Geometrically non-linear analysis of symmetrically laminated composite and sandwich shells with a higher-order theory and C0 finite elements
- 31 December 1994
- journal article
- Published by Elsevier in Composite Structures
- Vol. 27 (4) , 403-418
- https://doi.org/10.1016/0263-8223(94)90267-4
Abstract
No abstract availableKeywords
This publication has 19 references indexed in Scilit:
- A higher-order shear deformation theory of laminated elastic shellsPublished by Elsevier ,2003
- Estimation of interlaminar stresses in fibre reinforced composite cylindrical shellsComputers & Structures, 1991
- Non-linear dynamics of laminated plates with a higher-order theory and C0 finite elementsInternational Journal of Non-Linear Mechanics, 1991
- Transient/pseudo-transient finite element small/large deformation analysis of two-dimensional problemsComputers & Structures, 1990
- Transient dynamics of composite sandwich plates using 4-, 8-, 9-noded isoparametric quadrilateral elementsFinite Elements in Analysis and Design, 1989
- Higher-order theories for composite and sandwich cylindrical shells with C0 finite elementComputers & Structures, 1989
- An unsymmetric FRC laminate C° finite element model with 12 degrees of freedom per nodeEngineering Computations, 1988
- A simple finite element formulation of a higher-order theory for unsymmetrically laminated composite platesComposite Structures, 1988
- A C° continuous linear beam/bilinear plate flexure elementComputers & Structures, 1986
- Exact Solutions of Moderately Thick Laminated ShellsJournal of Engineering Mechanics, 1984