As fiber-reinforced polymer (FRP) composites find application in highway br
idge structures, methodologies for describing their long-term performance u
nder service loading will be a necessity for designers. The designer of FRP
bridge structures will be faced with out-of-plane damage and delamination
at ply interfaces. The damage most often occurs between hybrid plys and dom
inates the lifetime response of a thick-section FRP structure. In this pape
r a model is developed to address these issues. The methodology employs the
quadratic delamination initiation failure criteria, in conjunction with a
delamination growth law to describe the out-of-plane damage under bending.
These phenomena are combined with the critical element residual strength li
fe prediction tool to determine remaining bending stiffness and moment capa
city of a pultruded and hybrid FRP 20.3-cm-deep structural shape. The model
successfully describes the onset of delamination prior to fiber failure an
d suggests that out-of-plane failure controls the life of the structure.