吉林大学学报(理学版) ›› 2026, Vol. 64 ›› Issue (2): 430-0438.

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一类机翼模型的动力学行为

程利芳, 刘欣, 张理涛, 陈灿   

  1. 郑州航空工业管理学院 数学学院, 郑州 450046
  • 收稿日期:2024-12-09 出版日期:2026-03-26 发布日期:2026-03-26
  • 通讯作者: 程利芳 E-mail:lfczam@126.com

Dynamical Behavior of a Kind of Wing Model

CHENG Lifang, LIU Xin, ZHANG Litao, CHEN Can   

  1. School of Mathematics, Zhengzhou University of Aeronautics, Zhengzhou 450046, China
  • Received:2024-12-09 Online:2026-03-26 Published:2026-03-26

摘要: 研究一类修正机翼模型的平衡点和极限环的分岔行为以及平衡态的吸引域. 结果表明: 结构恢复力矩系数将影响平衡态的分岔结构, 导致两对具有相反稳定性的非平凡平衡点因同时发生Fold分岔而出现共存或消失现象; 当某些初始分量固定时, 吸引域呈中心对称的结构分布; 当频率比作为分岔参数时, 平凡平衡点因发生Hopf分岔而失去稳定性, 稳定极限环发生Pitchfork分岔产生2个稳定的极限环; 随着频率比的进一步减小, 2个共存极限环同时发生Neimmark-Sacker分岔, 出现2个稳定的二维环面.

关键词: Hopf分岔, Pitchfork分岔, 吸引域, 极限环

Abstract: We studied the bifurcation behaviors of equilibrium points and limit cycles as well as attraction domain of equilibrium state of a modified wing model. The results show that bifurcation structure of equilibrium state is affected by the coefficients of the structural restoring moment so that two pairs of nontrivial equilibrium points with opposite stability coexist or vanish due to the simultaneous occurrence of Fold bifurcations. The attraction domains exhibit a centrosymmetric structural distribution when some initial components are fixed. When the frequency ratio is used as a bifurcation parameter, the trivial equilibrium point loses stability due to Hopf bifurcation, and the stable limit cycles undergo a Pitchfork bifurcation to produce two stable limit cycles. With further reduction of the frequency ratio, two coexisting limit cycles simultaneously undergo a Neimmark-Sacker bifurca
tion, leading to two stable two-dimensional toruses.

Key words: Hopf bifurcation, Pitchfork bifurcation, attraction domain, limit cycle

中图分类号: 

  • O415.6