Journal of Composite Materials

 

Advanced Search

Journal Navigation

Journal Home

Subscriptions

Archive

Contact Us

Table of Contents

Register here to gain access to SAGE's 500+ Journals Online

Sign In to gain access to subscriptions and/or personal tools.
This Article
Right arrow Full Text (PDF)
Right arrow References
Right arrow Alert me when this article is cited
Right arrow Alert me if a correction is posted
Services
Right arrow Email this article to a friend
Right arrow Similar articles in this journal
Right arrow Alert me to new issues of the journal
Right arrow Add to Saved Citations
Right arrow Download to citation manager
Right arrowRequest Permissions
Right arrow Request Reprints
Right arrow Add to My Marked Citations
Citing Articles
Right arrow Citing Articles via HighWire
Right arrow Citing Articles via Google Scholar
Google Scholar
Right arrow Articles by Barbero, E. J.
Right arrow Articles by Davalos, J. F.
Right arrow Search for Related Content
Social Bookmarking
 Add to CiteULike   Add to Connotea   Add to Del.icio.us   Add to Digg   Add to Reddit   Add to Technorati  
What's this?
Journal of Composite Materials, Vol. 27, No. 8, 806-829 (1993)
DOI: 10.1177/002199839302700804

On the Mechanics of Thin-Walled Laminated Composite Beams

Ever J. Barbero

West Virginia University Morgantown, WV 26506-6101

Roberto Lopez-Anido

West Virginia University Morgantown, WV 26506-6101

Julio F. Davalos

West Virginia University Morgantown, WV 26506-6101

A formal engineering approach of the mechanics of thin-walled laminated beams based on kinematic assumptions consistent with Timoshenko beam theory is pre sented. Thin-walled composite beams with open or closed cross section subjected to bend ing and axial load are considered. A variational formulation is employed to obtain a com prehensive description of the structural response. Beam stiffness coefficients, which account for the cross section geometry and for the material anisotropy, are obtained. An explicit expression for the static shear correction factor of thin-walled composite beams is derived from energy equivalence. A numerical example involving a laminated I-beam is used to demonstrate the capability of the model for predicting displacements and ply stresses.


Add to CiteULike CiteULike   Add to Connotea Connotea   Add to Del.icio.us Del.icio.us   Add to Digg Digg   Add to Reddit Reddit   Add to Technorati Technorati    What's this?


This article has been cited by other articles:


Home page
Journal of Reinforced Plastics and CompositesHome page
H. A. Salim and J. F. Davalos
Shear Lag of Open and Closed Thin-walled Laminated Composite Beams
Journal of Reinforced Plastics and Composites, May 1, 2005; 24(7): 673 - 690.
[Abstract] [PDF]


Home page
Journal of Composite MaterialsHome page
H. A. Salim and J. F. Davalos
Torsion of Open and Closed Thin-Walled Laminated Composite Sections
Journal of Composite Materials, March 1, 2005; 39(6): 497 - 524.
[Abstract] [PDF]


Home page
Journal of Reinforced Plastics and CompositesHome page
N. Arlsan, H. Pihtili, and M. Gur
Elasto-Plastic Stress Analysis of Thermoplastic Matrix Composite Laminated and Perforated Plates under In-Plane Loading
Journal of Reinforced Plastics and Composites, September 1, 2001; 20(14-15): 1222 - 1252.
[Abstract] [PDF]


Home page
Journal of Reinforced Plastics and CompositesHome page
S. S. Sonti and E. J. Barbero
Material Characterization of Pultruded Laminates and Shapes
Journal of Reinforced Plastics and Composites, July 1, 1996; 15(7): 701 - 717.
[Abstract]