A review of recent wake vortex research for increasing airport capacity
JN Hallock, F Holzäpfel - Progress in Aerospace Sciences, 2018 - Elsevier
This paper is a brief review of recent wake vortex research as it affects the operational
problem of spacing aircraft to increase airport capacity and throughput. The paper …
problem of spacing aircraft to increase airport capacity and throughput. The paper …
Contrail modeling and simulation
There is large uncertainty in the radiative forcing induced by aircraft contrails, particularly
after they transform to cirrus. It has recently become possible to simulate contrail evolution …
after they transform to cirrus. It has recently become possible to simulate contrail evolution …
飞机尾涡演变及快速预测的大涡模拟研究
林孟达， 崔桂香， 张兆顺， 许春晓， 黄伟希 - 力学学报, 2017 - lxxb.cstam.org.cn
随着我国人民生活水平的提高, 航空运输的重要性与日俱增, 航班延误问题也日益严重.
尾流间隔(保障后机不受前机尾流影响的最小安全间隔) 是制约机场效率的关键因素 …
尾流间隔(保障后机不受前机尾流影响的最小安全间隔) 是制约机场效率的关键因素 …
A contrail cirrus prediction model
U Schumann - Geoscientific Model Development, 2012 - gmd.copernicus.org
A new model to simulate and predict the properties of a large ensemble of contrails as a
function of given air traffic and meteorology is described. The model is designed for …
function of given air traffic and meteorology is described. The model is designed for …
Long-wave deformation of in-ground-effect wake vortex under crosswind condition
Z Xu, D Li, J Cai - Aerospace Science and Technology, 2023 - Elsevier
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 …
when the vortex column is deformed with a long wavelength, the vortex core position is …
Aircraft wake-vortex decay in ground proximity—physical mechanisms and artificial enhancement
Aircraft wake-vortex evolution in ground proximity is investigated numerically by means of
large-eddy simulations. The simulations are performed either with a flat ground or with …
large-eddy simulations. The simulations are performed either with a flat ground or with …
[HTML][HTML] 飞机尾涡流场参数的仿真计算方法研究综述
魏志强， 屈秋林， 刘薇， 徐肖豪 - 空气动力学学报, 2019 - html.rhhz.net
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 …
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 …
On the life cycle of individual contrails and contrail cirrus
U Schumann, AJ Heymsfield - Meteorological Monographs, 2017 - journals.ametsoc.org
The life cycle of individual (initially line shaped) contrails behind aircraft and of contrail cirrus
(aged contrails mixed with other ice clouds) is described. The full contrail life cycle is …
(aged contrails mixed with other ice clouds) is described. The full contrail life cycle is …
Large-eddy simulation of aircraft wake evolution from roll-up until vortex decay
T Misaka, F Holzäpfel, T Gerz - AIAA journal, 2015 - arc.aiaa.org
The evolution of aircraft wake vortices from the roll-up until vortex decay is studied by large-
eddy simulation. An aircraft model and the surrounding flow field obtained from high-fidelity …
eddy simulation. An aircraft model and the surrounding flow field obtained from high-fidelity …
Review of idealized aircraft wake vortex models
NN Ahmad, F Proctor - 52nd Aerospace Sciences Meeting, 2014 - arc.aiaa.org
Properties of three aircraft wake vortex models, Lamb-Oseen, Burnham-Hallock, and Proctor
are reviewed. These idealized models are often used to initialize the aircraft wake vortex …
are reviewed. These idealized models are often used to initialize the aircraft wake vortex …