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Dynamical analysis and nonlinear vibration control of integrated composite beam structure in thermal environment

Donghui LI Faming ZHANG Qunfang LI Shang GAO Jian ZANG Yewei ZHANG Fengtian YANG

中国航空学报（英文版）2026，Vol.39Issue(1)：278-300,23.

中国航空学报（英文版）2026，Vol.39Issue(1)：278-300,23.DOI:10.1016/j.cja.2025.103702

Dynamical analysis and nonlinear vibration control of integrated composite beam structure in thermal environment

Donghui LI ¹Faming ZHANG ²Qunfang LI ³Shang GAO ¹Jian ZANG ¹Yewei ZHANG ¹Fengtian YANG¹

作者信息

1. College of Aerospace Engineering,Shenyang Aerospace University,Shenyang 110136,China
2. AVIC Shenyang Aircraft Design & Research Institute,Shenyang 110035,China
3. Liaoning General Aviation Academy,Shenyang 110136,China
折叠

摘要

关键词

Composite laminated beam/Dynamics characteristic/Integrated composite beam/Modal experiment/NiTiNOL steel wire rope/Nonlinear vibration control

Key words

Composite laminated beam/Dynamics characteristic/Integrated composite beam/Modal experiment/NiTiNOL steel wire rope/Nonlinear vibration control

引用本文复制引用

Donghui LI,Faming ZHANG,Qunfang LI,Shang GAO,Jian ZANG,Yewei ZHANG,Fengtian YANG..Dynamical analysis and nonlinear vibration control of integrated composite beam structure in thermal environment[J].中国航空学报（英文版）,2026,39(1):278-300,23.

基金项目

The work presented in this paper was supported by the National Natural Science Foundation of China(No.12272240),the Liaoning Revitalization Talents Program,China(No.XLYC2203197). （No.12272240）

中国航空学报（英文版）

ISSN：1000-9361

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