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Civil-Comp Proceedings
ISSN 1759-3433 CCP: 106
PROCEEDINGS OF THE TWELFTH INTERNATIONAL CONFERENCE ON COMPUTATIONAL STRUCTURES TECHNOLOGY Edited by:
Paper 22
Buckling and Post-Buckling Behaviour of Shear-Deformable Composite Laminated Plates using an Exact Finite Strip Method H.R. Ovesy1, E. Zia-Dehkordi1 and S.A.M. Ghannadpour2
1Department of Aerospace Engineering, Centre of Excellence in Computational Aerospace Engineering, Amirkabir University of Technology, Tehran, Iran
H.R. Ovesy, E. Zia-Dehkordi, S.A.M. Ghannadpour, "Buckling and Post-Buckling Behaviour of Shear-Deformable Composite Laminated Plates using an Exact Finite Strip Method", in , (Editors), "Proceedings of the Twelfth International Conference on Computational Structures Technology", Civil-Comp Press, Stirlingshire, UK, Paper 22, 2014. doi:10.4203/ccp.106.22
Keywords: high accuracy strip, moderately thick plates, post-buckling stage, first order shear deformation plate theory, Von-Karman's equations, full-analytical finite strip method..
Summary
A high accuracy finite strip for the buckling and post-buckling analysis of
moderately thick composite plates is presented in this paper by using first order
shear deformation theory. The method presented, which is designated by the name
full-analytical finite strip method, provides an efficient and extremely accurate
buckling solution in which the Von-Karman's equilibrium set of equations is solved
exactly, and the out-of-plane mode shapes and critical loads are obtained. In the
post-buckling stage, the Von-Karman's compatibility equation is solved exactly with
the assumption that the deflected form after buckling is a combination of buckling
modes obtained (single or multiple mode shapes). The principle of minimum
potential energy is invoked to solve for the unknown coefficients in the assumed
out-of-plane deflection and rotations functions.
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