A detailed study has been undertaken of the pull-out behaviour of aramid fi
bres with different surface characteristics from blocks of an epoxy resin m
atrix. The fibres employed had either no surface treatment (HM), a standard
surface finish (HMF) or had been treated with a special epoxy-based adhesi
on-activating finish (HMA). The point-to-point variation of axial fibre str
ain along the fibres both inside and outside of the resin matrix has been d
etermined from stress-induced Raman band shifts. This has enabled the distr
ibution of interfacial shear stress along the fibre/matrix interface to be
determined and, in combination with scanning electron microscope analysis o
f the specimens following pull-out testing, the failure mechanisms to be el
ucidated. It is found that pull out of the HM fibre takes place by a debond
propagating along the fibre/matrix interface at a low level of interfacial
shear stress. The HMF fibre showed better adhesion to the epoxy matrix wit
h pull out occurring in a complex manner through both separation of the fib
re skin and failure at the fibre/finish interface. No evidence of debonding
was found for the HMA fibre and failure occurred by fracture of the fibre
at the point where it entered the resin block. (C) 2000 Kluwer Academic Pub
lishers.