Nonlinear Finite Element Bending Analysis of Composite Shell Panels
| 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.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.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.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 |
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