Comparisons of Open-Hole Fatigue Strength Characteristics between Candidate High Temperature Polymer Matrix Composites for the Next Generation Aircraft(Composite 1)

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説明

One of critical technological issues for the realization of the supersonic transportation(SST) is to ensure the long-term high temperature structural integrity of advanced polymer matrix composite system. This research has been conducted as a part of long-term durability performance of composites and structures in Japan Supersonic Research Program for 2^<nd> Generation Supersonic Civil Transport. The final goal is to achieve through long-term and short-term tests under conditions simulating SST flight, development of associated predictive and accelerated test methods, and assessment of durability performances for design. This paper summarizes open-hole fatigue behavior for the interesting and candidate high temperature polymer matrix composites.

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