Oxidation Driven Damage on SiC/BN/SiC Ceramic Matrix Composite Aero-Engine Structures: An Iterative Computational Framework
Author:
Affiliation:
1. College of Science and Engineering, Nuclear Engineering, University of Derby, Markeaton Street Campus, Derby DE22 3AW, UK
2. Department of Industrial Engineering, Mechanical Engineering, University of Salerno, 84084 Fisciano, Italy
Abstract
Publisher
MDPI AG
Link
https://www.mdpi.com/1996-1944/17/12/3034/pdf
Reference32 articles.
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2. Karadimas, G., and Salonitis, K. (2023). Ceramic Matrix Composites for Aero Engine Applications—A Review. Appl. Sci., 13.
3. Royce, R. (2015). The Jet Engine, Wiley. [5th ed.].
4. Turbine blade temperature calculation and life estimation—A sensitivity analysis;Alizadeh;Propuls. Power,2013
5. DiCarlo, J.A. (2015). Advances in SiC/SiC Composites for Aero-Propulsion, in Ceramic Matrix Composites: Materials, Modelling and Technology, Wiley.
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