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Finite Element Model for Failure Study of Two-Dimensional Triaxially Braided Composite

Authors :
Li, Xuetao
Binienda, Wieslaw K
Goldberg, Robert K
Publication Year :
2010
Publisher :
United States: NASA Center for Aerospace Information (CASI), 2010.

Abstract

A new three-dimensional finite element model of two-dimensional triaxially braided composites is presented in this paper. This meso-scale modeling technique is used to examine and predict the deformation and damage observed in tests of straight sided specimens. A unit cell based approach is used to take into account the braiding architecture as well as the mechanical properties of the fiber tows, the matrix and the fiber tow-matrix interface. A 0 deg / plus or minus 60 deg. braiding configuration has been investigated by conducting static finite element analyses. Failure initiation and progressive degradation has been simulated in the fiber tows by use of the Hashin failure criteria and a damage evolution law. The fiber tow-matrix interface was modeled by using a cohesive zone approach to capture any fiber-matrix debonding. By comparing the analytical results to those obtained experimentally, the applicability of the developed model was assessed and the failure process was investigated.

Subjects

Subjects :
Composite Materials

Details

Language :
English
Database :
NASA Technical Reports
Notes :
WBS 698259.02.07.03.03.01, , NNX07AV60A
Publication Type :
Report
Accession number :
edsnas.20100026659
Document Type :
Report