An engineering approach to fracture load predictions for adhesive join
ts is presented. The approach is based on the premise that the in-situ
strength of the bondline can be characterized by the fracture envelop
e (critical energy release rate as a function of the mode of. loading)
, for a specific adhesive system. By using the J integral for large de
formations together with large-deformation beam theory, a simple close
d-form expression is obtained for the energy release rate per unit are
a extension when a crack propagates in the bondline of a generalized a
dhesive joint (adhesive sandwich). This technique, together with a pub
lished method for mode partitioning, enables fracture load prediction
by comparing the calculated fracture parameters with the critical ones
from the fracture envelope. The approach is shown to predict fracture
loads accurately for a variety of joints including the cracked lap sh
ear (CLS), the single lap shear (SLS) and the double strap (DS) joint.