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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 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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