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This document presents a nonlinear finite element model for analyzing the large amplitude free vibrations of laminated composite cylindrical shell panels. The model uses high order shear deformation theory and incorporates geometric nonlinearity using the Green-Lagrange formulation. Finite element analyses are conducted to determine the effects of orthotropic ratios, thickness ratios, curvature ratios, boundary conditions, and amplitude ratios on the nonlinear natural frequencies of cylindrical shells. Equa

Author
Abdelali Yacoubi
Language
EN

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