AN INVESTIGATION OF A FINITE ROTATION 4 NODE ASSUMED STRAIN SHELL ELEMENT

被引:77
|
作者
PARISCH, H
机构
[1] Institut für Statik und Dynamik der Luft-und Raumfahrtkonstruktionen, Universität Stuttgart, Stuttgart
关键词
D O I
10.1002/nme.1620310108
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The paper presents a shell formulation based on the 'degenerated solid approach'. The theory employs covariant strains and performs explicit integration through the shell thickness. The rigid body motion is exactly represented. The consistent tangent stiffness matrix is evaluated for the four node quadrilateral. It is shown, in the final part, that this type of element, which distinguishes itself by a very simple and easily understandable theory, gives good answers for linear as well as non-linear applications.
引用
收藏
页码:127 / 150
页数:24
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