Thermal buckling behavior of cross-ply hybrid composite laminates with inclined crack
Küçük Resim Yok
Tarih
2006
Yazarlar
Dergi Başlığı
Dergi ISSN
Cilt Başlığı
Yayıncı
ELSEVIER SCI LTD
Erişim Hakkı
info:eu-repo/semantics/closedAccess
Özet
Thermal buckling analysis of symmetric and antisymmetric cross-ply laminated hybrid composite plates with an inclined crack subjected to a uniform temperature rise are presented in this paper. The first-order shear deformation theory in conjunction with variational energy method is employed in the mathematical formulation. The eight-node Lagrangian finite element technique is used for obtaining the thermal buckling temperatures of hybrid composite laminates. The effects of crack size and lay-up sequences on the thermal buckling temperatures for symmetric and antisymmetric plates are investigated. The results are shown in graphical form for various boundary conditions. (c) 2006 Elsevier Ltd. All rights reserved.
Açıklama
Anahtar Kelimeler
hybrid composite plates, thermal buckling, finite element method
Kaynak
COMPOSITES SCIENCE AND TECHNOLOGY
WoS Q Değeri
Q1
Scopus Q Değeri
Q1
Cilt
66
Sayı
15
