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Micromechanical Modeling of Woven Metal Matrix CompositesThis report presents the results of an extensive micromechanical modeling effort for woven metal matrix composites. The model is employed to predict the mechanical response of 8-harness (8H) satin weave carbon/copper (C/Cu) composites. Experimental mechanical results for this novel high thermal conductivity material were recently reported by Bednarcyk et al. along with preliminary model results. The micromechanics model developed herein is based on an embedded approach. A micromechanics model for the local (micro-scale) behavior of the woven composite, the original method of cells (Aboudi), is embedded in a global (macro-scale) micromechanics model (the three-dimensional generalized method of cells (GMC-3D) (Aboudi). This approach allows representation of true repeating unit cells for woven metal matrix composites via GMC-3D, and representation of local effects, such as matrix plasticity, yarn porosity, and imperfect fiber-matrix bonding. In addition, the equations of GMC-3D were reformulated to significantly reduce the number of unknown quantities that characterize the deformation fields at the microlevel in order to make possible the analysis of actual microstructures of woven composites. The resulting micromechanical model (WCGMC) provides an intermediate level of geometric representation, versatility, and computational efficiency with respect to previous analytical and numerical models for woven composites, but surpasses all previous modeling work by allowing the mechanical response of a woven metal matrix composite, with an elastoplastic matrix, to be examined for the first time. WCGMC is employed to examine the effects of composite microstructure, porosity, residual stresses, and imperfect fiber-matrix bonding on the predicted mechanical response of 8H satin C/Cu. The previously reported experimental results are summarized, and the model predictions are compared to monotonic and cyclic tensile and shear test data. By considering appropriate levels of porosity, residual stresses, and imperfect fiber-matrix debonding, reasonably good qualitative and quantitative correlation is achieved between model and experiment.
Document ID
19970041400
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Bednarcyk, Brett A.
(Virginia Univ. Charlottesville, VA United States)
Pindera, Marek-Jerzy
(Virginia Univ. Charlottesville, VA United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1997
Subject Category
Composite Materials
Report/Patent Number
NASA-CR-204153
E-10944
NAS 1.26:204153
Report Number: NASA-CR-204153
Report Number: E-10944
Report Number: NAS 1.26:204153
Accession Number
97N32480
Funding Number(s)
CONTRACT_GRANT: NAG3-1319
PROJECT: RTOP 523-61-23
CONTRACT_GRANT: NAG3-1316
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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