1. Vorob’yev Yu.S., Romanenko V.N., Tishkovets E.V., et al. Oscillations of damaged turbine blades. Vibratsii v tekhnike i tekhnologiyakh, 2004, no. 5, pp. 47–51. (In Russ.).
2. Kataev V.A. High pressure compressor. Permskie aviatsionnye dvigateli, 2013, no. 27, pp. 52–53. (In Russ.).
3. Avgustinovich V.G., Kuznetsova T.A., Sultanov R.R. The identification of compressors’ pre-surge effects for use in an adaptive gas-turbine engine control system. Vestnik Permskogo natsional’nogo issledovatel’skogo politekhnicheskogo universiteta. Aerokosmicheskaya tekhnika [PNRPU Aerospace Engineering Bulletin], 2016, no. 46, pp. 126–143, doi: https://doi.org/10.15593/2224-9982/2016.46.07 (in Russ.).
4. Shabliy L.S., Kolmakova D.A., Krivtsov A.V. Parametric modeling of blade machines during optimization. Izvestiya Samarskogo nauchnogo tsentra RAN [Izvestia RAS SamSC], 2013, t. 15, no. 6-4, pp. 1013–1018. (In Russ.).
5. Korsov Yu.G., Tarabrin A.P., eds. Razrabotka, issledovanie i dovodka GTU, kompressorov, nagnetateley i ikh elementov [Design and adjustment of a gas turbine unit, compressor, injector and their elements]. Leningrad, NPO TsKTI Publ., 1990. 161 p. (In Russ.).