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.
Explore related subjects
Keep this discovery
Explore connections, maps & timelines
1997-03-01. Ceramic Matrix Composites: High Temperature Effects. (Latest Citations from the Aerospace Database). https://ntrs.nasa.gov/citations/19970024014
Cite the original work for its findings. Save a collection to share your selection of sources.