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Study on decay characteristics of vertical four-vortex system for increasing airport capacity

机译:垂直四涡流系统衰减特性升降机场容量

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The wake vortices of an aircraft descend by self-induction that enables a pilot to identify approximate wake location based on the preceding aircraft path. A pilot taking off an aircraft can avoid a wake vortex encounter by performing early rotation and flying at or above the climb path of the preceding aircraft. Such operation results in a situation in which two wake vortices are present in the air simultaneously in close proximity. In this study, the transport and decay characteristic processes involving interactions between the wake vortex pairs formed by the preceding and the following aircraft have been analyzed. The high altitude of the following aircraft was included as initial conditions, and atmospheric turbulence conditions were applied to large eddy simulations to account for the vortex core instability and nonlinear transport and decay. The obtained results were used to identify the decay processes that induce the rapid dissipation of wake vortices such as merging into a single counter-rotating pair, rapid dissipation, and formation of a vortex ring with or without deformation of the lower vortex pair. The third process could be effectively used to adjust the take-off separation time for increasing the capacity at airports. (C) 2020 The Authors. Published by Elsevier Masson SAS.
机译:飞机的尾部涡流通过自诱导下降,使得飞行员能够基于前面的飞机路径识别近似唤醒位置。消耗飞机的试验可以通过在前面飞机的爬坡路径或上方进行早期旋转和飞行来避免唤醒漩涡。这种操作导致在紧密接近时同时存在两个唤醒涡流的情况。在该研究中,已经分析了涉及通过前后和下列飞机形成的爪涡体对之间相互作用的运输和衰减特性过程。将下列飞机的高海拔被称为初始条件,并且将大气湍流条件应用于大涡模拟,以考虑涡旋核心不稳定性和非线性运输和衰减。所获得的结果用于识别诱导唤醒涡旋快速耗散的衰减过程,例如合并成单个反向旋转对,快速耗散和形成涡旋环,或者没有下涡体对的变形。第三种过程可以有效地用于调整用于增加机场容量的起飞分离时间。 (c)2020作者。由Elsevier Masson SA出版。

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