Adhesive bonding between different materials has been widely used for a large variety of
applications, such as in the aircraft, automotive, and many other civil engineering structures.
Adhesive-bonded joints as load bearing components have the potential to save significant weight and
cost over conventional riveted or bolted joints. For the last ten years a major problem in adhesive
technology has been the difficulty in predicting the accurate load bearing capacity of a joint. This
difficulty comes from the fact that the stress distribution in the adhesive joint is very complex and
singular stress field exists at the bi-material corner. And for bonded joints, the failure usually occurs at
the adhesive/adherend interface. Therefore another difficulty comes from the complex interfacial
failure analysis due to the formation of chemical bonds, whose strengths are difficult to measure.
Many studies have been conducted to investigate the effects of bond thickness, material properties of
adhesives and adherends, and geometric shape of bi-material corner tip to the fracture behavior of
bonded joints. In this paper, we analyze the stress fields at the interface corner of
composite/steel(anisotropic/isotropic) double lap joint to predict failure by using stress intensity
based fracture criterion. And analytical results are compared with experimental results of co-cured lap
joints under tensile load condition. Micro-structural features, hardness characteristics, and fracture
toughness determinations of the interfaces are also conducted.