The buckling of laminated cylindrical thin shells under torsion varying as a linear function of time

Sofiyev A. H., Zerin Z., Türkmen M.

Turkish Journal of Engineering and Environmental Sciences, cilt.27, sa.4, ss.237-245, 2003 (Scopus) identifier identifier

  • Yayın Türü: Makale / Tam Makale
  • Cilt numarası: 27 Sayı: 4
  • Basım Tarihi: 2003
  • Dergi Adı: Turkish Journal of Engineering and Environmental Sciences
  • Derginin Tarandığı İndeksler: Scopus, TR DİZİN (ULAKBİM)
  • Sayfa Sayıları: ss.237-245
  • Anahtar Kelimeler: Buckling, Dynamic critical load, Dynamic factor, Laminated, Orthotropic shell, Torsion, Wave numbers
  • Ondokuz Mayıs Üniversitesi Adresli: Evet

Özet

The buckling of laminated orthotropic cylindrical thin shells under torsion, which is a linear function of time, has been investigated. First, fundamental relations and the modified Donnell type stability equations of the laminated cylindrical thin shells are derived. Applying Galerkin's method, a differential equation having a variable coefficient depending on time is obtained and by applying the Ritz-type variational method to these equations, general formulas for static and dynamic critical loads, corresponding wave numbers and the dynamic factor are obtained. Finally after performing the computations, the effects of the variations of the numbers and ordering of layers, loading speed, and the ratio of radius to thickness on the critical parameters are investigated.