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An experimental evaluation of graphite/PEEK, APC-2, was carried out on specimens with various size holes acting under tension and compression loading. Quasiisotropic symmetrical laminates were tested at RT, 121, 135, and 149°C, and the Pipes three-parameter failure criterion was correlated with experimental results. Scanning electron microscopy photographs were used to determine specific notch effects on failure modes.
thermoplastic, strength, high temperature, compression, tension
Graduate student, Air Force Institute of Technology, Wright-Patterson Air Force Base, OH
Professor, Air Force Institute of Technology, Wright-Patterson Air Force Base, OH