Thermal buckling of hybrid angle-ply laminated composite plates with a hole

Yükleniyor...
Küçük Resim

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

Künye