Composite pipes are increasingly used in demanding applications thanks to their light weight and corrosion resistance. To manage their integrity, tools able to predict their fatigue life and residual properties under cyclic loads are required. A finite element progressive fatigue model was applied to filament-wound composite pipes with a hole submitted to tensile cyclic fatigue. The fatigue model combined continuum damage mechanics for intra-laminar failure mechanisms and cohesive zone modelling for inter-laminar and selected macroscopic cracks. A linear fatigue damage accumulation law was used along with an empirical sudden-death residual strength model, relying solely on the material S-N curve. The fatigue simulation was conducted by an external cycle-jump procedure. After calibration on one load level, the model was able to describe the fatigue life at other load levels within one standard deviation (0.63 decade) of the experiments and resulted in a S-N curve slope of −0.084 while the experimental one was −0.072.
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