1. David R. Clarke, Matthias Oechsner, and Nitin P. Padture, Thermal-barrier coatings for more efficient gas-turbine engines, MRS Bull., 2012, vol. 37, no. 10, pp. 891–898.
2. Moskal, G., Thermal barrier coatings: characteristics of microstructure and properties, generation and directions of development of bond, J. Ach. Mater. Manuf. Eng., 2009, vol. 37, no. 2, pp. 323–331.
3. Kumar, V. and Kandasubramanian, B., Processing and design methodologies for advanced and novel thermalbarrier coatings for engineering applications, Particuology, 2016, vol. 27, pp. 1–28. https://doi.org/10.1016/j.partic.2016.01.007
4. Kablov, E.N. and Muboyadzhyan, S.A., Heat-resistant coatings for the high-pressure turbine blades of promising GTES, Russ. Metall. (Metally), 2012, vol. 2012, no. 1, pp. 1–7. https://doi.org/10.1134/S0036029512010089
5. Chubarov, D.A. and Budnovskii, S.A., Selection of ceramic material for heat-protective coatings of aircraft engine turbine blades for operating temperatures up to 1400°C, Tr. VIAM, 2015. URL: http://viamworks.ru/ plugins/content/journal/uploads/articles/pdf/802.pdf (accessed January 28, 2018).