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Investigation of Micro-Scale Architectural Effects on Damage of CompositesThis paper presents a three-dimensional, energy based, anisotropic, stiffness reduction, progressive damage model for composite materials and composite material constituents. The model has been implemented as a user-defined constitutive model within the Abaqus finite element software package and applied to simulate the nonlinear behavior of a damaging epoxy matrix within a unidirectional composite material. Three different composite microstructures were considered as finite element repeating unit cells, with appropriate periodicity conditions applied at the boundaries. Results representing predicted transverse tensile, longitudinal shear, and transverse shear stress-strain curves are presented, along with plots of the local fields indicating the damage progression within the microstructure. It is demonstrated that the damage model functions appropriately at the matrix scale, enabling localization of the damage to simulate failure of the composite material. The influence of the repeating unit cell geometry and the effect of the directionality of the applied loading are investigated and discussed.
Document ID
20150010216
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Stier, Bertram
(Technische Hochschule Aachen, Germany)
Bednarcyk, Brett A.
(NASA Glenn Research Center Cleveland, OH United States)
Simon, Jaan W.
(Technische Hochschule Aachen, Germany)
Reese, Stefanie
(Technische Hochschule Aachen, Germany)
Date Acquired
June 9, 2015
Publication Date
May 1, 2015
Subject Category
Composite Materials
Report/Patent Number
E-19076
NASA/TM-2015-218740
GRC-E-DAA-TN22150
Report Number: E-19076
Report Number: NASA/TM-2015-218740
Report Number: GRC-E-DAA-TN22150
Funding Number(s)
WBS: WBS 826611.04.03.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
damage
composite materials
finite element method
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