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Crosswind Shear Gradient Affect on Wake Vortices

机译:侧风剪切梯度对尾涡的影响

摘要

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, i.e. the second vertical derivative of the environmental crosswind, 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, 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:使用具有大涡模拟(LES)模型的参数模拟来研究侧风切变对飞机尾流涡流的影响。先前基于现场测量,实验室实验以及LES的研究表明,侧风切变的垂直梯度,即环境侧风的第二个垂直导数,可以影响尾流涡流。侧风速度的非线性垂直切变的存在会降低下降速率,导致尾涡对倾斜并改变其横向间隔。 LES参数研究证实,侧风切变的垂直梯度确实会影响涡旋轨迹。参数结果还表明,由于横风切变以及横风切变的垂直梯度会影响尾流涡流之间的横向间隔是增大还是减小,因此剪切效应引起的涡旋衰减是复杂的。如果间隔减小,则涡旋连接时间减少,并且尾涡流循环更快地衰减。如果间隔增加,则连接时间增加,并且涡流对中的至少一个涡流的寿命可能比没有剪切的情况下更长。在某些情况下,尾流涡流可能永远不会链接。

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