机翼近场尾流流动特性的附着涡模型分析

许向阳; 李良星; 向祖涛

doi:10.7652/xjtuxb202504020

您当前的位置：

首页 >

文章列表页 >

机翼近场尾流流动特性的附着涡模型分析

—————————————————————— | 更新时间：2026-01-06

- 机翼近场尾流流动特性的附着涡模型分析
- Analysis of the Attached Vortex Model for the Flow Characteristics of Wing Near-Field Wakes
- 西安交通大学学报 2025年59卷第4期页码：213-222
- 作者机构：
  
  西安交通大学动力工程多相流国家重点实验室， 710049，西安
- 作者简介：
  
  许向阳（2000—），男，硕士生；
  李良星（通信作者），男，副教授。
- 基金信息：
  
  东方航空技术应用研发中心资助项目(CMC（2023）TC03103D)
- DOI：10.7652/xjtuxb202504020
  中图分类号： V211.4
- 收稿：2024-11-07，
  
  网络首发：2024-12-31，
  
  纸质出版：2025-04-10
- 稿件说明：
移动端阅览
许向阳, 李良星, 向祖涛. 机翼近场尾流流动特性的附着涡模型分析[J]. 西安交通大学学报, 2025,59(4):213-222.

XU Xiangyang, LI Liangxing, XIANG Zutao. Analysis of the Attached Vortex Model for the Flow Characteristics of Wing Near-Field Wakes[J]. Journal of Xi’an Jiaotong University, 2025, 59(4): 213-222.
许向阳, 李良星, 向祖涛. 机翼近场尾流流动特性的附着涡模型分析[J]. 西安交通大学学报, 2025,59(4):213-222. DOI： 10.7652/xjtuxb202504020.

XU Xiangyang, LI Liangxing, XIANG Zutao. Analysis of the Attached Vortex Model for the Flow Characteristics of Wing Near-Field Wakes[J]. Journal of Xi’an Jiaotong University, 2025, 59(4): 213-222. DOI： 10.7652/xjtuxb202504020.

摘要

为研究飞机尾流演化过程中的旋涡初始流动特性，提出了一种基于附着涡模型的尾流初始特征参数计算方法，用于准确计算飞机近场初始尾流环量、涡核间距和涡核半径等特征参数。采用SST

k-ω

湍流模型对NACA0012直机翼的尾流特性进行了三维数值模拟研究，分析了3种展弦比、3种迎角及3种来流速度下的近场尾流流动特性，并通过附着涡模型对模拟结果进行验证与分析，建立了近场尾流初始流动特征参数的计算模型。结果表明：与传统基于最大涡量值和最小压力位置确定涡核位置的方法相比，根据附着涡模型计算的尾流速度分布来确定涡核位置和半径的方法更为精确，近场尾流环量与Rankine模型预测的结果最为接近；利用拟合得到的机翼展向附着涡环量分布，尾流环量计算平均误差为7%，涡核间距和涡核半径计算平均误差为15%。基于附着涡模型的尾流初始特征参数计算方法比基于椭圆形载荷机翼计算方法更准确，更具备普适性。

Abstract

To investigate the initial flow characteristics of vortices during the evolution of aircraft wake

a novel method for calculating the initial characteristic parameters of wakes based on the attached vortex model is proposed to accurately calculate characteristic parameters such as the initial wake circulation

vortex core spacing

and vortex core radius in the near field of aircraft wakes. The near-field wake characteristics of a NACA0012 straight wing are numerically simulated in three dimensions using the SST

k-ω

turbulent model. The near-field wake flow characteristics under three aspect ratios

three angles of attack

and three freestream velocities are analyzed. The simulated results are validated and analyzed using the attached vortex model

and a calculation model for the initial flow characteristic parameters of near-field wakes is established. The findings indicate that compared to traditional methods that rely on maximum vorticity and minimum pressure positions to determine vortex core locations

the method of determining the vortex core position and radius based on the wake velocity distribution calculated by the attached vortex model is more accurate. The near-field wake circulation closely aligns with predictions from the Rankine model. By using the fitted distribution of the wing spanwise attached vortex circulation

the average error of wake circulation calculation is 7%

and the average error of vortex core spacing and vortex core radius calculation is 15%. The method of calculating the initial characteristic parameters of wakes based on the attached vortex model is more accurate and universal than the metho

d based on the elliptical load wing calculation.

关键词

Keywords

references

GERZ T , HOLZÄPFEL F , DARRACQ D . Commercial aircraft wake vortices [J ] . Progress in Aerospace Sciences , 2002 , 38 ( 3 ): 181 - 208 .

周彬 . 飞机尾流的微结构特征及散射特性研究 [D ] . 长沙 : 国防科学技术大学 , 2009 .

BOUHAFID Y , BONNE N , JACQUIN L . Combined Reynolds-averaged Navier-Stokes/large-eddy simulations for an aircraft wake until dissipation regime [J ] . Aerospace Science and Technology , 2024 , 154 : 109512 .

CHU Nana , NG K K H , LIU Ye , et al . Assessment of approach separation with probabilistic aircraft wake vortex recognition via deep learning [J ] . Transportation Research: Logistics and Transportation Review , 2024 , 181 : 103387 .

ROMEOS A , GIANNADAKIS A , PERRAKIS K , et al . Co-rotating vortex interaction [J ] . Aircraft Engineering and Aerospace Technology , 2016 , 88 ( 2 ): 285 - 293 .

WEI Zhiqiang , LU Tong , GU Runping , et al . DBN-GABP model for estimation of aircraft wake vortex parameters using lidar data [J ] . Chinese Journal of Aeronautics , 2024 , 37 ( 9 ): 347 - 368 .

HOLZÄPFEL F . Analysis of potential wake vortex encounters at a major European airport [J ] . Aircraft Engineering and Aerospace Technology , 2017 , 89 ( 5 ): 634 - 643 .

BREITSAMTER C . Wake vortex characteristics of transport aircraft [J ] . Progress in Aerospace Sciences , 2011 , 47 ( 2 ): 89 - 134 .

CHIGIER N A , CORSIGLIA V R . Tip vortices: velocity distributions [EB/OL ] . ( 1971-09-01 ) [ 2024-10-10 ] . https://ntrs.nasa.gov/citations/19710027203 https://ntrs.nasa.gov/citations/19710027203 .

LANCHESTER F W . Aerodynamics: constituting the first volume of a complete work on aerial flight [M ] . [S.l.] : Constable , 1911 .

TOLLMIEN W , SCHLICHTING H , GÖRTLER H , et al . Über Flüssigkeitsbewegung bei sehr kleiner reibung [J ] . Ludwig Prandtl Gesammelte Abhandlungen: Zur Angewandten Mechanik, Hydro-Und Aerodynamik , 1961 : 575 - 584 .

JOUKOVSKII N . Geometrische untersuchungen über die kutta'sche strömung [J ] . Trans Physical Section of the Imperial Society of the Friends of Natural Science, Moscow , 1912 , 15 : 36 - 47 .

JOUKOWSKI N . On annexed vortices [J ] . Proc Phys Section of the Natural Science Society , 1906 , 13 ( 2 ): 12 - 25 .

KUTTA W . Auftriebskräfte in strömenden Flüssigkeiten [J ] . Illustrierte Aeronautische Mitteilungen , 1902 , 6 ( 133 ): 133 - 135 .

FAGE A , SIMMONS L F G . VII. An investigation of the air-flow pattern in the wake of an aërofoil of finite span [J ] . Philosophical Transactions of the Royal Society of London: Containing Papers of a Mathematical or Physical Character , 1926 , 225 ( 626/635 ): 303 - 330 .

UHL A , DUFHAUS S , HÖRNSCHEMEYER R , et al . Numerical investigation of vortex roll-up processes using different wingtip shapes [J ] . PAMM , 2017 , 17 ( 1 ): 697 - 698 .

温瑞英 , 王红勇 , 刘薇 , 等 . 飞机近场尾涡特性数值模拟研究 [J ] . 飞行力学 , 2016 , 34 ( 1 ): 46 - 50 .

WEN Ruiying , WANG Hongyong , LIU Wei , et al . Numerical simulation of near field characteristics of aircraft wake vortex [J ] . Flight Dynamics , 2016 , 34 ( 1 ): 46 - 50 .

钱宇 , 蒋皓 . 基于 k-ω 湍流模型的翼尖涡演化过程数值模拟 [J ] . 科学技术与工程 , 2020 , 20 ( 35 ): 14708 - 14713 .

QIAN Yu , JIANG Hao . Numerical analysis of evolution process of vortex wake based on k-ω turbulent model [J ] . Science Technology and Engineering , 2020 , 20 ( 35 ): 14708 - 14713 .

张钰沁 . 飞机爬升阶段尾流演化与遭遇研究 [D ] . 广汉 : 中国民用航空飞行学院 , 2024 .

韩宝玉 , 熊鹰 , 叶金铭 . 湍流模型对三维翼梢涡流场数值模拟的影响 [J ] . 航空学报 , 2010 , 31 ( 12 ): 2342 - 2347 .

HAN Baoyu , XIONG Ying , YE Jinming . Effect of turbulence models on numerical simulation of tip vortex flow field behind 3D wing [J ] . Acta Aeronautica et Astronautica Sinica , 2010 , 31 ( 12 ): 2342 - 2347 .

BURNHAM D C , HALLOCK J N , TOMBACH I H , et al . Ground-based measurements of the wake vortex characteristics of a B-747 aircraft in various configurations [EB/OL ] . ( 1978-12-01 ) [ 2024-10-10 ] . https://rosap.ntl.bts.gov/view/dot/10807 https://rosap.ntl.bts.gov/view/dot/10807 .

RANKINE W J M . XXVII. On the thermal energy of molecular vortices [J ] . The London, Edinburgh, and Dublin Philosophical Magazine and Journal of Science , 1870 , 39 ( 260 ): 211 - 221 .

LAMB H . Hydrodynamics [M ] . 6th ed . Cambridge, UK : Cambridge University Press , 1993 : 764 .

PROCTOR F H . Numerical simulations of an isolated microburst. Part I: dynamics andstructure [J ] . Journal of the Atmospheric Sciences , 1988 , 45 ( 21 ): 3137 - 3160 .

WINCKELMANS G , COCLE R , DUFRESNE L , et al . Vortex methods and their application to trailing wake vortex simulations [J ] . Comptes Rendus Physique , 2005 , 6 ( 4/5 ): 467 - 486 .

CHOW J S , ZILLIAC G G , BRADSHAW P . Measurements in the near-field of a turbulent wingtip vortex [C ] // 31st Aerospace Sciences Meeting . Reston, VA, USA : AIAA , 1993 : 551 .

浏览量

下载量

CSCD

文章被引用时，请邮件提醒。

提交

工具集

关联资源

液氢管路输运中静电积聚机理与电流密度分布特征研究

X射线辐照下聚酰亚胺材料空间电荷分布特性的数值模拟

异质裂隙内超临界CO2地热提取特性数值模拟研究

工质与叶轮传热对超临界二氧化碳向心透平气动性能与流动特性的作用机制

直接空冷岛侧部百叶窗防冻性能与适用性研究