特征与零压力梯度普通边界层的统计学和运动学特征显着不同。随着压力梯度参数P〜+的增加,湍流能量和切应力传输vu〜2和vuv发生在远离壁的区域朝向壁的方向。此事件与零压力梯度情况下的事件完全相反。在近壁区域,三阶矩的瞬时波形发生了明显变化。象限分裂和轨迹分析显示,在大振幅扫动运动(Q4)和向外迭代(Q1)中确实发生了明显的变化。另一方面,来自其他相干运动,特别是喷射运动(Q2)的贡献显着降低,并且其持续时间变成记录器,即,这些运动是乏味的并且不太活跃。此外,用五个X探针进行多点同时测​​量,以描绘不利压力梯度对涡流结构的影响的运动学图像。

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