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Three-dimensional buckling analysis of laminated composite hollow cylinders and cylindrical panels

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Three-dimensional buckling analysis of laminated composite hollow cylinders and cylindrical panels. / Ye, Jianqiao; Soldatos, K P .
In: International Journal of Solids and Structures, Vol. 32, No. 13, 07.1995, p. 1949-1962.

Research output: Contribution to Journal/MagazineJournal articlepeer-review

Harvard

Ye, J & Soldatos, KP 1995, 'Three-dimensional buckling analysis of laminated composite hollow cylinders and cylindrical panels', International Journal of Solids and Structures, vol. 32, no. 13, pp. 1949-1962. https://doi.org/10.1016/0020-7683(94)00217-K

APA

Vancouver

Ye J, Soldatos KP. Three-dimensional buckling analysis of laminated composite hollow cylinders and cylindrical panels. International Journal of Solids and Structures. 1995 Jul;32(13):1949-1962. doi: 10.1016/0020-7683(94)00217-K

Author

Ye, Jianqiao ; Soldatos, K P . / Three-dimensional buckling analysis of laminated composite hollow cylinders and cylindrical panels. In: International Journal of Solids and Structures. 1995 ; Vol. 32, No. 13. pp. 1949-1962.

Bibtex

@article{a2d4ea28887244708c6c43bb87cba856,
title = "Three-dimensional buckling analysis of laminated composite hollow cylinders and cylindrical panels",
abstract = "The buckling problem of thick, cross-ply laminated cylinders and cylindrical panels under combined external loading is investigated on the basis of fully three-dimensional elasticity considerations. The three-dimensional pre-buckling stale that is initially employed, assumes zero shear stresses and is suitable for the analysis of both open panels and closed cylinders. This assumption leads to a set of three-dimensional linearized buckling equations. Both sets of three-dimensional prebuckling and buckling equations are then solved on the basis of a recursive method. The analysis is suitable for studying the buckling behavior of simply supported cross-ply cylinders, subjected to the single or the combined action of an axial compression and a uniform lateral pressure, or open cross-ply cylindrical panels under axial compression. The numerical results presented and discussed throughout this paper deal with cylinders and cylindrical panels having a symmetric or an antisymmetric cross-ply lay-up.",
author = "Jianqiao Ye and Soldatos, {K P}",
year = "1995",
month = jul,
doi = "10.1016/0020-7683(94)00217-K",
language = "English",
volume = "32",
pages = "1949--1962",
journal = "International Journal of Solids and Structures",
issn = "0020-7683",
publisher = "Elsevier Limited",
number = "13",

}

RIS

TY - JOUR

T1 - Three-dimensional buckling analysis of laminated composite hollow cylinders and cylindrical panels

AU - Ye, Jianqiao

AU - Soldatos, K P

PY - 1995/7

Y1 - 1995/7

N2 - The buckling problem of thick, cross-ply laminated cylinders and cylindrical panels under combined external loading is investigated on the basis of fully three-dimensional elasticity considerations. The three-dimensional pre-buckling stale that is initially employed, assumes zero shear stresses and is suitable for the analysis of both open panels and closed cylinders. This assumption leads to a set of three-dimensional linearized buckling equations. Both sets of three-dimensional prebuckling and buckling equations are then solved on the basis of a recursive method. The analysis is suitable for studying the buckling behavior of simply supported cross-ply cylinders, subjected to the single or the combined action of an axial compression and a uniform lateral pressure, or open cross-ply cylindrical panels under axial compression. The numerical results presented and discussed throughout this paper deal with cylinders and cylindrical panels having a symmetric or an antisymmetric cross-ply lay-up.

AB - The buckling problem of thick, cross-ply laminated cylinders and cylindrical panels under combined external loading is investigated on the basis of fully three-dimensional elasticity considerations. The three-dimensional pre-buckling stale that is initially employed, assumes zero shear stresses and is suitable for the analysis of both open panels and closed cylinders. This assumption leads to a set of three-dimensional linearized buckling equations. Both sets of three-dimensional prebuckling and buckling equations are then solved on the basis of a recursive method. The analysis is suitable for studying the buckling behavior of simply supported cross-ply cylinders, subjected to the single or the combined action of an axial compression and a uniform lateral pressure, or open cross-ply cylindrical panels under axial compression. The numerical results presented and discussed throughout this paper deal with cylinders and cylindrical panels having a symmetric or an antisymmetric cross-ply lay-up.

U2 - 10.1016/0020-7683(94)00217-K

DO - 10.1016/0020-7683(94)00217-K

M3 - Journal article

VL - 32

SP - 1949

EP - 1962

JO - International Journal of Solids and Structures

JF - International Journal of Solids and Structures

SN - 0020-7683

IS - 13

ER -