Analytical modeling of fiber–matrix interface failure in unidirectional laminae subjected to in-plane shear loads

Author:

Vignoli Lucas L.1ORCID,Carneiro Neto Ranulfo M.1,Savi Marcelo A.2,Pacheco Pedro M.C.L.3,Kalamkarov Alexander L.4

Affiliation:

1. Center of Technology and Applications of Composite Materials, Department of Mechanical Engineering, Universidade Federal do Rio de Janeiro, Macaé, RJ, Brazil

2. Center for Nonlinear Mechanics, COPPE – Department of Mechanical Engineering, Universidade Federal do Rio de Janeiro, Rio de Janeiro, Brazil

3. Department of Mechanical Engineering, Centro Federal de Educação Tecnológica Celso Suckow da Fonseca CEFET/RJ, Rio de Janeiro, RJ, Brazil

4. Department of Mechanical Engineering, Dalhousie University, Halifax, Nova Scotia, Canada

Abstract

Unidirectional laminae subjected to in-plane shear loads present complex behavior with strong nonlinear response. A novel analytical model is proposed considering a unit cell with square symmetry and circular fiber cross-section taking into account the failure on the interface between fiber and matrix. The interface failure is a shear-driven phenomenon described by a constant value during the failure process. The model validation is performed using two different approaches: the analytical estimations are compared with experimental data, and finite-element simulations are employed to evaluate the influence of fiber volume fraction. The proposed analytical model captures the main features of experimental data showing its capability and reliability to represent the complex interface debonding propagation phenomenon. Numerical simulations show in-plane shear stress–strain curves for four distinct unidirectional laminae with different fiber volume fractions. Results attest the model capability to describe composite materials with composite failure, essentially characterized by the interface behavior.

Funder

Conselho Nacional de Desenvolvimento Científico e Tecnológico

Coordenação de Aperfeiçoamento de Pessoal de Nível Superior

Air Force Office of Scientific Research

Natural Sciences and Engineering Research Council of Canada

Fundação Carlos Chagas Filho de Amparo à Pesquisa do Estado do Rio de Janeiro

Publisher

SAGE Publications

Cited by 1 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Using asymptotic homogenization and machine learning to derive a 3D trace theory for GFRP;Mechanics of Advanced Materials and Structures;2024-03-08

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