Nonlinear finite element analysis of composite shell under impact
Volume: 14, Issue: 6, Pages: 666 - 674
Published: Jun 1, 2000
Abstract
Large deflection dynamic responses of laminated composite cylindrical shells under impact are analyzed by the geometrically nonlinear finite element method based on a generalized Sander’s shell theory with the first order transverse shear deformation and the von-Karman large deflection assumption. A modified indentation law with inelastic indentation is employed for the contact force. The nonlinear finite element equations of motion of shell and...
Paper Details
Title
Nonlinear finite element analysis of composite shell under impact
Published Date
Jun 1, 2000
Volume
14
Issue
6
Pages
666 - 674
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