The bending behaviour of fibre reinforced plastic laminated shells without
a cutout has been studied using the finite element method based on a higher
-order shear deformation theory. The higher-order shear deformation theory
is derived by assuming that the transverse displacement is constant through
the thickness of the shell. An eight-noded degenerated isoparametric shell
element is considered with nine degrees of freedom at each node. Results a
re presented showing the variation of deflection and stresses in orthotropi
c and laminated symmetric/anti-symmetric spherical shell panels with simply
supported and clamped boundary conditions subjected to uniform normal pres
sure. (C) 2000 Elsevier Science Ltd. All rights reserved.