DocumentCode :
3235346
Title :
The research on hysteretic behavior of rectangular section components of cold-formed thin-wall steel
Author :
Na, Yang ; Yanan, Zhong ; Qingtong, Meng
Author_Institution :
Beijing Jiaotong Univ., Beijing, China
fYear :
2011
fDate :
22-24 April 2011
Firstpage :
880
Lastpage :
883
Abstract :
Based on stability theory and nonlinear finite element (FE) method, ANSYS finite element models (FEM) are presented, which introduce shell181 and take geometric and material nonlinear into account. The seismic behavior of rectangular section steel members under the axial compression and the bending load is investigated. The effect of length-slender ratio, width-thickness ratio of flange and web, axial-compression ratio is demonstrated, according to the enormous calculation of various parameters. The results show that the width-thickness ratio and axial-compression ratio have generous impact on component hysteretic performance. The length-slender ratio takes a great influence on the strength degradation and plastic deformation.
Keywords :
bending strength; compressive strength; finite element analysis; mechanical stability; plastic deformation; steel; structural engineering; thin wall structures; ANSYS finite element model; FEM; axial compression; bending load; cold-formed thin-wall steel; hysteretic behavior; length-slender ratio; nonlinear finite element method; plastic deformation; rectangular section component; rectangular section steel member; seismic behavior; shell181; stability theory; strength degradation; width-thickness ratio; Energy dissipation; Finite element methods; Flanges; Loading; Materials; Skeleton; Steel; cold-formed thin-wall rectangular section steel; failure mechanism; finite element calculation; hysteretic behavior;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electric Technology and Civil Engineering (ICETCE), 2011 International Conference on
Conference_Location :
Lushan
Print_ISBN :
978-1-4577-0289-1
Type :
conf
DOI :
10.1109/ICETCE.2011.5775191
Filename :
5775191
Link To Document :
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