A three-node, Co-type, layered flat-shell finite element is developed for t
he analysis of large elastic-plastic deformations in plate and shell struct
ures. The system equations are derived by using virtual work principle and
the updated Lagrangian formulation. Material is assumed to be isotropic and
rate insensitive obeying J(2)-flow rule. The displacement field assumption
of the MIN3 plate bending element is employed. A layered structure is used
to model through-the-thickness distribution of elastic and plastic zones.
The finite element results for three nonlinear plate bending problems are c
ompared with experimental results to verify the accuracy of the formulation
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