Show simple item record

contributor authorIzhak Sheinman
date accessioned2017-05-08T22:24:15Z
date available2017-05-08T22:24:15Z
date copyrightMarch 1989
date issued1989
identifier other%28asce%290733-9399%281989%29115%3A3%28659%29.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/79830
description abstractThe 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.
publisherAmerican Society of Civil Engineers
titleCylindrical Buckling Load of Laminated Columns
typeJournal Paper
journal volume115
journal issue3
journal titleJournal of Engineering Mechanics
identifier doi10.1061/(ASCE)0733-9399(1989)115:3(659)
treeJournal of Engineering Mechanics:;1989:;Volume ( 115 ):;issue: 003
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record