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Treating matrix nonlinearity in the binary model formulation for 3D ceramic composite structures
Authors:Shane Flores  Anthony G Evans  Frank W Zok  Martin Genet  Brian Cox  David Marshall  Olivier Sudre  Qingda Yang
Affiliation:1. Materials Department, University of California, Santa Barbara, CA 93106, United States;2. Laboratoire de Mécanique et de Technologie, 61 av. du Président Wilson, 94235 Cachan Cedex, France;3. Teledyne Scientific Co. LLC, Thousand Oaks, CA 91360, United States;4. Department of Mechanical and Aerospace Engineering, University of Miami, 1251 Memorial Drive, Suite EB205, Coral Gables, FL 33146, United States;1. Advanced Composites Centre for Innovation and Science (ACCIS), University of Bristol, University Walk, Bristol BS8 1TR, UK;2. Polymer Composites Research Group, University of Nottingham, University Park, Nottingham NG7 2RD, UK;1. Université de Lyon, LaMCoS UMR 5259, INSA-Lyon, 27 av Jean Capelle, F-69621 Villeurbanne, France;2. Université de Lyon, MATEIS UMR 5510, INSA-Lyon, 25 av Jean Capelle, F-69621 Villeurbanne, France;3. SNECMA, Site de Villaroche, Rond Point René Ravaud – Réau, F-77550 Moissy-Cramayel, France
Abstract:A computationally-efficient numerical approach to treating matrix nonlinearity in ceramic matrix composite components has been developed and validated. The model employs a dual mesh comprising strings of line elements that represent the fiber tows and 3D effective medium elements that define the external geometry and embody the matrix-dominated properties. Validation addressed test data for unnotched and open-hole tension specimens. For these tests, the onset of nonlinearity and subsequent plasticity due to matrix microcracking and interfacial debonding and sliding are satisfactorily represented by a linear Drucker–Prager model for failure initiation in the effective medium along with a fully-associated flow rule with isotropic, perfectly-plastic flow. Composite failure is assumed to be correlated with the maximum local stress averaged over a gauge volume dictated by the fiber tow width. Using one set of specimens for calibration, very good predictions of the nonlinear stress–strain response and ultimate strength of other specimens are obtained.
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