The buckling and postbuckling behavior of elastoplastic spherical shel
ls with circular apical, cutout under a ring load was investigated ana
lytically and experimentally. A finite element code based on the updat
ed Lagrangian formulation was established to analyze this buckling pro
blem by considering nonlinear geometric and material properties. An it
erative scheme controlled by displacement was adopted in the solution
procedure to avoid numerical instability near the limit buckling load.
Ring loads of both line and strip types were analyzed. A testing devi
ce was used to perform buckling experiments. The ratio of diameter to
thickness of the steel specimens was between 30.23 and 86.75. The infl
uence of the ratio of diameter to thickness and the sizes of the epica
l cutout and ring load on the limit buckling load are discussed. The a
nalytical results agree satisfactorily with experimental ones for medi
um carbon steel spherical shells, Convex and concave modes of postbuck
ling deformation around the apex are obtained in analysis and observed
in experiment for varied combinations of the sizes of ring load and a
pical cutout and ratio of diameter to thickness of the spherical shell
s.