Thermal buckling of rectangular laminated plates with a hole
Yükleniyor...
Dosyalar
Tarih
2005
Dergi Başlığı
Dergi ISSN
Cilt Başlığı
Yayıncı
SAGE PUBLICATIONS LTD
Erişim Hakkı
info:eu-repo/semantics/openAccess
Özet
Thermal buckling analysis of symmetric and antisymmetric laminated composite plates with clamped and simply supported edges, and containing a hole is presented in this paper. The first-order shear deformation theory in conjunction with the variational energy method is employed in mathematical formulation. The eight-node Lagrangian finite element technique is used to find thermal buckling temperatures of isotropic, glass-epoxy and boron-epoxy laminates. The effects of hole size, angle of ply orientation, lay-up sequences, and boundary conditions on thermal buckling temperatures are investigated. The result is shown in graphical forms for various boundary conditions.
Açıklama
Anahtar Kelimeler
composite plates, thermal buckling, finite element method
Kaynak
JOURNAL OF REINFORCED PLASTICS AND COMPOSITES
WoS Q Değeri
Q4
Scopus Q Değeri
Q1
Cilt
24
Sayı
3
