The bending behaviour of axisymmetric laminated composite shells with a cut
out has been investigated using the finite element method based on a higher
-order shear deformation theory. The governing equations and the finite ele
ment formulation are presented in Part I. Results are presented showing the
distributions of deflection and stresses in orthotropic and laminated symm
etric/anti-symmetric axisymmetric spherical shells with a central circular
cutout with simply supported and clamped boundary conditions subjected to u
niform normal pressure. (C) 2000 Elsevier Science Ltd. All rights reserved.