Durability of Woven Polymer Matrix
Composites
S. R. Patel, S. W. Case, and K. L. Reifsnider
The use of composite systems as structural materials is growing. Composite systems
offer the advantage of being generally lighter and stiffer than traditional structural
materials such as metal and wood. However, very little is known about the effects of
moisture and temperature on the durability of composite systems. Moreover, testing these
materials proves time consuming and expensive. Consequently, a need has grown for life
prediction tools that assess the durability and reliability of composite material systems
with minimal effort.
Life prediction of composite materials represents a somewhat greater problem than life
prediction of metals because failure of metals is defined by a single flaw (e.g., a
crack). In composite material systems, defining failure is more complicated since single
flaws do not necessarily lead to critical degradation of material properties. In recent
years, many investigations have been made into prediction of remaining strength and life
of composite materials, leading up to the development of three main types of models:
residual strength degradation models, modulus reduction models, and damage tolerance
models. However, relatively few studies have been done in which environmental and
mechanical degradation processes are simultaneously imposed on material.
The authors of this paper will obtain residual strength and damage accumulation data on
an unaged composite material system (PR500/AS4 five harness satin weave) exposed to
typical aircraft temperature and moisture conditions during mechanical fatiguing. The goal
will be to use this data to develop models of damage and failure modes to predict
remaining strength and life of the material as a function of material properties and
environmental factors. Specifically, the models will be based on damage tolerance concepts
where remaining strength is used as a measure of damage accumulated in the composite and
failure is assumed to occur when the remaining strength equals the applied strength.