The present formulation offers a general method for analyzing the static re
sponse of geometrically-exact sandwich shells undergoing large deformation.
The layer directors at a point in the reference surface are connected to e
ach other by universal joints, and form a chain of rigid links. Finite rota
tions of the directors in every layer are allowed, with shear deformation i
ndependently accounted for in each layer. The thickness and the length of e
ach layer can be arbitrary, thus allowing the modeling of an important clas
s of multilayer structures having ply drop-offs. The present formulation is
thus suitable to model shell structures with patches of constrained viscoe
lastic materials or of piezoelectric materials. The nonlinear weak form of
the governing equations of equilibrium is constructed here, and then the li
nearization of the weak form and the associated inextensible directors upda
te are derived, leading to a symmetric tangent stiffness matrix. A Galerkin
finite element projection of the linearized equilibrium equations results
in a system of nonlinear algebraic equations, in which the interpolation ac
counts for the finite rotations of the directors. We present extensive nume
rical examples, including sandwich shells with three identical layers and p
ly drop-offs, to illustrate the applicability and versatility of the propos
ed formulation. (C) 2000 Elsevier Science S.A. All rights reserved.