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Civil-Comp Proceedings
ISSN 1759-3433 CCP: 40
ADVANCES IN OPTIMIZATION FOR STRUCTURAL ENGINEERING Edited by: B.H.V. Topping
Paper VI.2
Optimal Design of Laminated Composite Plates G. Giambanco, S. Rizzo and R. Spallino
Department of Structural Engineering and Geotechnics, University of Palermo, Palermo, Italy G. Giambanco, S. Rizzo, R. Spallino, "Optimal Design of Laminated Composite Plates", in B.H.V. Topping, (Editor), "Advances in Optimization for Structural Engineering", Civil-Comp Press, Edinburgh, UK, pp 143-147, 1996. doi:10.4203/ccp.40.6.2
Abstract
To the optimal design (OD) problem of laminated composite
plates many contributions have been already devoted. The
problem takes its significance only if all the constraints stated by
various serviceability and/or failure conditions are carefully
accounted for. In this paper this OD problem is formulated as a
constrained nonlinear mathematical programming (NLP) one.
Despite of the fact the objective function has been assumed as
linear combination of lamina1 thicknesses, which are the
continuous design variables, nonlinearity is yielded by the
implicit elastic formulation of composite laminates, and by the
assumed maximum admissible failure criterion. Other linear
constraints are also appended to the NLP approach, herein
presented accounting for technological (minimum lamina
thickness) requirements, and/or for assigned buckling load or
first modal frequency, and for serviceability maximum
displacement requirement. For this class of problems a method
of solution, the directional derivative method, has been
developed by the authors following the general criteria of the
feasible direction method. The feasible directions method was
preferred to the sequential unconstrained minimization
techniques (SUMT) for the better performance exhibited, since
SUMT often require a great number of function evaluation and
are then computationally expensive. A feasible direction method
possesses also the feature that each design point obtained
throughout the optimization process is a feasible one, and that
for each new design point the objective function will be reduced
(or incremented in problems of maximization). A design point is
called feasible if it lies in the feasible region, i.e., it does not
violate any constraint of the problem. The unicity of the
solution is assured if the problem is convex.
The OD procedure herein presented has been successfully tested by implementation to the optimal design of rectangular laminated composite plates with constraints on the center plate deflection. The numerical results obtained from a parametric study are presented and discussed. purchase the full-text of this paper (price £20)
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