Abstract
A two-parameter model based on strength degradation was developed and its predictive reliability was checked on a series of fatigue life and residual strength data available in the literature. The modelling approach explicitly accounts for the maximum cyclic stress, \(\sigma_{\max}\), and the stress ratio, \(R= \sigma_{\min} /\sigma_{\max}\), and requires a limited number of experimental fatigue life data to predict the cycle-by-cycle strength degradation kinetics until the “sudden drop” of strength before catastrophic failure. Different loading conditions were analysed for a large variety of composites, including short-glass-fibre-reinforced polycarbonate, \([\pm45]_{\mathrm{S}}\) glass/epoxy laminates, \([\pm35]_{2\mathrm{S}}\) graphite/epoxy laminates, AS4 carbon/epoxy 3k/E7K8 plain weave fabric with [45/−45/90/45/−45/45/−45/0/45/−45]S layup, and [CSM/fabric/(CSM/UD)2]S glass/polyester laminate. The modelling approach indicates that the fatigue life and the residual strength are related to the statistical distribution of the static strength.
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