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旋翼高效/高精度气弹全耦合分析方法

WANG Xin ZHANG Xiayang ZHENG Lixiong XIANG Jinwu

航空学报2025,Vol.46Issue(z1):15-25,11.
航空学报2025,Vol.46Issue(z1):15-25,11.DOI:10.7527/S1000-6893.2025.32161

旋翼高效/高精度气弹全耦合分析方法

High-efficiency and high-precision aeroelastic full coupling method of rotor

WANG Xin 1ZHANG Xiayang 1ZHENG Lixiong 1XIANG Jinwu2

作者信息

  • 1. National Key Laboratory of Helicopter Aeromechanics,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China||Helicopter Research Institute,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China
  • 2. School of Aeronautic Science and Engineering,Beihang University,Beijing 100191,China
  • 折叠

摘要

Abstract

To balance calculation accuracy and efficiency of rotor aeroelastic coupling analysis,a fully coupling aero-elastic method based on GEBT/VVPM/L-B is established.Structurally,the dynamic model of blade is established by using the Geometrically Exact Beam Theory(GEBT),which effectively consider the large deformation.The Viscous Vortex Particle Method(VVPM)and the L-B dynamic stall model are coupled to consider the viscous flow,the distor-tion of the wake and the unsteady aerodynamics of the airfoil.In each iterative step,the aeroelastic response is in-serted into the aerodynamic computation module in a parametric form to realize the full coupling strategy.The c8534 flight of UH-60A is introduced for verification,and the effectiveness of the aeroelastic coupling method is verified by comparing with the experiment and the CFD/CSD tight coupling result.The results show that the proposed method can improve the computational accuracy significantly relative to the rigid rotor model.Compared with the CFD/CSD cou-pling method,the calculation efficiency can be improved by more than 54 times without apparently affecting the calcu-lation accuracy.The rotor aeroelastic loads can be effectively predicted in solving the strong nonlinear aeroelastic re-sponses,which verifies the robustness of the model.

关键词

黏性涡粒子方法/几何精确梁理论/气弹全耦合/结构载荷/气弹响应

Key words

viscous vortex particle method/geometrically exact beam theory/aeroelastic full coupling/structural loads/aeroelastic response

分类

航空航天

引用本文复制引用

WANG Xin,ZHANG Xiayang,ZHENG Lixiong,XIANG Jinwu..旋翼高效/高精度气弹全耦合分析方法[J].航空学报,2025,46(z1):15-25,11.

基金项目

国家自然科学基金(12472237,12032012) (12472237,12032012)

航空科学基金(2024Z010052002) (2024Z010052002)

中国科协青年人才托举工程(2022QNRC001) (2022QNRC001)

国家重点实验室基金(61422202201) (61422202201)

江苏高校优势学科建设工程 National Natural Science Foundation of China(12472237,12032012) (12472237,12032012)

Aeronautical Science Foundation of China(2024Z010052002) (2024Z010052002)

Young Elite Scientists Sponsorship Program by CAST(2022QNRC001) (2022QNRC001)

National Laboratory Foundation of China(61422202201) (61422202201)

Priority Academic Program Development of Jiangsu Higher Education Institutions ()

航空学报

OA北大核心

1000-6893

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