Concurrent topology and stacking sequence optimization of composite laminate plates using lamination parameters

Design engineers are constantly striving to minimize part weight, maximize stiffness, reduce cost, and optimize material usage. In this context, the use of composite materials provides an advantage when developing lightweight components because of their high strength to weight ratio and optimization potential. Most traditional topology optimization methods have been developed for isotropic materials and adapted to consider directiondependent materials only to define the optimum shape based on the fixed properties. Nevertheless, due to its anisotropic nature, a unidirectional composite mechanical response is highly dependent on the laminate stacking sequence, which is typically specified after the shape of the components has been defined. Therefore, new methods that can concurrently account for the shape and laminate orientation are essential for designing optimum composite structures. This article proposes a new density-based methodology for performing simultaneous topology optimization and stacking sequence optimization of constant stiffness laminated plates. In order to effectively achieve simultaneous placement of material and laminate lay-up, lamination parameters are used as design variables. Feasible domain equations are defined for lamination parameters and a laminate database concept is used for retrieving the lamination angles. Multiple example problems are provided to demonstrate the applicability of the proposed approach.

Automated summary

This article proposes a new density-based methodology for performing simultaneous topology optimization and stacking sequence optimization of constant stiffness laminated plates, providing a new approach for designing optimal composite structures.