Incremental mean-fields micromechanics scheme for non-linear response of ductile damaged composite materials

• Published in: Composites. Part B, Engineering Vol. 69; pp. 169 - 180
• Main Authors: Tchalla, A., Azoti, W.L., Koutsawa, Y., Makradi, A., Belouettar, S., Zahrouni, H.
• Format: Journal Article
• Language: English
• Published: Elsevier 01.02.2015
• Subjects: Engineering Sciences; C. Ductile damage; B. Effective tangent properties; C. Incremental Micromechanics Scheme; B. Bauschinger effect
• ISSN: 1359-8368; 1879-1069
• DOI: 10.1016/j.compositesb.2014.08.055

This work is concerned with the modeling of ductile damage behavior in composite materials by the means of the Incremental Micromechanics Scheme (IMS) as Mean-Fields Homogenization (MFH) technique. Indeed, IMS is known for its capability to overcome the well-known accuracy restrictions of the Mori-Tanaka (MT) and Self-Consistent (SC) schemes when a high volume fraction of heterogeneities or/and a high contrast between phases properties is reached. This micromechanics formalism is based on the Eshelby's inclusion concept. The kinematic equation of Dederichs and Zeller (1973) is used as formal solution of the heterogeneous material problem. The nonlinear behavior of the composite is addressed in a general framework based on the kinematic hardening of Lemaître-Chaboche's ductile damage model. Thus a classical J 2 plasticity that accounts for the damage evolution within the microstructure is implemented. The time discretization of all rate relations is solved through a generalized mid-point rule that yields to an anisotropic consistent (algorithmic) tangent modulus. To avoid a stiffer macroscopic stress-strain response, an isotropization procedure is adopted during the computation of the Eshelby tensor involved in the IMS modeling. From a computational aspect, the non linear response of the composite is obtained through two interdependent loops: inner and outer. In the inner loop, the IMS determines the global strain concentration tensor that is passed to the outer loop. Then, the macroscopic stress-strain response is derived using an iterative algorithm based on the Hilltype incremental formulation. Numerical results are obtained considering several heterogeneous materials such as Metal Matrix Composites (MMCs) as well as Carbon fibers reinforced Epoxy Matrix Composites. The model's predictions are compared in most of the cases, with experimental data and predictions obtained from MT-based modeling in the open literature.