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NASA NTRS ยท 19970024014

Ceramic Matrix Composites: High Temperature Effects. (Latest Citations from the Aerospace Database)

Abstract

The bibliography contains citations concerning the development and testing of ceramic matrix composites for high temperature use. Tests examining effects of the high temperatures on bond strength, thermal degradation, oxidation, thermal stress, thermal fatigue, and thermal expansion properties are referenced. Applications of the composites include space structures, gas turbine and engine components, control surfaces for spacecraft and transatmospheric vehicles, heat shields, and heat exchangers.

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BibTeXRIS

1997-03-01. Ceramic Matrix Composites: High Temperature Effects. (Latest Citations from the Aerospace Database). https://ntrs.nasa.gov/citations/19970024014

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