Abstract
The present paper treats the optimal design problems of laminated composite plates and shells based upon the netting theory in which the stiffnesses other than the longitudinal Young's modulus are neglected. Some stiffness characteristics are examined, that is, the vibration and buckling characteristics of laminated composite plates and the buckling characteristics of laminated composite cylindrical shells. Optimal laminate configurations for the vibration and the buckling are also obtained by using the netting theory and compared with the results based upon the lamination theory. Applicability and limitation of the netting theory to the laminated plates and shells are verified through the numerical examples.
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: Journal of the Japan Society for Composite Materials
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.
