A numerical model for layered composite structures based on a geometrical nonlinear shell theory is presented. The kinematic is based on a multi-director theory, thus the in-plane displacements of each layer are described by independent director vectors. Using the isoparametric approach a finite ele
✦ LIBER ✦
Composite laminates: nonlinear interlaminar stress analysis by multi-layer shell elements
✍ Scribed by Y. Başar; M. Itskov; A. Eckstein
- Book ID
- 108391021
- Publisher
- Elsevier Science
- Year
- 2000
- Tongue
- English
- Weight
- 858 KB
- Volume
- 185
- Category
- Article
- ISSN
- 0045-7825
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