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Variable-Kinematics Approach for Linearized Buckling Analysis of Laminated Plates and Shells

✍ Scribed by D'Ottavio, M.; Carrera, E.


Book ID
125502082
Publisher
American Institute of Aeronautics and Astronautics
Year
2010
Tongue
English
Weight
332 KB
Volume
48
Category
Article
ISSN
0001-1452

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Sensitivity analysis and optimal design
✍ J.S Moita; J Infante Barbosa; C.M Mota Soares; C.A Mota Soares πŸ“‚ Article πŸ“… 2000 πŸ› Elsevier Science 🌐 English βš– 292 KB

A high order shear deformation theory is used to develop a discrete model for the sensitivity analysis and optimization of laminated plate and shell structures in non-linear response. The geometrically non-linear analysis is based on an updated Lagrangian formulation associated with the NewtonΒ±Raphs