An anistropic damage model for the description of transversematrix cracking in a graphite-epoxy laminate

Composite Structures

Volumn 53, Issue 3, 2001, Pages 295-299

  Schipperen, J H A ^a  

^a DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

Author keywords

Anisotropic damage mechanics; Finite elements; Graphite epoxy laminates; Transverse matrix cracking

Indexed keywords

ANISOTROPY; CRACK INITIATION; DELAMINATION; FAILURE ANALYSIS; FIBER REINFORCED MATERIALS; FINITE ELEMENT METHOD; GRAPHITE; MATHEMATICAL MODELS;

GRPAHITE-EPOXY LAMINATES;

LAMINATED COMPOSITES;

ANISOTROPY; CRACKING; DAMAGE; FIBER REINFORCED COMPOSITE; GRAPHITE FIBER;

EID: 0035424884     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(01)00013-7     Document Type: Article

References (12)

1. Damage tolerance of laminated composites containing an open hole and subjected to compressive loadings: Part II - Experiment
2. Interlaminar stress in composite laminates under axial extension
3. Characterization of delamination onset and growth in a composite laminate
4. Fiber fracture in unidirectional composites
5. Borst Rde. Mixed mode delamination in graphite-epoxy prepregs: A numerical analysis
6. A progressive failure model for composite laminates containing openings
7. Damage modeling of laminated composites
8. Damage tolerance of laminated composites containing an open hole and subjected to compressive loadings: Part I - Analysis
9. Matrix crack initiation and progression in composite laminates subjected to bending and extension
10. Nonlinear elastic behavior of unidirectional composite laminac
11. Three-dimensional modeling of damage in laminated composites containing a central hole