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Stacking sequence optimization of composite beams with different layer thicknesses

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Języki publikacji
EN
Abstrakty
EN
In this study, stacking sequence optimization of composite beams with different layer thicknesses is investigated for various boundary conditions. A unified shear deformation theory is used for analytical solution. The optimization process is carried out in order to obtain the minimum deflection parameters for Clamped-Free (C-F), Clamped-Clamped (C-C) and simply supported (S-S) boundary conditions under a uniform distributed load by use of genetic algorithm for a specific number of population and generation. Finally, among all possible combinations of layer thicknesses, the one giving the minimum deflection parameter and corresponding stacking sequence is chosen. The minimum values and corresponding stacking sequences are presented for different boundary conditions.
Twórcy
autor
  • Department of Mechanical Engineering, Faculty of Engineering, Trakya University, Edirne 22030, Turkey
autor
  • Department of Mechanical Engineering, Faculty of Engineering, Trakya University, Edirne 22030, Turkey
Bibliografia
  • 1. Walker M., Smith R.E.: A technique for the multiobjective optimisation of laminated composite structures using genetic algorithms and finite element analysis. Composite Structures, 62, 1, 2003, 123–128.
  • 2. Conti P., Luparello S., Pasta A.: Layer thickness optimisation in a laminated composite. Composites Part B, 28B, 1997, 309–317.
  • 3. Lee D.S., Morillo C., Bugeda G., Oller S., Onate E.: Multilayered composite structure design optimisation using distributed/parallel multi-objective evolutionary algorithms. Composite Structures, 94, 3, 2012, 1087–1096.
  • 4. Brighenti R.: Fibre distribution optimisation in fibre-reinforced composites by a genetic algorithm. Composite Structures, 71, 2005, 1–15.
  • 5. Khosravi P., Sedaghati R.: Design of laminated composite structures for optimum fiber direction and layer thickness, using optimality criteria. Structural and Multidisciplinary Optimization, 36, 2, 2008, 159–167.
  • 6. Soldatos K.P., Tımarcı T.: A unified formulation of laminated composite, shear deformable five-degrees-of-freedom cylindrical shell theories. Composite Structures, 25, 1993, 165–171.
  • 7. Timarci T., Soldatos K.P.: Comparative dynamic studies for symmetric cross-ply circular cylindrical shells on the basis of a unified shear deformable shell theory. Journal of Sound Vibration, 187, 4, 1995, 609–624.
  • 8. Karaçam F.: MSc. Thesis (In Turkish), Trakya University, Institute of Science, Turkey, Edirne, 2005.
  • 9. Goldberg D.E.: Genetic Algorithms in Search, Optimization and Machine Learning. Addison-Wesley Longman Publishing Co., Inc., USA, Boston, MA, 1989.
  • 10. Karama K.S., Afaq S., Mistou S.: Mechanical behaviour of laminated composite beam by the new multilayered laminated composite structures model with transverse shear stress continuity. International Journal of Solids and Structures, 40, 2003, 1525–1546.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-46b2fdd1-2eec-427c-b016-688e7830cb19
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