Thermal buckling of hybrid angle-ply laminated composite plates with a hole
Yükleniyor...
Tarih
2005
Yazarlar
Dergi Başlığı
Dergi ISSN
Cilt Başlığı
Yayıncı
ELSEVIER SCI LTD
Erişim Hakkı
info:eu-repo/semantics/openAccess
Özet
In this paper, thermal buckling analysis of symmetric and antisymmetric laminated hybrid composite plates with a hole subjected to a uniform temperature rise for different boundary conditions is presented. The first-order shear deformation theory in conjunction with variational energy method is employed in mathematical formulation. The eight-node Lagrangian finite element technique is used for obtaining the thermal buckling temperatures of glass-epoxy/boron-epoxy hybrid laminates. The effects of hole size, layup sequences and boundary conditions on thermal buckling temperatures are investigated. The results are shown in graphical form for various boundary conditions. (c) 2005 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
65
Sayı
11.12.2020
