Abstract
The influence of the reinforcement architecture on the fatigue behaviour of woven composites is evaluated. Glass/epoxy laminates with stacking sequence UD-woven-UD were produced with the woven layer at 0/90° and ± 45°. Plain and twill fabrics with the same matrix and fibres were used. The damage evolution was monitored during tension-tension fatigue tests, leading to a comparison between laminates based on life to crack initiation, crack growth and crack density evolution. The fatigue behaviour in terms of life to crack initiation was found to be predicted through local stresses in the matrix of the bundles, calculated using a recent multi-scale model.
Sign-in/Register to access full text options 
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 callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
