Optimum design of laminated composite plates to maximize buckling load using MFD method

Topal U., Uzman U.

THIN-WALLED STRUCTURES, cilt.45, ss.660-669, 2007 (SCI-Expanded) identifier identifier

  • Yayın Türü: Makale / Tam Makale
  • Cilt numarası: 45
  • Basım Tarihi: 2007
  • Doi Numarası: 10.1016/j.tws.2007.06.002
  • Dergi Adı: THIN-WALLED STRUCTURES
  • Derginin Tarandığı İndeksler: Science Citation Index Expanded (SCI-EXPANDED), Scopus
  • Sayfa Sayıları: ss.660-669
  • Anahtar Kelimeler: laminated composite plates, FSDT, buckling loads, modified feasible direction method, optimal designs, OPTIMIZATION, SUBJECT
  • Karadeniz Teknik Üniversitesi Adresli: Evet

Özet

This paper presents optimal design of simply supported laminated composite plates subject to given in-plane static loads for which the critical failure mode is buckling. The objective function is to maximize the buckling load capacity of laminated plates and the fiber orientation is considered as design variable. The first-order shear deformation theory is used for the finite element analysis. In this paper, the effects of bending-twisting coupling are also included for the buckling optimization. The modified feasible direction method is used as an optimization method. Also, computer programs are coded in MATLAB and Golden Section method is adapted in this program for the optimal design of laminated plates for maximum buckling load. The effect of width-to-thickness ratio, aspect ratio, number of layers, material anisotropy, load ratios (N-y/N-x), uncertainties in material properties and functionally graded materials on the results is investigated and compared. (c) 2007 Elsevier Ltd. All rights reserved.