Abstract (EN):
This work reports on the experimental and numerical study of the bending behaviour of
two-dimensional adhesively-bonded scarf repairs of carbon-epoxy laminates, bonded with the
ductile adhesive Araldite 2015®. Scarf angles varying from 2 to 45º were tested. The experimental
work performed was used to validate a numerical Finite Element analysis using ABAQUS® and a
methodology developed by the authors to predict the strength of bonded assemblies. This
methodology consists on replacing the adhesive layer by cohesive elements, including mixed-mode
criteria to deal with the mixed-mode behaviour usually observed in structures. Trapezoidal laws in
pure modes I and II were used to account for the ductility of the adhesive used. The cohesive laws
in pure modes I and II were determined with Double Cantilever Beam and End-Notched Flexure
tests, respectively, using an inverse method. Since in the experiments interlaminar and transverse
intralaminar failures of the carbon-epoxy components also occurred in some regions, cohesive laws
to simulate these failure modes were also obtained experimentally with a similar procedure. A good
correlation with the experiments was found on the elastic stiffness, maximum load and failure mode
of the repairs, showing that this methodology simulates accurately the mechanical behaviour of
bonded assemblies.
Language:
English
Type (Professor's evaluation):
Scientific
No. of pages:
6
License type: