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Crosswind Shear Gradient Affect on Wake Vortices

机译:横向剪切梯度影响尾部漩涡

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Parametric simulations with a Large Eddy Simulation (LES) model are used to explore the influence of crosswind shear on aircraft wake vortices. Previous studies based on field measurements, laboratory experiments, as well as LES, have shown that the vertical gradient of crosswind shear, Le. the second vertical derivative of the environmental crosswind (?~2u_c/?z~2), can influence wake vortex transport. The presence of nonlinear vertical shear of the crosswind velocity can reduce the descent rate, causing a wake vortex pair to tilt and change in its lateral separation. The LES parametric studies confirm that the vertical gradient of crosswind shear does influence vortex trajectories. The parametric results also show that vortex decay from the effects of shear are complex since the crosswind shear (?u_c/?z), along with the vertical gradient of crosswind shear, can affect whether the lateral separation between wake vortices is increased or decreased. If the separation is decreased, the vortex linking time is decreased, and a more rapid decay of wake vortex circulation occurs. If the separation is increased, the time to link is increased, and at least one of the vortices of the vortex pair may have a longer life time than in the case without shear. In some cases, the wake vortices may never link.
机译:用大涡模拟(LES)模型参数模拟可用于探索侧风切变的飞机尾涡流的影响。基于现场测量,实验室实验,以及LES,先前的研究已经表明,侧风切变,勒的垂直梯度。环境侧风(?〜2u_c / - Z〜2),可以影响尾涡流传输的第二垂直衍生物。侧风速度的非线性垂直切变的存在可以减少下降速度,使尾流对倾斜和变化在其横向分离。在LES参数研究证实,侧风切变的垂直梯度确实会影响涡流轨迹。参数结果还显示从剪切效应涡流衰减是由于侧风切变(?u_c /ΔZ)复杂,侧风切变的垂直梯度一起可以影响尾涡流之间的横向间隔是增加还是减少。如果分离被降低,交联时间的涡流减小,尾涡流循环的更快速衰减发生。如果分离增加,则时间到链路增加,涡流对涡流中的至少一个可以具有更长的寿命的时间比在没有剪切的情况。在某些情况下,尾流可能永远不会联系起来。

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