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Behaviour and Design of Composite Beams Subjected to Negative Bending and Axial Compression

Authors :
Brendan Kirkland
George Vasdravellis
Ee Loon Tan
Brian Uy
Source :
Proceedings of the 10th International Conference on Advances in Steel Concrete Composite and Hybrid Structures.
Publication Year :
2012
Publisher :
Research Publishing Services, 2012.

Abstract

article i nfo This paper investigates the behaviour of steel-concrete composite beams subjected to the combined effects of negative bending and axial compression. For this study, six full-scale tests were conducted on composite beams subjected to negative moment while compression was applied simultaneously. The level of the applied axial compression varied from low to high. Following the tests, a nonlinear finite element model was developed and calibrated against the experimental results. The model was found to be capable of predicting the nonlinear response and the ultimate failure modes of the tested beams. The developed finite element model was further used to carry out a series of parametric analyses on a range of composite sections commonly used in practice. It was found that, when a compressive load acts in the composite section, the negative moment capacity of a compositebeamissignificantlyreducedand local bucklinginthe steel beamismorepronounced, compromising the ductility of the section. Rigid plastic analysis based on sectional equilibrium can reasonably predict the com- bined strength of a composite section and, thus, can be used conservatively in the design practice. Detailing with longitudinal stiffeners in the web of the steel beam in the regions of negative bending eliminate web buckling and increase the rotational capacity of the composite section. Based on the experimentaloutcomes and the finite element analyses a simplified design model is proposed for use in engineering practice.

Details

Database :
OpenAIRE
Journal :
Proceedings of the 10th International Conference on Advances in Steel Concrete Composite and Hybrid Structures
Accession number :
edsair.doi...........c15138f93382986391337c4e48ab626f
Full Text :
https://doi.org/10.3850/978-981-07-2615-7_166