A multiscale approach to composite failure, in which detailed information o
n small-scale micromechanics is incorporated approximately yet accurately i
nto larger-scale models capable of simulating extensive damage evolution an
d ultimate failure, is applied to the deformation and failure of a Ti-matri
x composite. The composite is reinforced with SiC fibers under conditions o
f matrix yielding and interfacial sliding via Coulomb friction. Specificall
y, a fully three-dimensional finite element model is employed to investigat
e the load transfer from broken to unbroken fibers as a function of applied
stress and interface friction coefficient. With a von Mises matrix yield c
riterion, constraint effects permit the matrix to carry some of the transfe
rred load near the fiber break, a feature not captured in previous composit
e models. The single-break results for stress concentrations are then used
as the discrete Green's functions for load transfer in the full composite,
and the predicted load transfer around a seven-fiber-break cluster is shown
in good agreement with finite element results. The Green's function model
is then used to predict overall damage evolution and composite failure for
an IMI-834 Ti/SCS-6 SiC system for various interface friction coefficients.
The composite tensile strength is rather insensitive to the friction coeff
icient and, for values of mu comparable to those measured experimentally, t
he predicted tensile strength is in excellent agreement with the measured v
alue. Analytic models for scaling of the tensile strength to very large siz
es are then shown to agree well with strengths obtained from simulations. T
hese results suggest that the hierarchical coupling approach used here may
be useful for approaching a wide variety of damage and failure problems in
fiber composites. (C) 2001 Acta Materialia Inc. Published by Elsevier Scien
ce Ltd. All rights reserved.