Geometrically nonlinear analysis of thin shell by a quadrilateral finite element with in-plane rotational degrees of freedom
Author:
Affiliation:
1. a LGC, Laboratoire de Génie Civil , Université Badji Mokhtar de Annaba BP 12 , 23100 , Annaba , Algérie
2. b Université Fares Yahia de Médéa , 26000 , Médéa , Algérie
Publisher
River Publishers
Subject
Mechanical Engineering,Mechanics of Materials,Modeling and Simulation
Link
https://www.tandfonline.com/doi/pdf/10.3166/ejcm.19.707-724
Reference20 articles.
1. A compatible triangular element including vertex rotations for plane elasticity analysis
2. A study of three-node triangular plate bending elements
3. Evaluation of a new quadrilateral thin plate bending element
4. Computation of thin structures at large strains and large rotations using a simple C0 isoparametric three-node shell element
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