BUCKLING OF MODERATELY THICK COMPOSITE PLATES

被引：8

作者：

BRUNO, D

LATO, S

机构：

[1] Department of Structures, University of Calabria, Arcavacata di Rende, Cosenza

来源：

COMPOSITE STRUCTURES | 1991年 / 18卷 / 01期

关键词：

D O I：

10.1016/0263-8223(91)90014-P

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

In this paper an analysis of the buckling behaviour of anisotropic elastic plates is developed. The analysis is carried out by using a finite-element technique based on a shear-deformable plate model. Numerical results are also given relative to buckling of laminated plates under uniform axial compression, together with some comparisons with previous results available in the literature.

引用

页码：65 / 75

页数：11

共 8 条

[1]

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[2]

Chia, Nonlinear Analysis of Plates, (1980)

[3]

Harris, The buckling and postbuckling behaviour of composite plates under biaxial loading, Int. J. Mech. Sci., 17, pp. 187-202, (1975)

[4]

Hui, Imperfections sensitivity of axially compressed laminated flat plates due to bending-stretching coupling, Int. J. Sol. Struct., 22, pp. 13-22, (1986)

[5]

Whitney, Jones, Morgan, Buckling and vibration of antisymmetrically laminated angle-ply rectangular plates, J. Appl. Mech., pp. 1143-1144, (1973)

[6]

Librescu, Schmidt, Refined theories of elastic anisotropic shells accounting for small strains and moderate rotations, Int. J. Nonlinear Mech., 23, pp. 217-229, (1988)

[7]

Reddy, A small strain and moderate rotation theory of elastic anisotropic plates, J. Appl. Mech., 54, pp. 623-626, (1987)

[8]

Budiansky, Theory of buckling and postbuckling behaviour of elastic structures, Advances in Applied Mechanics, 14, (1974)

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