The purpose of this work is to present some numerical results on nonlinear,
snap-through buckling of shallow spherical shells made of laminated compos
ite materials under general static loading. Isotropic shells are covered as
a special case of the general problem. A special-purpose finite-difference
computer program has been developed. Moreover, the general-purpose compute
r program ANSYS has also been used. Effects of various material properties
on the nonlinear behavior of the shells are investigated. One of the conclu
sions of the study is that ANSYS may yield erroneous results in some cases.
Another conclusion is that the buckling curves of composite shallow spheri
cal shells have a shape similar to that of the corresponding isotropic shel
l. This finding implies that the geometry of a shell may be an important fa
ctor in giving a characteristic shape to the buckling curve, at least for t
he shell parameters considered here.