Finite-element implementation for nonlinear static and dynamic frame analysis of tapered members

•Refined element formulations for eight common types of sections are firstly derived.•The handling methods for the member distributed loads on non-prismatic members are proposed.•The consistent mass matrices for dynamic analysis of tapered members are given.•The Updated-Lagrangian method is introduc...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Engineering structures 2018-10, Vol.172, p.358-381
Hauptverfasser: Bai, Rui, Liu, Si-Wei, Chan, Siu-Lai
Format: Artikel
Sprache:eng
Schlagworte:
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Beschreibung
Zusammenfassung:•Refined element formulations for eight common types of sections are firstly derived.•The handling methods for the member distributed loads on non-prismatic members are proposed.•The consistent mass matrices for dynamic analysis of tapered members are given.•The Updated-Lagrangian method is introduced for allowing large deflection.•The numerical method for both nonlinear static and dynamic analyses is established.•A complete solution for analyzing tapered members is proposed and validated with extensive examples. Non-prismatic members are popular for civil engineering structures. This paper derives a set of unified beam-column formulations for nonlinear static and dynamic analyses of the structures made of members with tapered sections, addressing the problems in engineering design practices. The element shape-functions are established upon the local-axes by extracting the rigid-body movements for simplifying mathematical expressions. To represent the variations in the stiffness gradients of tapered sections, the tapered-variability indexes are proposed. The generalized tangent stiffness and consistent mass matrices are developed based on the indexes. When analyzing non-prismatic members, the conventional method for handling member loads is inapplicable because it is derived for prismatic sections. Therefore, a new approach for converting the member loads acting on tapered members into the equivalent nodal forces is proposed based on the energy conservation principle. To consider the offsets in section axes, the eccentricity matrices are employed. For allowing large deflections, the incremental secant-stiffness method (ISM) based on Updated-Lagrangian (UL) description is proposed. Finally, extensive examples are provided for validating the accuracy and efficiency of the proposed element formulations in solving both the static and dynamic nonlinear problems.
ISSN:0141-0296
1873-7323
DOI:10.1016/j.engstruct.2018.05.088