Oxide Ceramic Matrix Composite Materials for Aero-Engine Applications: A Literature Review
نویسندگان
چکیده
The development of aircraft gas turbine engines has extensively been required for the advanced materials. This complex process is however justified by system-level benefits in terms reduced weight, higher temperature capability, and/or cooling, each which increases efficiency. where high-temperature ceramics have made considerable progress and ceramic matrix composites (CMCs) are foreground. CMCs classified into non-oxide oxide-based ones. Both families material types that a high potential use propulsion applications. Typical ones based on an oxide fiber (Ox-Ox). Some most common subcategories, alumina, beryllia, ceria, zirconia ceramics. Such used example combustion liners exhaust nozzles. However, until now thorough study available such applications not presented. paper focus assessing literature survey composite materials mechanical thermal properties.
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ژورنال
عنوان ژورنال: Advances in transdisciplinary engineering
سال: 2021
ISSN: ['2352-751X', '2352-7528']
DOI: https://doi.org/10.3233/atde210029