Optimum design of composite laminates for minimum thickness

  • Authors:
  • Mustafa Akbulut;Fazil O. Sonmez

  • Affiliations:
  • Department of Mechanical Engineering, Bogazici University, Istanbul, Bebek 34342, Turkey;Department of Mechanical Engineering, Bogazici University, Istanbul, Bebek 34342, Turkey

  • Venue:
  • Computers and Structures
  • Year:
  • 2008

Quantified Score

Hi-index 0.00

Visualization

Abstract

In this study, an optimization procedure is proposed to minimize thickness (or weight) of laminated composite plates subject to in-plane loading. Fiber orientation angles and layer thickness are chosen as design variables. Direct search simulated annealing (DSA), which is a reliable global search algorithm, is used to search the optimal design. Static failure criteria are used to determine whether load bearing capacity is exceeded for a configuration generated during the optimization process. In order to avoid spurious optimal designs, both the Tsai-Wu and the maximum stress criteria are employed to check static failure. Numerical results are obtained and presented for different loading cases.