The modeling of damage in a laminated composite pinned-joint presents
many difficulties because of the inherent complexity of the failure pr
ocess. The joint area is a region with stress concentrations thus a co
mplicated stress state exists. In order to model progressive damage fr
om initial to final failure, finite element methods are used rather th
an closed form stress analyses. Two approaches for the finite element
technique can be used: a simple two-dimensional linear model or one th
at has been enhanced with non-linear assumptions. Adding non-linear ma
terial behaviour and large deformation theory are two improvements tha
t can be made to a linear finite element model. Failure analysis must
be a logical combination of suitable failure criteria and appropriate
material property degradation rules. It is understood that a three-dim
ensional analysis may now be a better alternative, but the goal here i
s to fully understand the limits of two-dimensional modeling for solvi
ng the composite pinned-joint problem.