A procedure involving iterative finite-element analyses has been developed
for the accurate prediction of the debond length as a function of force by
using the progressive debonding load/deflection data from fiber push-out te
sts conducted on a polyester/epoxy model composite with a thickness of appr
oximately 2.5 fiber diameters. The finite-element simulation included loads
due to chemical shrinkage of the matrix during cure as well as the boundar
y conditions corresponding to the exact probe and sample Support dimensions
. The resulting debond lengths corresponded to within 7% of the measured de
bond lengths. Fracture energy, was also determined by the finite-element me
thod by computing the change in potential energy when incrementing the inte
rface crack length by 0.1% of the total crack length and subtracting the in
crease in the energy dissipated by friction. (C) 1998 Elsevier Science Ltd.
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