Computational & Technology Resources
an online resource for computational,
engineering & technology publications |
|
Civil-Comp Proceedings
ISSN 1759-3433 CCP: 91
PROCEEDINGS OF THE TWELFTH INTERNATIONAL CONFERENCE ON CIVIL, STRUCTURAL AND ENVIRONMENTAL ENGINEERING COMPUTING Edited by: B.H.V. Topping, L.F. Costa Neves and R.C. Barros
Paper 18
The Effect of Local Geometric Imperfections on the Non-Linear Analysis of Stub Columns M.M. Pastor, M. Casafont, F. Roure and M. Ferrer
Department of Strength of Materials and Structural Engineering, School of Industrial Engineering of Barcelona (ETSEIB), Universitat Politècnica de Catalunya (UPC), Barcelona, Spain M.M. Pastor, M. Casafont, F. Roure, M. Ferrer, "The Effect of Local Geometric Imperfections on the Non-Linear Analysis of Stub Columns", in B.H.V. Topping, L.F. Costa Neves, R.C. Barros, (Editors), "Proceedings of the Twelfth International Conference on Civil, Structural and Environmental Engineering Computing", Civil-Comp Press, Stirlingshire, UK, Paper 18, 2009. doi:10.4203/ccp.91.18
Keywords: geometric imperfections, local buckling, cold-formed members, pallet-rack profiles, non-linear analysis, finite element.
Summary
This research focuses on short columns subject to compression. The purpose of this paper is to analyse sensitivity to different geometric imperfection magnitudes of the non-linear finite element analysis. Twenty open cold-formed steel sections have been analysed, with a nominal thickness range of 1.0 to 2.5 mm.
Experimental tests on the 20 sections have been carried out in our laboratory. As a general rule, five tests are needed for each section in order to find the position of the effective centre of gravity [1]. As local buckling usually occurs within tested lengths, the typically recommended geometric imperfection values for this mode have been applied to the finite element models. Three different magnitudes have been analysed: w/200, 0.006w, and w/100. The study is carried out with the intention of seeing how the finite element analyses are affected depending on which imperfection value has been chosen. A parametric finite element model has been created [2]. On a particular node of the outer face of both load plates, the displacements are prescribed. The material behaviour has been reproduced by means of an elastic-plastic bi-linear model. In the first step, an elastic (linear) buckling analysis was carried out on a perfect mesh to obtain its deformed shape (eigenvalue) in the critical buckling mode. This deformed shape indicates the possible buckling mode of the specimen and is introduced as a starting point for the second step: the non-linear analysis. The displacement is increased in successive increments until the maximum load is reached and it clearly begins to decrease or remains constant for a significant increment of displacement. The simulation is repeated, displacing the load node along the symmetry line in increments of 1 mm. The following conclusions have been drawn from this study:
References
purchase the full-text of this paper (price £20)
go to the previous paper |
|