2001
DOI: 10.1016/s0020-7683(01)00134-2
|View full text |Cite
|
Sign up to set email alerts
|

Application of transversely isotropic materials to multi-layer shell elements undergoing finite rotations and large strains

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1

Citation Types

0
1
0

Year Published

2002
2002
2017
2017

Publication Types

Select...
4
1

Relationship

0
5

Authors

Journals

citations
Cited by 6 publications
(1 citation statement)
references
References 19 publications
0
1
0
Order By: Relevance
“…Owing to symmetries, only one quarter of the structure is illustrated in Figure 19 together with data and boundary conditions considered in the computation. The analysis is performed for two di erent material models, the St. Venant model and a hyperelastic model [22] where the material constants are selected so as to describe a transversely isotropic material with reinforcements placed in circumferential direction. To consider this e ect the circumferential sti ness is assumed to be twice the sti ness of the isotropic material while the sti ness normal to the reinforcement is reduced to half the corresponding value of the isotropy.…”
Section: Non-linear Bending Deformations Of a Pinched Cylindermentioning
confidence: 99%
“…Owing to symmetries, only one quarter of the structure is illustrated in Figure 19 together with data and boundary conditions considered in the computation. The analysis is performed for two di erent material models, the St. Venant model and a hyperelastic model [22] where the material constants are selected so as to describe a transversely isotropic material with reinforcements placed in circumferential direction. To consider this e ect the circumferential sti ness is assumed to be twice the sti ness of the isotropic material while the sti ness normal to the reinforcement is reduced to half the corresponding value of the isotropy.…”
Section: Non-linear Bending Deformations Of a Pinched Cylindermentioning
confidence: 99%