ScienceDirect® Home Skip Main Navigation Links
You have guest access to ScienceDirect. Find out more.
 
Home
Browse
My Settings
Alerts
Help
 Quick Search
 Search tips (Opens new window)
    Clear all fields    
advertisementadvertisement
Computers & Structures
Volume 56, Issue 6, 17 September 1995, Pages 1009-1017
 
Font Size: Decrease Font Size  Increase Font Size
 Abstract - selected
Purchase PDF (719 K)

 
 
 
Related Articles in ScienceDirect
View More Related Articles
 
View Record in Scopus
 
doi:10.1016/0045-7949(94)00572-K    How to Cite or Link Using DOI (Opens New Window)
Copyright © 1995 Published by Elsevier Science Ltd.

Finite elements for post-buckling analysis. I—The W-formulation

L. A. Godoy, E. J. Barbero and I. G. Raftoyiannis

Mechanical and Aerospace Engineering, Constructed Facilities Center, West Virginia University, Morgantown, WV 26506-6106, U.S.A.

Received 3 February 1994. 
Available online 5 April 2000.

Purchase the full-text article



References and further reading may be available for this article. To view references and further reading you must purchase this article.

Abstract

This paper presents a convenient formulation for the stability analysis of structures using the finite element method. The main assumptions are linear elasticity, a linear fundamental path, and the existence of distinct critical loads (i.e. no coupling between buckling modes occurs). The formulation developed is known as W-formulation, in which the energy is written in terms of a sliding set of incremental coordinates measured with respect to the fundamental path. In the presentation developed here, the only ingredients required to carry out the analysis are the strain-displacement and the constitutive matrices at the element level. The present formulation is compared with the so called V-formulation, in which the displacements refer to the unloaded state. It is shown that under the present assumptions of linear fundamental path, the advantages of the V-formulation are lost and both approaches are similar. An example of a circular plate under in-plane loading illustrates the procedures. Part II of this paper deals with the application to the post buckling analysis of plate assemblies made of composite materials.

Article Outline

• References

Computers & Structures
Volume 56, Issue 6, 17 September 1995, Pages 1009-1017
 
Home
Browse
My Settings
Alerts
Help
Elsevier.com (Opens new window)
About ScienceDirect  |  Contact Us  |  Information for Advertisers  |  Terms & Conditions  |  Privacy Policy
Copyright © 2008 Elsevier B.V. All rights reserved. ScienceDirect® is a registered trademark of Elsevier B.V.