Plasticity dependent damage evolution in composites with strain-gradient effects. (15th June 2015)

• Record Type: Journal Article
• Authors: Legarth, Brian Nyvang
• Is Part Of: International journal of solids and structures. Volume 63(2015)
• Page Start: 1
• Page End: 10
• Publication Date: 2015-06-15
• Subjects: Elastic-viscoplastic strain gradient plasticity -- Higher-order Debonding -- Fibre-reinforced composite material -- Finite elements; Mechanics, Applied -- Periodicals; Structural analysis (Engineering) -- Periodicals; Elastic solids -- Periodicals; Mécanique appliquée -- Périodiques; Constructions, Théorie des -- Périodiques; Solides élastiques -- Périodiques; Elastic solids; Mechanics, Applied; Structural analysis (Engineering); Periodicals; 624.18
• DOI: 10.1016/j.ijsolstr.2015.01.017
• Languages: English
• ISSNs: 0020-7683

Abstract

Highlights: Size effects and debonding of composite materials. Higher-order strain-gradient plasticity with consistent cohesive law. Finite element. Monotonic effect of cohesive length scale parameter on the failure strain. Non-monotonic effect of matrix length scale parameter on the failure strain. Abstract: A unit cell approach is adopted to numerically analyze the effect of reinforcement size on fracture evolution in metal matrix composites. The matrix material shows plastic size-effects and is modeled by an anisotropic version of the single parameter strain-gradient (higher-order) plasticity model by Fleck and Hutchinson (2001). The fracture process along the fiber–matrix interface is modeled using a recently proposed cohesive law extension, where plasticity affects the fracture process as both the average as well as the jump in plastic strain across the interface are accounted for Tvergaard et al. (2013). In this study the reinforcement is assumed perfectly stiff and consequently only one new cohesive material parameter is introduced. Results are shown for both conventional isotropy as well as plastic anisotropy with higher-order material behavior. Due to fiber–matrix decohesion a sudden stress-drop is seen in the macroscopic stress–strain response curve, which defines the failure strain of the composite. It is shown, that decreasing the value of the new cohesive material length parameter will monotonically decrease the failure strain. On the other hand, the material length scale parameter of the matrix affects the failure strain in a non-monotonic manner. Depending on the degree of anisotropy a maximum failure strain is predicted for a length scale corresponding to 10–15% of the reinforcement radius.