A finite element analysis for the free vibration behaviour of doubly curved shells is presented in which eight-noded curved quadrilateral isoparametric finite elements are used. The first order shear deformation theory for thin and shallow shells is used in the formulation. Results are obtained for
Finite element buckling analysis of rotationally periodic laminated composite shells
โ Scribed by Zhihai Xiang; Mingde Xue; Yinghua Liu; Zhangzhi Cen
- Publisher
- John Wiley and Sons
- Year
- 2001
- Tongue
- English
- Weight
- 719 KB
- Volume
- 53
- Category
- Article
- ISSN
- 0029-5981
- DOI
- 10.1002/nme.322
No coin nor oath required. For personal study only.
๐ SIMILAR VOLUMES
A finite element analysis for the free vibration behaviour of point supported laminated composite cylindrical shells is presented. Eight-noded curved quadrilateral isoparametric elements are used. The formulation is based on the assumptions of the first order shear deformation theory for thin, shall
## Abstract By considering the characteristics of deformation of rotationally periodic structures subjected to rotationally periodic loads, the periodic structure is divided into several identical substructures in this paper. If the structure is really periodic but not axisymmetric, the number of t
The present work describes the transient dynamic response of unsti!ened/sti!ened composite plates/shells using "nite element method. Composite panels "nd wide applications in aerospace, marine and other engineering because of its high strength to weight ratios. These structures are often subjected t