For citations:

Potapov V.A., Sanko A.A. Performance simulation of multi-stage axial-flow compressor of turbo-shaft engine with account for erosive wear nonlinearity of its blades. Civil Aviation High Technologies. 2020;23(5):39-53. (In Russ.) https://doi.org/10.26467/2079-0619-2020-23-5-39-53