The objective of this effort was to evaluate and model the effects of moist
ure, temperature and combined hygrothermal conditions on the strength and l
ife of a graphite/epoxy woven composite material system. The material syste
m specified is a candidate for use in an advanced subsonic aircraft engine,
and the imposed environmental conditions were considered to be representat
ive of engine service conditions. Fatigue and residual strength data showed
that initial and residual tensile properties and fatigue life of the mater
ial were only minimally affected by any of the imposed environmental condit
ions for the fatigue stress levels considered in this study. Based on this
data, it was shown a residual-strength-based life prediction approach could
be used to model strength and life with reasonable results. Fatigue damage
progression and accumulation were found to be dependent on testing environ
ment, suggesting that more adverse effects of environment on strength and l
ife may be manifested for other types of loading (i.e., off-axis loading).
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