Abstract
In this study, several different types of delamination (partial debonding in the adhesive layers) were introduced in carbon fiber reinforced plastic (CFRP) laminated cantilever beams and then experimental measurements and finite element method (FEM) numerical analysis and simulation were applied to free vibration of those specimens made in this study. The experimental measurement showed that first bending mode frequencies and their modal loss factors varied when delaminations were introduced in the specimens. Distributions in each laminate with delamination of transverse shear strain energy and contact pressure were also obtained by FEM and then quantitatively examined.
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 callMore From: The Proceedings of the Dynamics & Design Conference
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.
