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Title: | The effects of axial tension on the sagging-moment regions of concrete-filled tubular flange girders |
Authors: | Al-Dujele, R Cashell, KA |
Keywords: | concrete-filled tubular flange girders;axial tension;sagging momen;finite element analysis;combined loading;interaction diagram |
Issue Date: | 5-Dec-2018 |
Publisher: | ICASS'2018 |
Citation: | Al-Dujele, R. and Cashell, K.A. (2018) 'The effects of axial tension on the sagging-moment regions of concrete-filled tubular flange girders', Proceedings of the 9th International Conference on Advances in Steel Structures, ICASS 2018, Hong Kong, China, 5-7 December, pp. 1 - 12. doi: 10.18057/ICASS2018.P.009. |
Abstract: | Steel-concrete composite construction is commonly used for many types of structure, including heavy load-bearing applications such as bridges and multi-storey car parks. Some of their component elements such as bridge approaches, inclined parking ramps and stadium beams are exposed to a simultaneous combination of high axial loads and bending moments. A relatively new solution for heavily loaded composite members are concrete-filled tubular flange girders (CFTFGs) which are unconventional I-shaped girders where one or both of the steel flanges are replaced with a hollow section and then filled with concrete to increase the strength and stiffness. These are complex members and their behaviour is governed by a number of inter-related parameters. This work aims to investigate the ultimate strength of CFTFGs with a stiffened web under the combined effects of various levels of axial tension and positive (sagging) bending moment. Nonlinear three-dimensional finite element (FE) analyses using the ABAQUS computer software package are employed to conduct parametric studies. Several influential parameters are examined and conclusions are discussed. |
URI: | https://bura.brunel.ac.uk/handle/2438/27097 |
DOI: | httpa://doi.org/10.18057/ICASS2018.P.009 |
ISBN: | 978-988-99140-9-7 |
Other Identifiers: | ORCID iD: Katherine A. Cashell https://orcid.org/0000-0003-2804-4542 |
Appears in Collections: | Dept of Mechanical and Aerospace Engineering Research Papers |
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