Framework for the buckling optimisation of variable-angle-tow composite plates

Zhangming Wu, Gangadharan Raju, Paul M. Weaver

Research output: Contribution to journalArticle

65 Citations (Scopus)
183 Downloads (Pure)

Abstract

Variable-angle tow describes fibers in a composite lamina that have been steered curvilinearly. In doing so, substantially enlarged freedom for stiffness tailoring of composite laminates is enabled. Variable-angle tow composite structures have been shown to have improved buckling and postbuckling load-carrying capability when compared to straight fiber composites. However, their structural analysis and optimal design is more computationally expensive due to the exponential increase in number of variables associated with spatially varying planar fiber orientations in addition to stacking sequence considerations. In this work, an efficient two-level optimization framework using lamination parameters as design variables has been enhanced and generalized to the design of variable-angle tow plates. New explicit stiffness matrices are found in terms of component material invariants and lamination parameters. The convex hull property of B-splines is exploited to ensure pointwise feasibility of lamination parameters. In addition, a set of new explicit closed-form expressions defines the feasible region of two in-plane and two out-of-plane lamination parameters, which are used for the design of orthotropic laminates. Finally, numerical examples of plates under compression loading with different boundary conditions and aspect ratios are investigated. Reliable optimal solutions demonstrate the robustness and computational efficiency of the proposed optimization methodology.
Original languageEnglish
Pages (from-to)3788-3804
Number of pages17
JournalAIAA Journal
Volume53
Issue number12
Early online date30 Jul 2015
DOIs
Publication statusPublished - 1 Dec 2015

Keywords

  • buckling
  • optimisation methods
  • variable angle tow (VAT)
  • composite plates

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