50th Anniversary Article: Review on Interface Fracture and Delamination of Composites

ABSTRACT In this review paper, a methodology for measuring the interface fracture toughness of a crack between two isotropic, homogeneous materials and a delamination between two laminae of unidirectional composite materials of differing directions is presented. Four cases are considered. Two isotropic material pairs are described: glass/epoxy and two ceramic clays. Similar studies are presented for two cross‐ply laminates: 0°/90° and +45°/−45. The Brazilian disk specimen was used to carry out mixed mode fracture tests. The load and crack or delamination length at fracture were measured and used in a finite element analysis to determine the displacement field. An interaction energy orM‐integral was used to obtain the stress intensity factors at failure. These in turn were employed to calculate the critical interface energy release rateand two phase anglesψandφ, which measure the mode mixity. For theM‐integral and for each interface crack or delamination, the first term of the asymptotic solution of the fields is required. For two isotropic materials, these solutions are well known. For the laminates described here, they were determined by the Stroh and Lekhnittski formalisms. A failure criterion determined from first principles is presented. The values of,ψandφare used to specify the criterion for each material pair. A statistical analysis is presented, which predicts a 5% probability of failure.