Thermal Barrier Coatings for Gas-Turbine Engine Applications
By N. Padture, M. Gell, E. Jordan. Science, 2002
4,521 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Materials Chemistry
View Paper: https://www.semanticscholar.org/paper/318b388a44f8d3f83593c11d20cbb25a204eaf58
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In Aerospace Engineering
In Materials Chemistry
Citations in the corpus
- Protective coatings on zirconium-based alloys as accident-tolerant fuel (ATF) claddings (2017, background): “The utilization of coatings to protect structural materials, such as superal-loys, refractory metals, and carbon composites, from fast oxidation to improve the service life of components at elevated temperature always remains an important issue (Westwood et al., 1996; Padture et al., 2002).”
- Breakthrough applications of high-entropy materials (2018, background): “A bond coat is the necessary bond layer between the superalloy substrate and top coat of thermal barrier Y-stabilized zirconium oxide, providing good bonding and oxidation resistance.(16) Table III shows the comparison between the HEA bond coat of NiCo0.”