Abstract
The mechanical behaviour and progressive damage of a plain woven carbon-epoxy fabric at different length scales is modelled, taking into account the weave's geometric, and consequently, material variability. Micromechanical simulations are performed with different fibre volume fractions using a fibre distribution algorithm in order to obtain the mechanical properties of the tows along their length. A Representative Unit Cell (RUC) is generated and a set of in-plane Periodic Boundary Conditions (PBCs) implemented in order to run non-homogenised mesomechanical analyses. The influence of material variability is captured through volumetric homogenisation to study damage evolution and corresponding stiffness degradation in a plain weave fibre architecture under different loading conditions. © CCM 2020 - 18th European Conference on Composite Materials. All rights reserved.
| Original language | English |
|---|---|
| Title of host publication | ECCM 2018 - 18th European Conference on Composite Materials |
| Publisher | Applied Mechanics Laboratory |
| Number of pages | 8 |
| Publication status | Published - 2019 |
Bibliographical note
18th European Conference on Composite Materials, ECCM 201824 - 28 June 2018
Athens, Greece
Keywords
- Computational mechanics Finite Element Analysis (FEA) Mechanical properties Multiscale modelling Textile composites Carbon Composite materials Degrees of freedom (mechanics) Finite element method Different length scale Distribution algorithms Fibre volume fraction Micromechanical simulation Multi-scale modelling Periodic boundary conditions Stiffness degradation Textile composite Weaving