Nonlinear Shell Deflections With Thickness Updating
Abstract In the present investigation the incremental Hellinger-Reissner variational principle, a hybrid-strain based formulation and an updated Lagrangian formulation are adopted to derive explicit expressions for element stiffness matrices of various flat triangular shell finite elements. These elements are developed for application to the analysis of thin and thick shell structures undergoing large geometrically nonlinear deformation at finite strain. Correct representations of finite rotations and the specifically chosen strain field maintain appropriate rigid body motions and prevent shear locking phenomena. Consideration of thickness updating and a finite strain formulation relaxes any plane stress assumptions and enables the analyst to deal with three-dimensional constitutive models. Two numerical examples are presented to demonstrate the performance of the elements.