TY - JOUR
T1 - Modeling geometry and progressive interfacial damage in textile composites
AU - Hsu, Su Yuen
AU - Cheng, Ron Bin
N1 - Funding Information:
This paper is based on research funded by the Hypersonics Project of the NASA Fundamental Aeronautics Program during 2009 and 2010.
PY - 2013/5
Y1 - 2013/5
N2 - A procedure combining geometrically nonlinear, explicit dynamic contact analysis, computer-aided-design techniques, elasticity-based mesh deformation, and cohesive contact modeling is proposed to efficiently construct practical finite element models for meso-mechanical analysis of progressive damage in textile composites. In the procedure, the geometry of the fiber tows is computed by imposing a fictitious expansion on the tows. Meshes resulting from the procedure are incongruent at the computed tow-tow and tow-matrix interfaces. The interfaces are treated as cohesive contact surfaces not only to resolve the incongruence but also to simulate progressive interfacial damage. Example meshes are constructed for two plain weaves, a ceramic-matrix composite with matrix porosity and a polymeric-matrix composite without porosity. To verify the meshes and interfaces, the composite models are simplified to only have interfacial damage in numerical experiments of uniaxial cyclic loading. Although the computed progression of damage is rather complex, anticipated major qualitative characteristics are reproduced in the computations.
AB - A procedure combining geometrically nonlinear, explicit dynamic contact analysis, computer-aided-design techniques, elasticity-based mesh deformation, and cohesive contact modeling is proposed to efficiently construct practical finite element models for meso-mechanical analysis of progressive damage in textile composites. In the procedure, the geometry of the fiber tows is computed by imposing a fictitious expansion on the tows. Meshes resulting from the procedure are incongruent at the computed tow-tow and tow-matrix interfaces. The interfaces are treated as cohesive contact surfaces not only to resolve the incongruence but also to simulate progressive interfacial damage. Example meshes are constructed for two plain weaves, a ceramic-matrix composite with matrix porosity and a polymeric-matrix composite without porosity. To verify the meshes and interfaces, the composite models are simplified to only have interfacial damage in numerical experiments of uniaxial cyclic loading. Although the computed progression of damage is rather complex, anticipated major qualitative characteristics are reproduced in the computations.
UR - http://www.scopus.com/inward/record.url?scp=84877968974&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=84877968974&partnerID=8YFLogxK
U2 - 10.1177/0021998312447207
DO - 10.1177/0021998312447207
M3 - Article
AN - SCOPUS:84877968974
VL - 47
SP - 1343
EP - 1356
JO - Journal of Composite Materials
JF - Journal of Composite Materials
SN - 0021-9983
IS - 11
ER -