[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
… In the research field of wake vortex numerical simulation, the formation, evaluation and decay
of wake vortex are calculated … Induction of ground secondary vortex on aircraft wake vortex

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
… Aimed at this problem, this paper study the evolution of wake vortexEnhanced airport
capacity through safe, dynamic reductions in … mechanisms and artificial enhancement. Journal of …

基于数值模拟的飞机近场尾涡特征参数计算

温瑞英, 李鹏柯, 刘聪, 王红勇 - 空气动力学学报, 2023 - kqdlxxb.xml-journal.net
… Investigation of characteristic parameters of aircraft near-field wake vortex based on
numerical simulation[J]. Acta Aerodynamica Sinica, 2023, 41(5): 59-67. DOI: 10.7638/kqdlxxb-…

侧风影响下航空器尾涡LES 数值模拟

潘卫军, 王靖开, 罗玉明, 韩帅 - 西华大学学报(自然科学版), 2021 - xhuqk.com
… ensure the safety of aircraft operation and improve flight efficiency, ICEM CFD and Fluent
software were used to conduct numerical simulation of aircraft approach wake vortex under dif- …

[HTML][HTML] 大涡模拟技术在航空湍流研究中的应用

宋君强, 白皓坤, 程彬, 张宁, 张卫民, 冷洪泽… - 空气动力学 …, 2023 - pubs.cstam.org.cn
… However, in terms of mechanism, the interaction mechanism … the predictive skill of LES of
aviation turbulence is still limited by errors … of crosswind on the motion of aircraft wake vortex[J]. …

[PDF][PDF] 环境扰动下空中动目标探测技术综述

任维贺, 张月, 苏云, 张学敏, 邓红艳, 柳祎 - 红外与激光工程, 2022 - researching.cn
… moving targets and high-speed aircraft have caused serious threats to the national security
of all countries in the world, the detection of stealth moving targets and high-speed aircraft in …