Enviar artigo por via de e-mail Effect of a Model and Boundary Conditions on the Results of Analyzing the Stress-Strain State of a Low-Pressure Compressor Rotor
- Autores: Arkhipov A.N.1, Volgina M.V.2, Matushkin A.A.1, Ravikovich Y.A.1, Kholobtsev D.P.1
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Afiliações:
- Moscow Aviation Institute (National Research University)
- NPO Saturn
- Edição: Volume 61, Nº 4 (2018)
- Páginas: 509-516
- Seção: Structural Mechanics and Strength of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/230675
- DOI: https://doi.org/10.3103/S1068799818040025
- ID: 230675
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Resumo
The results of analyzing the stress-strain state in the critical zone of the low-pressure compressor rotor of the gas turbine engine at choosing different models of the rotor and boundary conditions are presented.
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Sobre autores
A. Arkhipov
Moscow Aviation Institute (National Research University)
Autor responsável pela correspondência
Email: arkhipov.48@list.ru
Rússia, Volokolamskoe sh. 4, Moscow, 125993
M. Volgina
NPO Saturn
Email: arkhipov.48@list.ru
Rússia, ul. Lenina 163, Rybinsk, 152903
A. Matushkin
Moscow Aviation Institute (National Research University)
Email: arkhipov.48@list.ru
Rússia, Volokolamskoe sh. 4, Moscow, 125993
Yu. Ravikovich
Moscow Aviation Institute (National Research University)
Email: arkhipov.48@list.ru
Rússia, Volokolamskoe sh. 4, Moscow, 125993
D. Kholobtsev
Moscow Aviation Institute (National Research University)
Email: arkhipov.48@list.ru
Rússia, Volokolamskoe sh. 4, Moscow, 125993
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