Title of article
Numerical prediction of delamination onset in carbon/epoxy composites drilling
Author/Authors
Durمo، نويسنده , , L.M.P. and de Moura، نويسنده , , M.F.S.F. and Marques، نويسنده , , A.T.، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2008
Pages
12
From page
2767
To page
2778
Abstract
Despite the fact that their physical properties make them an 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).
te element model considering solid elements of the ABAQUS® 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.
Keywords
Delamination , Finite element , Carbon fibre laminates
Journal title
ENGINEERING FRACTURE MECHANICS
Serial Year
2008
Journal title
ENGINEERING FRACTURE MECHANICS
Record number
2342335
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