In this paper, the fracture behavior of a pressure vessel involving a full circumferential wall crack at the inner surface is investigated by applying the axisymmetric model. By using the extended finite element method (X-FEM), the stress intensity factor is calculated and compared for the case of a crack in the Aluminum monolayer cylinder as well as when the composite coating is mounted on its outer surface. Also, the stress intensity factor is obtained for different crack lengths, materials, and fiber orientations in the composite laminate. The materials of composite laminate are Glass-epoxy and Carbon-epoxy. An axisymmetric extended finite element formulation is developed for the pressure vessel, and a MATLAB programming code is implemented to solve the problem. To validate the developed code, two examples are solved and compared with the available results of two-level finite element method (2LFEM) and exact solutions. The results obtained from the axisymmetric X-FEM model is in good agreement with the existing results. The results show that the most reduction of SIFs occurred in pressure vessels with the Carbon-epoxy coating with 0° fiber orientation. • An axisymmetric X-FEM model is developed for calculation of stress intensity factors (SIFs) in cracked pressure vessel. • An interaction integral is used for the computation of mixed-mode SIFs. • The effect of Glass-epoxy and Carbon-epoxy coating of pressure vessel on SIFs is investigated. • The effect of different fiber orientations of composite coating on SIFs is investigated. • The most reduction of SIFs occurred in pressure vessels with the Carbon-epoxy coating with hoop (0°) fiber orientation.
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