The flow part comparative analysis of a gas turbine engine intermediate casing with a starter generator integrated onto the rotor shaft

A. D. Kondryakov

Civil Aviation High Technologies
Nauchnyi Vestnik MGTU GA

ISSN 2079-0619 (Print)
ISSN 2542-0119 (Online)

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Kondryakov A.D. The flow part comparative analysis of a gas turbine engine intermediate casing with a starter generator integrated onto the rotor shaft. Civil Aviation High Technologies. 2026;29(2):93-105. (In Russ.) https://doi.org/10.26467/2079-0619-2026-29-2-93-105

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ISSN 2079-0619 (Print)
ISSN 2542-0119 (Online)

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Eliseev B.P.

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About the Author

A. D. Kondryakov
Moscow Aviation Institute (National Research University) ; Experimental Design Bureau named after A. M. Lyulka (Branch of PJSC UEC-UMPO)
Russian Federation

Arthur D. Kondryakov, Postgraduate Student and Assistant of the 203 Chair “Engine Design and Engineering”; The Head of the Stator Subdepartment in the Compressor Design Department

Moscow