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Civil-Comp Proceedings
ISSN 1759-3433
CCP: 67
COMPUTATIONAL TECHNIQUES FOR MATERIALS, COMPOSITES AND COMPOSITE STRUCTURES
Edited by: B.H.V. Topping
Paper VIII.5

The Effect of Stiffeners on the Optimal Design of Laminated Plates Subject to Buckling Loads: A Comparative Study

M. Walker

Center for Advanced Materials, Design and Prototyping Research, Technikon Natal, Durban, South Africa

Full Bibliographic Reference for this paper
M. Walker, "The Effect of Stiffeners on the Optimal Design of Laminated Plates Subject to Buckling Loads: A Comparative Study", in B.H.V. Topping, (Editor), "Computational Techniques for Materials, Composites and Composite Structures", Civil-Comp Press, Edinburgh, UK, pp 349-358, 2000. doi:10.4203/ccp.67.8.5
Abstract
Optimal designs of symmetrically laminated rectangular plates with different stiffener layouts are presented. The plates are subject to a combination of simply supported, clamped and free boundary conditions, and the design objective is the maximisation of the biaxial buckling load. This is achieved by determining the fibre orientations optimally with the effects of bending-twisting coupling taken into account. Square tubing is used as stiffeners, and the finite element method coupled with ail optimisation routine is employed in analysing and optimising the laminated plate designs. The effect of the stiffener layout and boundary conditions on the optimal ply angles and the buckling load are numerically studied. It is demonstrated that in some cases, stiffeners call sometimes reduce, rather than increase the buckling strength of an optimally designed plate.

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