作为缩减尾流间隔, 提高运行效率的研究基础, 尾涡流场的仿真计算技术是国内外民航空管研究
领域的一个研究热点. 在飞机尾涡流场的数值模拟方面, 介绍了雷诺平均, 大涡模拟和分离涡模拟 …

The in-ground-effect (IGE) aircraft wake vortex poses great hazards to airplanes. Especially
when the vortex column is deformed with a long wavelength, the vortex core position is …

The final approach and touchdown of a landing aircraft is studied numerically with different
hybrid Reynolds-averaged Navier–Stokes (RANS)/large-eddy simulations (LES) …

To mitigate the risk of wake vortex encounters during final approach, so-called plate lines
have been developed. Wake vortices generated by landing aircraft induce secondary …

Pairwise multirotor wake-encounter response studies with identical leader-follower
unmanned aerial system (UAS) were conducted for a pair of Phantom 3 sized (∼ 1.2 kg) …

Abstract The Wake Vortex Prediction System WSVS (WirbelSchleppenVorhersageSystem)
has been developed to tactically increase airport capacity by employing dynamically …

The effect of crosswinds on paired approach (PA) procedures for Closely Spaced Parallel
Runways (CSPR) is investigated in this paper by fully utilizing the crosswind environment to …

The observation and identification of wake vortex are considered important factors to reduce
aviation accidents and increase airport capacity. In addition to aircraft parameters, the …

To mitigate the risk of wake vortex encounters during final approach, so-called plate lines
have been developed. Data collected during a six-month measurement campaign at Vienna …

A turbulent two-vortex system (T-2VS) is obtained by inserting analytical model wake
vortices into very weak homogeneous isotropic turbulence (HIT) and by evolving them in …