This paper proves the generalized compatibility of the boundary displacement pattern of the generalized conforming ¯at shell element with drilling degrees of freedom and the central line displacement pattern of the beam element with Hermite interpolation. According to the incremental equation of vir
Geometric non-linear analysis of space shell structures using generalized conforming flat shell elements-for space shell structures
✍ Scribed by Qun, Zhang ;Mu, Lu ;Wenqi, Kuang
- Publisher
- John Wiley and Sons
- Year
- 1998
- Tongue
- English
- Weight
- 201 KB
- Volume
- 14
- Category
- Article
- ISSN
- 1069-8299
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✦ Synopsis
An updated Lagrangian formulation of the generalized conforming ¯at shell element with drilling degrees of freedom is derived based on the incremental equation of virtual work of a three-dimensional (3D) continuum for a purely geometric non-linear analysis of the space structure. While solving the non-linear equations, the Euler±Newton method and modi®ed Euler±Newton method are used in static analyses, and the modi®ed arc-length method and Newton arc-length method for post-buckling problems. A number of numerical examples are given to demonstrate the eectiveness of the proposed approach and programs.
📜 SIMILAR VOLUMES
Based on the re"ned non-conforming element method, simple #at triangular elements with standard nodal displacement parameters are proposed for the analysis of shell structures. For ensuring the convergence of the elements a new coupled continuity condition at the inter-element has been established i