BUCKLING OF ANGLE-PLY LAMINATED CIRCULAR CYLINDRICAL-SHELLS

被引：30

作者：

HIRANO, Y

机构：

[1] Department of Mechanical Engineering, Aeronautical Engineering and Mechanics, Rensselaer Polytechnic Institute, Troy, NY

来源：

JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME | 1979年 / 46卷 / 01期

关键词：

D O I：

10.1115/1.3424514

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

This Note presents closed-form solutions for axisymmetrical and axially unsymmetrical buckling of angle-ply laminated circular cylindrical shells under axial compression. The axisymmetrical and axially unsymmetrical buckling stress are found to be different from each other, and the best lamination angles which give the highest buckling stress are obtained. © 1979 by ASME.

引用

页码：233 / 234

页数：2