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Civil Aviation High Technologies

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For citations:

Petrov Y.V., Ratenko O.A., Kharina V.K. The method of calculating the minimum creep rate of turbine blades of gas turbine engines based on the degradation of the alloy microstructure. Civil Aviation High Technologies. 2023;26(1):95-103. (In Russ.) https://doi.org/10.26467/2079-0619-2023-26-1-95-103



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ISSN 2079-0619 (Print)
ISSN 2542-0119 (Online)
Moscow State Technical University of Civil Aviation,
Kronshtadtskiy boulevard 20,
Moscow, Russia, 125993

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