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A Damage Model for the Simulation of Delamination in Advanced Composites under Variable-Mode Loading
- Source :
- Mechanics of Materials. 38(11)
- Publication Year :
- 2006
- Publisher :
- United States: NASA Center for Aerospace Information (CASI), 2006.
-
Abstract
- A thermodynamically consistent damage model is proposed for the simulation of progressive delamination in composite materials under variable-mode ratio. The model is formulated in the context of Damage Mechanics. A novel constitutive equation is developed to model the initiation and propagation of delamination. A delamination initiation criterion is proposed to assure that the formulation can account for changes in the loading mode in a thermodynamically consistent way. The formulation accounts for crack closure effects to avoid interfacial penetration of two adjacent layers after complete decohesion. The model is implemented in a finite element formulation, and the numerical predictions are compared with experimental results obtained in both composite test specimens and structural components.
- Subjects :
- Composite Materials
Subjects
Details
- Language :
- English
- Volume :
- 38
- Issue :
- 11
- Database :
- NASA Technical Reports
- Journal :
- Mechanics of Materials
- Notes :
- 23-719-20-40-10
- Publication Type :
- Report
- Accession number :
- edsnas.20080014292
- Document Type :
- Report