首页|期刊导航|中国航空学报(英文版)|Dynamical analysis and nonlinear vibration control of integrated composite beam structure in thermal environment

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

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

College of Aerospace Engineering,Shenyang Aerospace University,Shenyang 110136,ChinaAVIC Shenyang Aircraft Design & Research Institute,Shenyang 110035,ChinaLiaoning General Aviation Academy,Shenyang 110136,ChinaCollege of Aerospace Engineering,Shenyang Aerospace University,Shenyang 110136,ChinaCollege of Aerospace Engineering,Shenyang Aerospace University,Shenyang 110136,ChinaCollege of Aerospace Engineering,Shenyang Aerospace University,Shenyang 110136,ChinaCollege of Aerospace Engineering,Shenyang Aerospace University,Shenyang 110136,China

Composite laminated beamDynamics characteristicIntegrated composite beamModal experimentNiTiNOL steel wire ropeNonlinear vibration control

Composite laminated beamDynamics characteristicIntegrated composite beamModal experimentNiTiNOL steel wire ropeNonlinear vibration control

《中国航空学报(英文版)》 2026 (1)

278-300,23

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).

10.1016/j.cja.2025.103702

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