Back to Search Start Over

A Damage Model for the Simulation of Delamination in Advanced Composites under Variable-Mode Loading

Authors :
Turon, A
Camanho, P. P
Costa, J
Davila, C. G
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

Subjects :
Composite Materials

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