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Aircraft Wake Vortex Scenarios Simulation Package for Takeoff and Departure

机译:飞机起降涡流情景模拟软件包

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摘要

WakeScene-D, a software package to determine wake vortex encounter probabilities for departures is described. The components of WakeScene-D that model traffic mix, aircraft trajectories, meteorological conditions, wake vortex evolution, and potential hazard area are specified together with the validation work accomplished thus far. Further, a brief estimation of related uncertainties is provided. WakeScene-D is an extension of WakeScene [10] that has been developed for approach and landing. Compared with this precursor version, major improvements have been achieved regarding realistic aircraft trajectory modeling on different standard departure routes. The developed trajectory model fully considers the impact of the most relevant parameters for 6 heavy vortex generator and 4 medium follower aircraft types. The comparison of simulated departures with full-flight simulator data and with 20,000 measured departures at Frankfurt airport yields good agreement. Another step ahead has been achieved by modeling the wake vortex behavior within inclined and moving gates. The gates that are oriented perpendicularly to the aircraft heading and flight-path angles are released in predefined time steps along the flight path and are adverted through space by the prevailing headwind's respective tailwinds. The real target of WakeScene-D, the determination of appropriate crosswind thresholds allowing for reduced aircraft separations, is the subject of ongoing work and will be documented in a future publication. The first application examples of the software package can be found in [9].
机译:描述了WakeScene-D,这是一种用于确定离开后尾流涡流遭遇概率的软件包。指定了WakeScene-D的组件,这些组件对交通混合,飞机轨迹,气象条件,尾流涡旋演变和潜在危险区域进行建模,并完成了迄今为止的验证工作。此外,提供了有关不确定性的简要估计。 WakeScene-D是WakeScene [10]的扩展,已针对进近和着陆而开发。与该先驱版本相比,在不同标准出发路线上的真实飞机轨迹建模方面已取得重大改进。所开发的轨迹模型充分考虑了最相关参数对6种重型涡流发生器和4种中型从动飞机的影响。将模拟离场与全程模拟器数据以及在法兰克福机场测得的20,000个离场进行比较,可以得出很好的一致性。通过对倾斜和移动门内的尾流涡流行为进行建模,已经迈出了又一步。垂直于飞行器航向角和飞行路径角定向的闸门会在预定的时间步长内沿着飞行路径释放,并通过盛行的逆风各自的顺风在整个空间进行调节。 WakeScene-D的真正目标是确定适当的侧风阈值以减少飞机的分离,这是正在进行的工作的主题,并将在以后的出版物中进行记录。软件包的第一个应用示例可在[9]中找到。

著录项

  • 来源
    《Journal of Aircraft》 |2009年第2期|713-717|共5页
  • 作者单位

    Deutsches Zentrum fuer Luft- und Raumfahrt, 82234 Wessling, Germany Institut fuer Physik der Atmosphaere, Oberpfaffenhofen;

    Deutsches Zentrum fuer Luft- und Raumfahrt, 82234 Wessling, Germany Institut fuer Robotik und Mechatronik, Oberpfaffenhofen;

    Technische Universitaet Berlin, 10587 Berlin, Germany;

    Deutsches Zentrum fuer Luft- und Raumfahrt, 38108 Braunschweig, Germany Institut fuer Flugfuehrung;

    Deutsches Zentrum fuer Luft- und Raumfahrt, 38108 Braunschweig, Germany Institut fuer Flugsystemtechnik;

    Universite Catholique de Louvain, 1348 Louvain-la-Neuve, Belgium;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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