Cylindrical Buckling Load of Laminated Columns
- 1 March 1989
- journal article
- Published by American Society of Civil Engineers (ASCE) in Journal of Engineering Mechanics
- Vol. 115 (3) , 659-661
- https://doi.org/10.1061/(asce)0733-9399(1989)115:3(659)
Abstract
The cylindrical buckling load of a composite laminated column is derived from plate theory. The effect of lamina orientation is taken into account by treating the stiffness parameter as a matrix product rather than as a single value drawn from the definition of the elastic coefficients. This refined stiffness parameter leads to significant improvement of the buckling load, depending on the stacking combination and orientation.Keywords
This publication has 1 reference indexed in Scilit:
- Nonlinear analysis of axially-loaded laminated cylindrical shellsComputers & Structures, 1983