1. Influence of in-plane transverse compression on the behaviour of the face plate component in weak axis and tubular steel joints.
- Author
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Seyoum Lemma, Melaku, Rebelo, Carlos, Conde, Jorge Conde, and Simões da Silva, Luís
- Subjects
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FINITE element method , *FLANGES , *STEEL - Abstract
The behaviour of the face-plate component under out-of-plane loading has been previously studied, and analytical formulations characterizing the initial stiffness have been proposed. However, research investigating the response of this component under simultaneous transverse loading is limited. This study examines the influence of in-plane transverse compression on the out-of-plane behaviour of the face-plate component in weak axis and tubular beam-to-column steel joints. An experimental test campaign was conducted, covering five representative joint configurations for connections to both I-section and tubular columns. Finite element models of the tested specimen were generated and validated based on the test results. Subsequently, these results were supplemented by two sets of numerical parametric studies, encompassing a total of 329 connections under different levels of transverse loads. The results indicate the detrimental effect of transverse compression on the stiffness and resistance of the face-plate component. Analytical expressions for the reduction of initial stiffness under compressive in-plane transverse loads were proposed and validated, facilitating easy incorporation into design standards. ● Experimental tests conducted on the face plate component under both out-of-plane and in-plane transverse loading conditions. ● Numerical models validated through test findings, which are then extended through a comprehensive parametric study. ● Influence of flange rotational restraint assessed regarding its effects on the initial stiffness of the face plate component. ● An analytical model proposed to evaluate in-plane transverse compression's impact on the initial stiffness of the face plate. [ABSTRACT FROM AUTHOR]
- Published
- 2025
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