DocumentCode
693023
Title
Large deformation analysis of shell structures using a corotational solid-shell element
Author
Wang Zhen ; Sun Qin
Author_Institution
Sch. of Aeronaut., Northwestern Polytech. Univ., Xi´an, China
fYear
2013
fDate
20-22 Dec. 2013
Firstpage
2838
Lastpage
2842
Abstract
An efficient locking-free 8-node solid-shell element is developed for geometrically nonlinear analysis of shell structures. The solid-shell element is developed based on the conventional brick solid element with only translational degrees of freedom. A initial coordinate system is created to orient the right thickness direction of the shell for each solid-shell element. The Assumed Natural Strain (ANS) method and the Enhanced Assumed strain (EAS) method are used to improve the linear performance of the element formulation. The corotational formulation is used to extend the linear element to geometrically nonlinear analysis. Numerical examples demonstrate the excellent performance of the present solid-shell element.
Keywords
deformation; finite element analysis; interpolation; shells (structures); structural engineering; ANS method; EAS method; assumed natural strain; brick solid element; coordinate system; corotational formulation; corotational solid-shell element; element formulation; enhanced assumed strain; finite element interpolation; geometrically nonlinear analysis; large deformation analysis; linear element; linear performance; locking-free 8-node solid-shell element; shell structures; thickness direction; translational degrees of freedom; Educational institutions; Finite element analysis; Force; Solid modeling; Solids; Strain; Vectors; ANS; Corotational formulation; EAS; Solid-shell element;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechatronic Sciences, Electric Engineering and Computer (MEC), Proceedings 2013 International Conference on
Conference_Location
Shengyang
Print_ISBN
978-1-4799-2564-3
Type
conf
DOI
10.1109/MEC.2013.6885514
Filename
6885514
Link To Document