A simple beam theory for the buckling of symmetric composite beams including interaction of in-plane stresses

T. A. Morey, E. Johnson, C. K. Shield

Research output: Contribution to journalArticlepeer-review

8 Scopus citations

Abstract

A theory for symmetrically laminated, doubly-symmetric composite beams including the effects of anticlastic curvature is presented. Verification of the theory is demonstrated through comparisons with classical plate theory on the buckling loads for eight-layer symmetric angle-ply laminates caused by uniform compression and linearly distributed stress (lateral-torsional buckling). A significant reduction in buckling load is observed when the beams have many layers that are oriented between 25 and 60°C. Closed-form approximations for the new theory for rectangular beams are also presented and the theory is applied to box and I beams. These results show a reduction in the buckling load as compared to other beam theories for the box beams and for strong axis buckling of the I beams when there are many layers with lamination angles between 25 and 60°.

Original languageEnglish (US)
Pages (from-to)1321-1333
Number of pages13
JournalComposites Science and Technology
Volume58
Issue number8
DOIs
StatePublished - Aug 1998

Bibliographical note

Funding Information:
The work presented herein was funded by the National Science Foundation, grant No. CMS-9409526 and the University of Minnesota Graduate School under the McKnight Land-Grant Professorship program.

Copyright:
Copyright 2004 Elsevier Science B.V., Amsterdam. All rights reserved.

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