The most predominant failure mechanism in carbon fiber reinforced composites is delamination. Dispersed second phase particles have been added to the interlayer region to reduce this damaging effect. In this work a phase field damage model is used to study Mode I crack propagation in particle-toughened interlayers. The simulations show several damage mechanisms observed in experiments and the processes that produce crack growth. In particular, failure involves multiple micro-cracks forming ahead of the main crack tip that coalesce and lead to crack branching, deflection and the formation of ligaments. Additionally, increasing the particle stiffness and the surface energy of the matrix-particle interface do not lead to an improvement of the interlaminate toughness as the fiber-matrix interface becomes a preferential path for the crack through the nucleation of extended delamination zones ahead of the crack tip. (C) 2016 Elsevier Ltd. All rights reserved.
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Univ Michigan, Dept Aerosp Engn, Ann Arbor, MI 48109 USA
Univ Michigan, Dept Mech Engn, Ann Arbor, MI 48109 USAUniv Michigan, Dept Aerosp Engn, Ann Arbor, MI 48109 USA
Rudraraju, Siva Shankar
Salvi, Amit
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Univ Michigan, Dept Aerosp Engn, Ann Arbor, MI 48109 USAUniv Michigan, Dept Aerosp Engn, Ann Arbor, MI 48109 USA
Salvi, Amit
Garikipati, Krishna
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Univ Michigan, Dept Mech Engn, Ann Arbor, MI 48109 USAUniv Michigan, Dept Aerosp Engn, Ann Arbor, MI 48109 USA
Garikipati, Krishna
Waas, Anthony M.
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Univ Michigan, Dept Aerosp Engn, Ann Arbor, MI 48109 USA
Univ Michigan, Dept Mech Engn, Ann Arbor, MI 48109 USAUniv Michigan, Dept Aerosp Engn, Ann Arbor, MI 48109 USA