In this paper, delamination progression in a composite laminate is modelled by interface elements within a geometrically non-linear FE analysis setting. With the assumption of small continuum deformations, a rotational interface formulation is obtained from a recently proposed formulation based on t
β¦ LIBER β¦
Delamination analysis of holed composite laminates using interface elements
β Scribed by H. Hosseini-Toudeshky; M. Jalalvand; B. Mohammadi
- Book ID
- 108255618
- Publisher
- Elsevier
- Year
- 2009
- Tongue
- English
- Weight
- 414 KB
- Volume
- 1
- Category
- Article
- ISSN
- 1877-7058
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