| dc.contributor.author |
Patel, S. N. |
|
| dc.date.accessioned |
2022-12-17T13:53:44Z |
|
| dc.date.available |
2022-12-17T13:53:44Z |
|
| dc.date.issued |
2014-12 |
|
| dc.identifier.uri |
https://link.springer.com/chapter/10.1007/978-81-322-2190-6_13 |
|
| dc.identifier.uri |
http://dspace.bits-pilani.ac.in:8080/xmlui/handle/123456789/7921 |
|
| dc.description.abstract |
This paper deals with the geometric nonlinear bending response of laminated composite shell panels subjected to transverse loading. The eight-noded degenerated shell element with five degrees of freedom per node is adopted in the present analysis to model the composite shell panels. The Green-Lagrange strain displacement relationship is adopted to formulate the matrices. The total Lagrangian approach is taken in the formulation. The arc-length method of solution is adopted in tracing the equilibrium path. The results by this method are compared with the available results and the conclusions are made. |
en_US |
| dc.language.iso |
en |
en_US |
| dc.subject |
Civil Engineering |
en_US |
| dc.subject |
Degenerated shell element |
en_US |
| dc.subject |
Nonlinear analysis |
en_US |
| dc.subject |
Green-Lagrange nonlinearity |
en_US |
| dc.subject |
Cylindrical panels |
en_US |
| dc.title |
Nonlinear Finite Element Bending Analysis of Composite Shell Panels |
en_US |
| dc.type |
Book chapter |
en_US |