Using finite strain 3D‐material models in beam and shell elements

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A mixed shell formulation accounting for thickness strains and finite strain 3d material models (2008, methodology): “displacement u shell [4] solid shell [25] present 2/2/1 present 2/2/2”
A robust non‐linear mixed hybrid quadrilateral shell element (2005, unknown): “[41].”
Isogeometric Kirchhoff–Love shell formulations for general hyperelastic materials (2015, methodology): “Compressible materials For compressible materials, the plane stress condition S 33 = 0 is satisfied by iteratively solving for C33, using a Newton linearization of the plane stress condition similar to what was presented in [51, 52]:”