Review on the artificial calculating methods for aircraft wake vortex flow field parameters

WEI Zhiqiang; QU Qiulin; LIU Wei; XU Xiaohao

doi:10.7638/kqdlxxb-2017.0160

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Review on the artificial calculating methods for aircraft wake vortex flow field parameters

更新时间：2026-05-28

- Review on the artificial calculating methods for aircraft wake vortex flow field parameters
- Vol. 37, Issue 1, Pages: 33-42(2019)
- 作者机构：
  
  1. 中国民航大学空中交通管理学院,天津,300300
  2. 北京航空航天大学航空科学与工程学院,北京,100028
- 作者简介：
- 基金信息：
- DOI：10.7638/kqdlxxb-2017.0160
  CLC： V212.13+3
- Published：2019
- 稿件说明：
移动端阅览
魏志强, 屈秋林, 刘薇, 徐肖豪. 飞机尾涡流场参数的仿真计算方法研究综述[J]. 空气动力学学报, 2019, 37(1): 33-42.

WEI Zhiqiang, QU Qiulin, LIU Wei, et al. Review on the artificial calculating methods for aircraft wake vortex flow field parameters[J]. 2019, 37(1): 33-42.
魏志强, 屈秋林, 刘薇, 徐肖豪. 飞机尾涡流场参数的仿真计算方法研究综述[J]. 空气动力学学报, 2019, 37(1): 33-42. DOI： 10.7638/kqdlxxb-2017.0160.

WEI Zhiqiang, QU Qiulin, LIU Wei, et al. Review on the artificial calculating methods for aircraft wake vortex flow field parameters[J]. 2019, 37(1): 33-42. DOI： 10.7638/kqdlxxb-2017.0160.

摘要

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方法在流场数值模拟方面的研究现状及存在问题；在尾涡流场参数的快速仿真计算方面，综述了典型计算模型的特点及存在的主要问题，包括CROW不稳定性、Greene消散模型、APA消散模型、TDAWP消散模型、D2P消散模型和三阶段消散模型等，分析了上述模型的精度与应用情况。最后对国内外研究现状进行了总结分析，提出了该领域未来的研究方向。

Abstract

As the basis of the research on reducing wake vortex separations

numerical simulation and constructing of fast-models for simulating wake vortex have become the focus of many international ATM research institutes. In the research field of wake vortex numerical simulation

the formation

evaluation and decay of wake vortex are calculated based on RANS

LES or DES methods. These data can help to reveal the regulation of wake vortex

and can provide basic foundation for constructing wake vortex models. In the field of fast simulation of wake vortex

Some organizations have done many theoretical researches on the formation and dissipation of wake vortex

attempting to deduce the behavioural characteristics of wake vortex by establishing complex mathematical models

including CROW instability

Greene model

APA model

TDAWP model

D2P model and the three-phase decay model

etc. The research status quo is analyzed and the key works in the next phase are also provided.

关键词

Keywords

references

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