Abstract
Advanced fiber-reinforced laminated composite materials have been used for structural members in various fields, because of their high specific strength and stiffness. In the present paper, the thermal buckling problems of carbon fiber / epoxy (CFRP) cross-ply laminated cylindrical shells are considered. Buckling analysis is performed by assuming the buckling deformation that satisfy the boundary conditions and the equilibrium equation based on the Flugge-type expressions. The effects due to various factors such as lamination constitution, stacking sequence, number of layers and dimension of cylinders on the buckling temperature are clarified analytically.
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.
