A numerical procedure for the simulation of skin-stringer debonding growth in stiffened composite panels
- Author
- RICCIO, A1 ; RAIMONDO, A1 ; DI FELICE, G1 ; SCARAMUZZINO, F1
[1] Second University of Naples, Department of Industrial and Information Engineering, via Roma n 29, 81031 Aversa, Italy - Source
Aerospace science and technology (Imprimé). 2014, Vol 39, pp 307-314, 8 p ; ref : 33 ref
- ISSN
- 1270-9638
- Scientific domain
- Aeronautics astronautics; Mechanics acoustics
- Publisher
- Elsevier, Issy-les-Moulineaux
- Publication country
- France
- Document type
- Article
- Language
- English
- Author keyword
- Cohesive elements Damage growth FEM Skin-stringer debonding
- Keyword (fr)
- Endommagement Matériau composite Modélisation Méthode élément fini Plaque renforcée Simulation numérique 4650
- Keyword (en)
- Damaging Composite material Modeling Finite element method Reinforced plate Numerical simulation
- Keyword (es)
- Deterioración Material compuesto Modelización Método elemento finito Placa reforzada Simulación numérica
- Classification
- Pascal
- 001 Exact sciences and technology / 001B Physics / 001B40 Fundamental areas of phenomenology (including applications) / 001B40F Solid mechanics / 001B40F30 Structural and continuum mechanics / 001B40F30N Fracture mechanics (crack, fatigue, damage...)
- Discipline
- Physics : solid mechanics
- Origin
- Inist-CNRS
- Database
- PASCAL
- INIST identifier
- 29022554
Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS
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DOI
10.1016/j.ast.2014.10.003 
https://dx.doi.org/10.1016/j.ast.2014.10.003
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