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.

Full Text
Published version (Free)

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call