The high temperature processing of fibrous metal matrix composites has
been predicted to result in the development of large residual stresse
s because of a difference between the coefficients of thermal expansio
n (CTE) of the fibers and matrix. The R1 and R2 optical luminescence l
ine shifts of single crystal alpha-Al2O3 fibers embedded in a titanium
matrix have been measured using a fiber optic method and related to t
he reinforcing fiber's principal stresses. The fiber's axial stress co
mponent has been found to be more than twice that predicted by a conce
ntric cylinder's (CTE difference) model, whilst the fiber's radial (an
d hoop) direction stresses are smaller than expected. We propose that
the stress in these composites is affected by two presently unmodeled
effects: an elevation of composite's residual stress due to the large
CTE difference between the tooling used for processing of the composit
e and a relaxation of the transverse stress components by radial matri
x cracking. The result has important consequences for the manufacture
of metal matrix composites and for efforts to predict their mechanical
properties.