Local buckling loads of sandwich panels made with laminated faces

被引：24

作者：

Aiello, MA ^{[1
]}

Ombres, L ^{[1
]}

机构：

[1] Univ Lecce, Dept Mat Sci, I-73100 Lecce, Italy

来源：

COMPOSITE STRUCTURES | 1997年 / 38卷 / 1-4期

关键词：

D O I：

10.1016/S0263-8223(97)00055-X

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

The paper is devoted to assessing the optimal arrangements of hybrid laminated faces of sandwich panels in order to maximize local buckling loads corresponding to the wrinkling of compressed faces. The analysis is carried out by modelling compressed faces as thin unsymmetric laminates resting on elastic two-parameter foundations. The First-order Shear Deformation Theory, in conjunction with the Rayleigh-Ritz method, has been used to evaluate buckling loads of simply supported flat laminates subjected to in-plane biaxial compression and shear forces. A numerical investigation is intended to support evidence for the influence of laminate parameters (fibre orientation, geometrical dimensions) and foundation parameters (modulus of subgrade reaction and shear modulus); obtained results are reported and discussed in the paper. (C) 1997 Elsevier Science Ltd.

引用

页码：191 / 201

页数：11

共 13 条

[1] Maximum buckling loads for unsymmetric thin hybrid laminates under in-plane and shear forces [J].