Plate lines to enhance wake vortex decay for reduced separations between landing aircraft

IF 2.8 Q2 MECHANICS Flow (Cambridge, England) Pub Date : 2022-03-02 DOI:10.1017/flo.2021.16
F. Holzäpfel, D. Vechtel, Grigory Rotshteyn, A. Stephan
{"title":"Plate lines to enhance wake vortex decay for reduced separations between landing aircraft","authors":"F. Holzäpfel, D. Vechtel, Grigory Rotshteyn, A. Stephan","doi":"10.1017/flo.2021.16","DOIUrl":null,"url":null,"abstract":"Abstract 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 International Airport are used to assess the potential for reducing minimum aircraft separations facilitated by plate lines during approach and landing following the re-categorisation (RECAT-EU) methodology for revised wake turbulence categorisation. To ensure that no other parameters controlling wake vortex decay bias the analysis, it is verified that wind speed, atmospheric turbulence, thermal stratification and flight altitude reside in similar ranges with and without the plates. The analysis follows the steps of the RECAT-EU method to generate non-dimensional so-called reasonable worst-case circulation decay curves; one as a reference for nominal operations without plates and one representing the accelerated wake vortex decay brought about by the plate lines. The difference between the two circulation decay curves corresponds to the non-dimensional time-based aircraft separation reduction potential that can be translated into distance-based separation gains. Depending on the particular RECAT-EU category combination, the attained aircraft separation reduction potential ranges between 12% and 15%. Constricting the analysis to wake vortices generated by one aircraft type representing the Upper Heavy RECAT-EU category, the separation reduction potential amounts up to 24%.","PeriodicalId":93752,"journal":{"name":"Flow (Cambridge, England)","volume":" ","pages":""},"PeriodicalIF":2.8000,"publicationDate":"2022-03-02","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"2","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Flow (Cambridge, England)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1017/flo.2021.16","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q2","JCRName":"MECHANICS","Score":null,"Total":0}
引用次数: 2

Abstract

Abstract 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 International Airport are used to assess the potential for reducing minimum aircraft separations facilitated by plate lines during approach and landing following the re-categorisation (RECAT-EU) methodology for revised wake turbulence categorisation. To ensure that no other parameters controlling wake vortex decay bias the analysis, it is verified that wind speed, atmospheric turbulence, thermal stratification and flight altitude reside in similar ranges with and without the plates. The analysis follows the steps of the RECAT-EU method to generate non-dimensional so-called reasonable worst-case circulation decay curves; one as a reference for nominal operations without plates and one representing the accelerated wake vortex decay brought about by the plate lines. The difference between the two circulation decay curves corresponds to the non-dimensional time-based aircraft separation reduction potential that can be translated into distance-based separation gains. Depending on the particular RECAT-EU category combination, the attained aircraft separation reduction potential ranges between 12% and 15%. Constricting the analysis to wake vortices generated by one aircraft type representing the Upper Heavy RECAT-EU category, the separation reduction potential amounts up to 24%.
查看原文
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
加强尾流涡流衰减的板线,以减少着陆飞机之间的间隔
摘要为了降低尾流在最终接近过程中遇到尾流涡的风险,人们提出了所谓的板线。在维也纳国际机场进行的为期六个月的测量活动中收集的数据用于评估在修订尾流湍流分类的重新分类(RECAT-EU)方法之后,在进近和降落过程中减少由板线促进的最小飞机分离的潜力。为了确保控制尾流衰减的其他参数不影响分析,验证了在有和没有板的情况下,风速、大气湍流度、热分层和飞行高度处于相似的范围内。分析遵循RECAT-EU方法的步骤,生成无因次的所谓合理最坏情况环流衰减曲线;一个作为标称操作的参考,没有板,一个代表加速尾迹涡衰减带来的板线。两个循环衰减曲线之间的差异对应于基于时间的无量纲飞机分离减少势,可以转化为基于距离的分离增益。根据具体的RECAT-EU类别组合,实现的飞机分离减少潜力在12%到15%之间。将分析范围缩小到代表上层重型RECAT-EU类别的一种飞机产生的尾流涡,分离减少的潜力高达24%。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 去求助
来源期刊
CiteScore
2.40
自引率
0.00%
发文量
0
期刊最新文献
Benefits of controlled inclination for contactless transport by squeeze-film levitation Investigating cohesive sediment dynamics in open waters via grain-resolved simulations Stream lamination and rapid mixing in a microfluidic jet for X-ray spectroscopy studies Competing effects of buoyancy-driven and electrothermal flows for Joule heating-induced transport in microchannels Effects of prey capture on the swimming and feeding performance of choanoflagellates
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术
文献互助 智能选刊 最新文献 互助须知 联系我们:info@booksci.cn
Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。
Copyright © 2023 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1