Buckling optimization of composite laminated adaptive structures

This paper deals with the optimal design of laminated composite plates with integrated piezoelectric actuators. Refined finite element models based on equivalent single layer high-order shear deformation theories are used. These models are combined with simulated annealing, a stochastic global optimization technique, in order to find the optimal location of piezoelectric actuators and also to find the optimal fiber reinforcement angles in both cases having the objective of maximizing the buckling load of the composite adaptive plate structure. To show the performance of the proposed optimization models, two illustrative and simple examples are presented and discussed. In one of these examples a comparison between the simulated annealing technique and a gradient based optimization scheme, is carried out.

[1]  Garret N. Vanderplaats,et al.  Numerical Optimization Techniques for Engineering Design: With Applications , 1984 .

[2]  Carlos A. Mota Soares,et al.  Optimization of multilaminated structures using higher-order deformation models , 1997 .

[3]  Hui-Shen Shen Postbuckling of laminated cylindrical shells with piezoelectric actuators under combined external pressure and heating , 2002 .

[4]  Sérgio Frascino Müller de Almeida,et al.  Enhancement of pre-buckling behavior of composite beams with geometric imperfections using piezoelectric actuators , 1999 .

[5]  Barry Hilary Valentine Topping,et al.  Parallel simulated annealing for structural optimization , 1999 .

[6]  Afzal Suleman,et al.  Modelling and design of adaptive composite structures , 2000 .

[7]  Scott Kirkpatrick,et al.  Optimization by simulated annealing: Quantitative studies , 1984 .

[8]  Sarp Adali,et al.  Developments in thermopiezoelasticity with relevance to smart composite structures , 2000 .

[9]  C. D. Gelatt,et al.  Optimization by Simulated Annealing , 1983, Science.

[10]  Tarun Kant,et al.  A critical review and some results of recently developed refined theories of fiber-reinforced laminated composites and sandwiches , 1993 .

[11]  J. Loughlan,et al.  Buckling control using embedded shape memory actuators and the utilisation of smart technology in future aerospace platforms , 2002 .

[12]  Romesh C. Batra,et al.  Enhancement of the dynamic buckling load for a plate by using piezoceramic actuators , 2001 .

[13]  Mir M. Atiqullah,et al.  SIMULATED ANNEALING AND PARALLEL PROCESSING: AN IMPLEMENTATION FOR CONSTRAINED GLOBAL DESIGN OPTIMIZATION , 2000 .

[14]  J. Herskovits Feasible Direction Interior-Point Technique for Nonlinear Optimization , 1998 .

[15]  Carlos A. Mota Soares,et al.  Refined models for the optimal design of adaptive structures using simulated annealing , 2001 .

[16]  J. Reddy Mechanics of laminated composite plates and shells : theory and analysis , 1996 .

[17]  K. Chandrashekhara,et al.  Active buckling control of smart composite plates-finite-element analysis , 1993 .