Design of a laminated composite variable curvature panel under uniaxial compression

Cagdas I., ADALI S.

ENGINEERING COMPUTATIONS, cilt.29, sa.1-2, ss.48-64, 2012 (SCI-Expanded) identifier identifier

  • Yayın Türü: Makale / Tam Makale
  • Cilt numarası: 29 Sayı: 1-2
  • Basım Tarihi: 2012
  • Doi Numarası: 10.1108/02644401211190564
  • Dergi Adı: ENGINEERING COMPUTATIONS
  • Derginin Tarandığı İndeksler: Science Citation Index Expanded (SCI-EXPANDED), Scopus
  • Sayfa Sayıları: ss.48-64
  • Anahtar Kelimeler: Optimum design, Composite materials, Laminates, Variable curvature panel, First-ply failure, Buckling, Finite element method, STACKING-SEQUENCE OPTIMIZATION, CYLINDRICAL PANELS, BUCKLING OPTIMIZATION, BEHAVIOR
  • Akdeniz Üniversitesi Adresli: Evet

Özet

Purpose - The purpose of this paper is to present the optimal design of a simply supported variable curvature laminated angle-ply composite panel under uniaxial compression. The objective is to maximize the failure load which is defined as the minimum of the buckling load and the first-ply failure load.