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Tytuł artykułu

Ply thickness tolerances in stacking sequence optimization of multilayered laminate plates

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Treść / Zawartość
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Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
The paper deals with the impact of manufacturing tolerances of plies thicknesses on optimal design of multi-layered laminated plates in compression. It is assumed that the considered tolerances are represented by the maximum acceptable deviation of every individual ply thickness from its nominal design value. The robustness of the optimum is achieved diminishing the buckling load amplitude factor by the product of arbitrary assumed tolerances and appropriate sensitivities. The discussed optimization problem is solved numerically by the direct enumeration method. The proposed approach is illustrated with examples of the rectangular multi-layered laminated plate design under uni- and biaxial compression. The achieved results emphasise the robustness of the proposed method compared to the approaches with ignored tolerances.
Rocznik
Strony
1039--1052
Opis fizyczny
Bibliogr. 15 poz., rys., tab.
Twórcy
autor
  • Lublin University of Technology, Department of Applied Mechanics, Lublin, Poland
Bibliografia
  • 1. Adali A., Duffy K., 1990, Design of antisymetric hybrid laminates for maximum buckling load: I. Optimal fibre orientation, Composite Structures, 14, 1, 49-60
  • 2. Chryssanthopoulos M.K., Poggi C., 1995, Probabilistic imperfection sensitivity analysis of axially compressed composite cylinders, Engineering Structures, 17, 6, 398-406
  • 3. Fong M., Liu Y.P., Chan S.L., 2010, Second-order analysis and design of imperfect composite beam columns, Engineering Structures, 32, 6, 1681-1690
  • 4. Gutkowski W., Bauer J., 1999, Manufacturing tolerance incorporated in minimum weight design of trusses, Engineering Optimization, 31, 3, 393-403
  • 5. Gutkowski W., Latalski J., 2003,Manufacturing tolerances of fiber orientations in optimisation of laminated plates, Engineering Optimization, 35, 2, 201-213
  • 6. Haftka R.T., G¨urdal Z., Lamat M.P, 1990, Elements of Structural Optimization, 2nd Edition, Kluwer, Dordrecht
  • 7. Haftka R.T., Walsh J.L., 1992, Stacking-sequence optimization for buckling of laminated plates by integer programming, AIAA Journal, 30, 2, 814-819
  • 8. Jiang C., Han X., Liu G.P., 2008, Uncertain optimization of composite laminated plates using a nonlinear interval number programming method, Computers and Structures, 86, 17/18, 1696-1703
  • 9. Kogiso N., Shao S., Murotsu Y., 1997, Reliability-based optimum design of a symmetric laminated plate subject to buckling, Structural Optimization, 14, 2/3, 184-192
  • 10. Kristinsdottir B., Zabinsky Z., Tuttle M., Csendes T., Incorporating manufacturing tolerances in near-optimal design of composite structures, Engineering Optimization, 26, 1, 1-23
  • 11. Lee K.-H., Park G.-J., 2001, Robust optimization considering tolerances of design variables, Computers and Structures, 79, 1, 77-86
  • 12. Nemeth M.P., 1986, Importance of anisotropy on buckling of compression-loaded symmetric composite plates, AIAA Journal, 24, 11, 1831-1835
  • 13. Singh B.N., Yadav D., Iyengar N.G.R., 2001, Stability analysis of laminated cylindrical panels with uncertain material properties, Composite Structures, 54, 1, 17-26
  • 14. Walker M., Hamilton R., 2005, A methodology for optimally designing fibre-reinforced laminated structures with design variable tolerances for maximum buckling strength, Thin-Walled Structures, 43, 1, 161-174
  • 15. Walker M., Hamilton R., 2006, A technique for optimally designing fibre-reinforced laminated plates under in-plane loads for minimum weight with manufacturing uncertainties accounted for, Engineering with Computers, 21, 4, 282-288
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-42d31601-1f25-493a-b31d-9c57742a3ff5
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