The objective of this effort was to evaluate and model the effects of moisture, temperature, and combined hygrothermal aging on the strength and life of a graphite/epoxy woven composite material system. The material system studied is a candidate for use in an advanced subsonic aircraft engine, and the imposed environmental and aging conditions were considered to be representative of the engine service conditions. Fatigue and residual strength data showed that initial and residual tensile properties and fatigue life of the material were only minimally affected by any of the imposed environmental conditions. However, fatigue damage progression and accumulation were found to vary with temperature and with different fatigue stress levels. Because of the lack of environmental effects on the residual strength data and life of the material, room temperature data were used in a residual strength based life prediction approach to model with reasonable results.


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    Durability of a Woven Polymer Matrix Composite in Aerospace Applications

    Case, S. W. / Patel, S. R. / American Institute of Aeronautics and Astronautics et al. | British Library Conference Proceedings | 2000



    Durability of Woven Polymer Matrix Composites

    Patel, S. R. / Case, S. W. / Reifsnider, K. L. et al. | British Library Conference Proceedings | 1998


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    Polymer composite applications to aerospace equipment

    McCarthy, R.F.J. / Haines, G.H. / Newley, R.A. | Tema Archive | 1994