A numerical study was carried out to determine the suitability of a tw
o-dimensional approach for obtaining estimates of the fiber-bridging s
tress and the corresponding crack-tip stress intensity factors in crac
ked fiber-metal laminates (FML), when the delamination size and shape
between the prepeg and the metal layers of the laminate are known or a
ssumed. To this end, the boundary element method for two-dimensions is
employed, and the numerical results of the bridging stress and the st
ress intensity factor for range of parameters are compared with those
obtained from the corresponding three-dimensional finite element analy
sis. They show that reasonable estimates for these quantities can be o
btained when simple assumptions on the fiber-bridging stress distribut
ions are made.