An analytical solution for the contact between a rigid sphere and a th
in composite laminate supported on a rigid substrate is presented. The
contact force-deformation, including damage effects, is obtained from
an axisymmetric formulation of the contact problem. The material is a
ssumed to be transversely isotropic and following an elastic-perfectly
plastic stress-strain law. Damage is predicted using a maximum shear
failure criterion. Experimental data previously reported in the litera
ture agree well with the analysis.