Computational geometrical and mechanical modeling of woven ceramic composites at the mesoscale
Autor: | Pierre Ladevèze, Emmanuel Baranger, Martin Genet, C. Fagiano |
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Přispěvatelé: | ONERA - The French Aerospace Lab [Châtillon], ONERA-Université Paris Saclay (COmUE), Laboratoire de Mécanique et Technologie (LMT), École normale supérieure - Cachan (ENS Cachan)-Université Pierre et Marie Curie - Paris 6 (UPMC)-Centre National de la Recherche Scientifique (CNRS) |
Rok vydání: | 2014 |
Předmět: |
Materials science
Scale (ratio) Strain energy density function 02 engineering and technology 021001 nanoscience & nanotechnology [PHYS.MECA.MEMA]Physics [physics]/Mechanics [physics]/Mechanics of materials [physics.class-ph] Matrix (mathematics) 020303 mechanical engineering & transports 0203 mechanical engineering visual_art Damage mechanics Ceramics and Composites visual_art.visual_art_medium Plain weave Polygon mesh Ceramic Hexahedron Composite material 0210 nano-technology Civil and Structural Engineering |
Zdroj: | Composite Structures Composite Structures, Elsevier, 2014, Computational geometrical and mechanical modeling of woven ceramic composites at the mesoscale, 112, pp.146-156. ⟨10.1016/j.compstruct.2014.01.045⟩ Composite Structures, 2014, Computational geometrical and mechanical modeling of woven ceramic composites at the mesoscale, 112, pp.146-156. ⟨10.1016/j.compstruct.2014.01.045⟩ |
ISSN: | 0263-8223 |
Popis: | International audience; Woven composite materials are receiving particular attention in a wide range of specialized aeronautical applications. Reliable numerical prediction tools based on computational modeling are required to quantitatively characterize the role of the microstructure and damage mechanisms at the mesoscale. In this paper, such a computational strategy is illustrated on a generic SiC/SiC plain weave composite with chemical vapor infiltrated matrix. Matrix and tows damage mechanisms are respectively introduced through the use of an anisotropic damage model, and an homogenized model based on a micromechanical model on the fiber scale. The latter is presented in this paper for the first time. Particular attention is paid to the generation of accurate hexahedral meshes, compatible at the tow–tow and tow–matrix interfaces. The mesh quality is analyzed using an error estimator variable based on the strain energy density. Damage predictions obtained using tetrahedral and hexahedral meshes are compared for basic loading cases, illustrating the need for using high quality meshes in the growing community of woven composites computational modeling. |
Databáze: | OpenAIRE |
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