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Structural behaviour of hybrid stainless steel stub columns under axial compression
- Source :
- Structures. 27:128-140
- Publication Year :
- 2020
- Publisher :
- Elsevier BV, 2020.
-
Abstract
- Numerical study on structural performance of hybrid stainless steel stub columns are provided in this paper by utilizing finite element (FE) software, Abaqus. Two novel stainless steel grades were used viz., Lean duplex stainless steel (LDSS) and Duplex stainless steel (DSS) for hybrid stainless steel stub columns. The current investigation on hybrid stub columns consist of two configurations: (1) Hybrid stainless steel (HSS) stub column adopting DSS on the flanges and LDSS on the web; and (2) Hybrid stainless steel (HSSa) stub column using DSS and LDSS on the web and flanges respectively. The numerical results are presented in terms of column capacity (Pu) and failure modes. As observed from the investigation, both flange thickness (tf) and flange width (bf) have more influence on the column capacity for HSS stub column as compared to HSSa stub column. On the other hand, increase in web thickness (tw) is found to provide an enhancement in column capacity for HSSa compared to HSS stub column, in contrast to the effect of tf and bf. In general, EN 1993-1-4 Class 3 limit for internal web is observed to be reliable for all stainless steel stub columns. Based on the FE results, new DSM formulation for HSS and HSSa stub columns was proposed based on modified DSM equation for carbon steel.
- Subjects :
- Materials science
Carbon steel
0211 other engineering and technologies
020101 civil engineering
02 engineering and technology
Building and Construction
Flange
engineering.material
Finite element method
0201 civil engineering
Stub (electronics)
Axial compression
021105 building & construction
Architecture
engineering
Composite material
Safety, Risk, Reliability and Quality
Civil and Structural Engineering
Subjects
Details
- ISSN :
- 23520124
- Volume :
- 27
- Database :
- OpenAIRE
- Journal :
- Structures
- Accession number :
- edsair.doi...........0dc1964102762073fd0e12b9eab8fd42