THERMAL BUCKLING OF CROSS-PLY COMPOSITE LAMINATES USING A 1ST-ORDER SHEAR DEFORMATION-THEORY

被引：34

作者：

ABRAMOVICH, H

机构：

[1] Faculty of Aerospace Engineering, Technion, Israel Institute of Technology, Haifa

来源：

COMPOSITE STRUCTURES | 1994年 / 28卷 / 02期

关键词：

D O I：

10.1016/0263-8223(94)90049-3

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

Thermal buckling of symmetric and non-symmetric cross-ply composite laminated beams is investigated based on a first-order shear deformation theory. Detailed analytical analysis is carried out for the thermal buckling parameter of laminated beams made out of Kevlar-epoxy, carbon-epoxy and glass-epoxy. The results are presented for various boundary conditions, lay-up sequences, slenderness ratios and transverse shear moduli.

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收藏

页码：201 / 213

页数：13

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