1. D. V. Ivchenko, P. K. Shtan’ko, N. V. Isaev, and I. Yu. Pavlov, “Erosion strength of the parts in the gas–air conduit of helicopter gas turbine engines during operation under air dustiness conditions. State of the art of the problem and a possible way of its solution,” Aviats.-Kosm. Tekh. Tekhnol., No. 7(15), 135–139 (2004).
2. J. H. Richardson, G. P. Sallee, and F. K. Smakula, “Causes of high temperature compressor deterioration in service,” in Proceedings of 15th Joint Propulsion Conference (Las Vegas, 19789), pp. AIAA-79–1234.
3. E. N. Kablov, S. A. Muboyadzhyan, S. A. Budinovskii, and A. N. Lutsenko, “Ion-Plasma protective coatings for gas-turbine engine blades,” Russian Metallurgy (Metally), No. 5, 413–424 (2007).
4. E. N. Kablov, S. A. Muboyadzhyan, and A. N. Lutsenko, “Nanostructured ion-plasma protective and hardening coatings for gas turbine engine blades,” Vopr. Materialoved., No. 2, 175–180 (2008).
5. S. A. Muboyadzhyan and Ya. A. Pomelov, “Erosion resistance of coatings deposited by high-energy plasmochemistry,” Vopr. Aviats. Nauki Tekhn., No. 1, 58–66 (1992).