4.7 Article Proceedings Paper

Numerical prediction of delamination onset in carbon/epoxy composites drilling

Journal

ENGINEERING FRACTURE MECHANICS
Volume 75, Issue 9, Pages 2767-2778

Publisher

PERGAMON-ELSEVIER SCIENCE LTD
DOI: 10.1016/j.engfracmech.2007.03.009

Keywords

delamination; finite element; carbon fibre laminates

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Despite the fact that their physical properties make them art attractive family of materials, composites machining can cause several damage modes such as delamination, fibre pull-out, thermal degradation, and others. Minimization of axial thrust force during drilling reduces the probability of delamination onset, as it has been demonstrated by analytical models based on linear elastic fracture mechanics (LEFM). A finite element model considering solid elements of the ABAQUS (R) software library and interface elements including a cohesive damage model was developed in order to simulate thrust forces and delamination onset during drilling. Thrust force results for delamination onset are compared with existing analytical models. (c) 2008 Published by Elsevier Ltd.

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