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NASA NTRS · 19930042278

Fatigue-environment interactions in a SiC/Ti-15-3 composite

Abstract

Load-controlled isothermal and nonisothermal fatigue lives of a (0-deg)s SiC/Ti-15-3 were evaluated at temperatures between 150 and 550 C and a target strain range of about 0.45 percent. In nonisothermal fatigue tests, load was first cycled at minimum temperature and then temperature was cycled at zero load. For fatigue tests with peak temperatures at or above 300 C, fatigue life was dramatically reduced compared to that at 150 C. The shortest life was produced by the nonisothermal test with the greatest temperature range (Delta T = 400 C) and highest peak temperature (T(max) = 550 C). Vacuum testing showed that much of the life reduction under isothermal and nonisothermal conditions was related to environmental effects, although the nature of the fatigue-environment interaction was decidedly different for the isothermal and nonisothermal test cycles which were studied.

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BibTeXRIS

Gayda, J., Gabb, T. P., Lerch, B. A.. 1993-01-01. Fatigue-environment interactions in a SiC/Ti-15-3 composite. https://ntrs.nasa.gov/citations/19930042278

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