Abstract

In the present work, two woven carbon/epoxy laminates with different areal weight were tested under tension-compression (R = −1) and compression-compression (R = -∞) cyclic loadings. Their performance was evaluated in terms life to final separation and stiffness degradation during the fatigue life. In addition, microscopic observations were carried out at regular intervals during the tests to identify the damage evolution at the micro-scale. The bundle waviness was found to have a large influence on the damage mechanisms and the fatigue life of the laminates both for tension-compression and compression-compression loadings, while the stiffness loss remained small until final failure in all cases.

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

Disclaimer: 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.