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Formation of Gas Turbine Engine Parts from Heat-Resistant Alloys by the Pressure Method with Torsion under Isothermal Conditions (Technology and Equipment)

Crossref DOI link: https://doi.org/10.1134/S1052618824700419

Published Online: 2024-12-02

Published Print: 2024-12

Update policy: https://doi.org/10.1007/springer_crossmark_policy

Authors

Burlakov, I. A.

Utyashev, F. Z.

Ibragimov, A. R.

Sukhorukov, R. Yu.

Gavrilina, L. V.
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Text and Data Mining valid from 2024-12-01

Version of Record valid from 2024-12-01
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Article History

Received: 16 October 2023

Revised: 31 October 2023

Accepted: 20 April 2024

First Online: 2 December 2024

CONFLICT OF INTEREST

: The authors of this work declare that they have no conflicts of interest.

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