Research Article
Effect of Boundary Conditions on Buckling Load for Laminated Composite Plates
Osama Mohammed Elmardi Suleiman1*, Mahmoud Yassin Osman2 and Tagelsir Hassan3
1Federal University of Technology, Akure, Nigeria
2Department of Mechanical Engineering, Kassala University, Sudan
1Department of Mechanical Engineering, Omdurman Islamic University, Sudan
Osama Mohammed Elmardi Suleiman, Department of Mechanical Engineering, Nile Valley University, Atbara, River Nile, Sudan.
Received Date: March 27, 2019; Published Date: April 30, 2019
Abstract
It is observed that, for all cases the buckling load increases with the mode number but at different rates depending on whether the plate is simply supported, clamped or clamped – simply supported. The buckling load is a minimum when the plate is simply supported and a maximum when the plate is clamped. Because of the rigidity of clamped boundary condition, the buckling load is higher than in simply supported boundary condition. It is also observed that as the mode number increases, the plate needs additional support.
Keywords: Boundary conditions; Biaxial buckling; Classical laminated plate theory; Finite element; Fortran program; Composite laminated decks plates
-
Osama Mohammed Elmardi Suleiman, Mahmoud Yassin Osman, Tagelsir Hassan. Effect of Boundary Conditions on Buckling Load for Laminated Composite Plates. Glob J Eng Sci. 2(1): 2019. GJES.MS.ID.000527.
-
This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License.