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Unsteady aerodynamic modeling and analysis of aircraft model in multi-DOF coupling maneuvers at high angles of attack with attention mechanism

Wenzhao DONG Xiaoguang WANG Dongbo HAN Qi LIN

中国航空学报(英文版)2025,Vol.38Issue(6):349-361,13.
中国航空学报(英文版)2025,Vol.38Issue(6):349-361,13.DOI:10.1016/j.cja.2025.103444

Unsteady aerodynamic modeling and analysis of aircraft model in multi-DOF coupling maneuvers at high angles of attack with attention mechanism

Unsteady aerodynamic modeling and analysis of aircraft model in multi-DOF coupling maneuvers at high angles of attack with attention mechanism

Wenzhao DONG 1Xiaoguang WANG 1Dongbo HAN 1Qi LIN1

作者信息

  • 1. School of Aerospace Engineering,Xiamen University,Xiamen 361102,China
  • 折叠

摘要

关键词

Unsteady aerodynamics/Aerodynamic modeling/High angle of attack/Wind tunnel test/Attention mechanism

Key words

Unsteady aerodynamics/Aerodynamic modeling/High angle of attack/Wind tunnel test/Attention mechanism

引用本文复制引用

Wenzhao DONG,Xiaoguang WANG,Dongbo HAN,Qi LIN..Unsteady aerodynamic modeling and analysis of aircraft model in multi-DOF coupling maneuvers at high angles of attack with attention mechanism[J].中国航空学报(英文版),2025,38(6):349-361,13.

基金项目

This research was supported by the National Natural Science Foundation of China(Nos.12172315,12072304,11702232),the Fujian Provincial Natural Science Foundation,China(No.2021J01050),and the Aeronautical Science Foundation of China(No.20220013068002). (Nos.12172315,12072304,11702232)

中国航空学报(英文版)

1000-9361

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