期刊文献+

基于风速的动态尾流间隔标准计算方法 被引量:4

Dynamic Wake Turbulences Interval Standard Calculation Based on Wind Speed
下载PDF
导出
摘要 在保证安全的前提下压缩进场前后航空器间隔有助于提高机场容量,缓解拥堵情况。研究表明在逆风天气条件下能加快航空器尾涡的消散,同时在逆风天气条件下航空器的地速减小。这使得传统的基于距离的间隔标准存在提升潜力。欧美相关的科研机构和空管单位经过多年研究使用基于时间的间隔标准弥补基于距离的间隔标准在逆风条件下的不足。通过建立航空器进近阶段速度剖面计算所需飞行时间,统计机型和风速的分布并计算不同风速条件下采用基于时间的间隔标准对机场容量提升的效果。 On the premise of ensuring safety,we compress spacing between each arrival pair to help improve the airport capacity and relieve congestion.Studies have shown that aircraft wake turbulence can be accelerated dissipation under headwind conditions,at the same time,the ground speed of the aircraft is reduced under headwind conditions.This makes the traditional distance based separation standards have potential for improvement.European American research institutions and air traffic control units after years of research use time based separation offset the shortcomings of distance based separation standards under headwind conditions.Through establishing aircraft approach speed profile to calculate the required flight time.,statistical aircraft models and wind speed distribution to compute under different wind speed conditions using time based separation effect on airport capacity improvement.
作者 魏志强 胡杨 WEI Zhi-qiang;HU Yang(College of Air Traffic Management,Civil Aviation University of China,Tianjin 300300,China)
出处 《航空计算技术》 2018年第6期24-28,共5页 Aeronautical Computing Technique
基金 国家自然科学基金项目资助(U1533116 U1633125) 中央高校基本科研业务费项目资助(3122017067)
关键词 动态尾流 基于距离的间隔标准 基于时间的间隔标准 进近速度剖面 机场容量提升 dynamic wake turbulence distance based separation time based separation approach speed profile airport capacity improvement
  • 相关文献

参考文献4

二级参考文献29

  • 1[1]GREENE G C.An approximate model of vortex decay[J].Journal ofAircraft,1986,23 (7):566-573.
  • 2[2]LIU H-T.Tow-Tank Simulation of Vortex Wake Dynamics[C]//Procee-dings of the Aircraft Wake Vortices Conference.Washington D C:JN Hallock Ec1,1991.
  • 3[3]COBJON A,POINSOT T.Vortex model to define safe aircraft sepa-ration distances[J].Journal of Aireraft,1996,33(3):547-553.
  • 4[4]TURGUT SARPKAYA.A new model for vortex decay in the atmo-sphere[J].Journal of Aircraft,2000,37 (1):53-61.
  • 5[5]DAVID K R,CORNELIUS J O.The NASA Aircraft Vortex Spacing Sys-tem:Concept Demonstration Results and Future Direction[R].Virgini-a:NASA Langley Research Center,2001.
  • 6[6]ROBINS R E,DELISI D P.NWRA AVOSS Wake Vortex Prediction Algorithm Version 3.1.1[R].Virginia:NASA STI Program Of Office,2002.
  • 7[7]CROW S C.Stability theory for a pair of trailing vortices[J].AIAA Journal,1970,8(12):2172-2179.
  • 8VICROY D D,VIJGEN P M,REIMER H M,et al.Recent NASA wake-vortex flight tests,flow-physics database and wake-development analysis[C] ∥AIAA.World Aviation Congress and Exposition.Anaheim:AIAA,1998:1-14.
  • 9LIOT D.Wake vortex encounter model implementation and validation in the online(piloted)flight simulation environ-ment[R].Toulouse:WAVENC Technical Note TN-19,AM Airbus,2000.
  • 10DE BRUIN A C,SPEIJKER L J P,MOET H,et al.S-wake:assessment of wake vortex safety[R].Amsterdam:National Aerospace Laboratory NLR,2003.

共引文献49

同被引文献25

引证文献4

二级引证文献1

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部