Abstract
This paper deals with the large deflection flexural vibration of unsymmetric cross-ply laminated plates which are simply supported at two opposite edges and clamped at the other two edges. Stress-free and movable in-plane boundary conditions are considered. Non-linear frequency is obtained as a function of lamination parameters, material constants, aspect ratio, linear frequency and amplitude of vibration. Non-linear frequency to linear frequency ratio versus amplitude curves are presented for isotropic, glass-epoxy, graphite-epoxy and boron-epoxy plates.
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.
