Inelastic large deflection analysis of space steel frames using an equivalent accumulated element. (1st May 2018)

• Record Type: Journal Article
• Authors: Zubydan, Ahmed H.; ElSabbagh, Ashraf I.; Sharaf, Tarek; Farag, Abbad-Elrahman
• Is Part Of: Engineering structures. Volume 162(2018)
• Page Start: 121
• Page End: 134
• Publication Date: 2018-05-01
• Subjects: Inelastic -- Large deflection -- Space frame -- Nonlinear analysis -- Spread of plasticity -- Beam-column; Structural engineering -- Periodicals; Structural analysis (Engineering) -- Periodicals; Construction, Technique de la -- Périodiques; Génie parasismique -- Périodiques; Pression du vent -- Périodiques; Earthquake engineering; Structural engineering; Wind-pressure; Periodicals; 624.105
• DOI: 10.1016/j.engstruct.2018.01.059
• Languages: English
• ISSNs: 0141-0296

Abstract

Highlights: A new space frame element was developed for inelastic large deflection analysis of space frame. The new element predicted well the full nonlinear behavior of space frames using only one element per member. The derived element saved much run time required storage memory. Abstract: This paper presents a new model to perform inelastic large deflection analysis of space steel frames depending on the spread of plasticity method. A stiffness matrix of a beam-column element with only two nodes and six degrees of freedom for each node is derived to represent the space frame member. The proposed matrix includes the effect of section yielding along the member as well as the effect of large deflection. Stiffness degradation at the cross-section due to yielded parts is calculated using a formula for the tangent modulus which is affected by the sectional internal forces. The proposed technique of accumulation of rigidity factors is submitted as a first step to get exact first order stiffness factors for a member with variable cross sections. The effect of large deflection is included by considering the axial force while deriving the stiffness factors. Both cubic and higher order shape functions are tried to produce an element that can represent the member without discretization. A finite element program based on stiffness matrix method is developed to predict the inelastic large deflection behavior of steel space frames using the derived stiffness matrix. The proposed finite element technique exhibits good correlation when compared with the conventional spread of plasticity model results. Verification by solving benchmarked steel structures is carried out. The analysis results indicate that the new model is accurate with simple equations and it achieves a significant improvement to the run time.