Strength analysis of carbon fiber reinforced polymer and titanium alloy for axisymmetric lap joint

Many industries such as oil, gas, aerospace, and automotive, use axisymmetric adhesively bonded single lap joints. Different materials are frequently mated using When composite adherents delaminate, the stress circulation inside adhesive layer significantly influenced. As a result, importance of considering stresses in presence considerable delamination is investigated this paper. To understand analysis examine bond strength at static loading conditions, model created finite element with cohesive zone modelling. A complete parametric study carried simple code ABAQUS, joins joints prepared different material adherents. Analysis on influence numerous factors distribution In connection, mating carbon reinforced polymer to titanium alloy adherends discussed thoroughly. The results show that depending position delamination, throughout-the-thickness affects structural response both by varying overlap length. reduced peel shear joint configurations.