Design of composite laminates for optimum frequency response

In this study, natural frequency response of symmetrically laminated composite plates was optimized. An analytical model accounting for bending–twisting effects was used to determine the laminate natural frequency. Two different problems, fundamental frequency maximization and frequency separation maximization, were considered. Fiber orientation angles were chosen as design variables. Because of the existence of numerous local optimums, a global search algorithm, a variant of simulated annealing, was utilized to find the optimal designs. Results were obtained for different plate aspect ratios. Effects of the number of design variables and the range of values they may take on the optimal frequency were investigated. Problems in which fiber angles showed uncertainty were considered. Optimal frequency response of laminates subjected to static loads was also investigated.

► In this study, natural frequency response of composite plates is optimized. ► Natural frequency is analytically determined accounting for bending–twisting effects. ► A new variant of simulated annealing is used to find the globally optimal designs. ► Fiber angles are considered as random variables. ► Optimal frequency response of laminates subjected to static loads is also investigated.