1983
DOI: 10.1002/nme.1620191207
|View full text |Cite
|
Sign up to set email alerts
|

Anisotropic cylindrical shell element based on discrete Kirchhoff theory

Abstract: A triangular cylindrical shell element based on discrete Kirchhoff theory is developed. It is a three-node, 27-degrees-of-freedom element using cubic polynomials for the tangential and normal displacement interpolations. The normal rotations are independently interpolated by quadratic polynomials. The formulation is capable of modelling general anisotropy representative of multi-layered, multi-directionally oriented composite construction. The numerical results indicate that the solution for 'displacements and… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1

Citation Types

0
1
0

Year Published

1987
1987
2023
2023

Publication Types

Select...
6

Relationship

0
6

Authors

Journals

citations
Cited by 17 publications
(2 citation statements)
references
References 8 publications
0
1
0
Order By: Relevance
“…The method of discretizing the Kirchhoff-Love hypotheses was first proposed in [8] and was then widely used in designing thin plates and shells [5,7,15].…”
Section: A Methods For Solving Geometrically Nonlinear Problems For Ormentioning
confidence: 99%
“…The method of discretizing the Kirchhoff-Love hypotheses was first proposed in [8] and was then widely used in designing thin plates and shells [5,7,15].…”
Section: A Methods For Solving Geometrically Nonlinear Problems For Ormentioning
confidence: 99%
“…They considered isotropic as well as multilayered anisotropic materials. Sridhara murthy and Gallagher [7] applied a triangular thin shell element, based on Discrete Kirchhoff Theory with three nodes and 27 dof to the analysis of an orthotropic cylinder with a circular hole subjected to axial tension. Han and Gould [8] developed and applied a special finite element model that combined an axisymetric shell element, a general shell element and a transition element to the problem of cylindrical shell with a circular cutout under axial tension.…”
Section: Introductionmentioning
confidence: 99%