A reduced-order method for geometrically nonlinear analysis of the wing-upper-skin panels in the presence of buckling
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Publication:6590228
DOI10.1016/J.CAMWA.2024.06.014MaRDI QIDQ6590228
Zhen Yin, Ke Liang, Qiuyang Hao
Publication date: 21 August 2024
Published in: Computers & Mathematics with Applications (Search for Journal in Brave)
Cites Work
- Buckling of structures with finite prebuckling deformations - a perturbation, finite element analysis
- The Koiter-Newton approach using von Kármán kinematics for buckling analyses of imperfection sensitive structures
- An isogeometric formulation of the Koiter's theory for buckling and initial post-buckling analysis of composite shells
- A novel and highly efficient strategy to determine the `worst' imperfection shape for buckling of cylindrical shell panels
- Buckling and post-buckling analysis of extensible beam-columns by using the differential quadrature method
- Thermal-mechanical buckling analysis and optimization of the stringer stiffened cylinder using smeared stiffener based reduced-order models
- The reformulated Koiter–Newton method for thermal–mechanical buckling and postbuckling analysis of thin‐walled structures
- A novel Trefftz-based meshfree method for free vibration and buckling analysis of thin arbitrarily shaped laminated composite and isotropic plates
- Improved-FSDT-based solid-shell element for buckling analysis of plate, spherical cap, and cylindrical shell of FG porous materials
- A corotational mixed flat shell finite element for the efficient geometrically nonlinear analysis of laminated composite structures
- Accurate and efficient \textit{a posteriori} account of geometrical imperfections in Koiter finite element analysis
- An efficient mixed variational reduced-order model formulation for nonlinear analyses of elastic shells
- Post-buckling optimization of composite structures using Koiter's method
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