Мақаланы E-mail арқылы жіберу Effect of a Model and Boundary Conditions on the Results of Analyzing the Stress-Strain State of a Low-Pressure Compressor Rotor
- Авторлар: Arkhipov A.N.1, Volgina M.V.2, Matushkin A.A.1, Ravikovich Y.A.1, Kholobtsev D.P.1
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Мекемелер:
- Moscow Aviation Institute (National Research University)
- NPO Saturn
- Шығарылым: Том 61, № 4 (2018)
- Беттер: 509-516
- Бөлім: 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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Тек жазылушылар үшін
Аннотация
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.
Негізгі сөздер
Авторлар туралы
A. Arkhipov
Moscow Aviation Institute (National Research University)
Хат алмасуға жауапты Автор.
Email: arkhipov.48@list.ru
Ресей, Volokolamskoe sh. 4, Moscow, 125993
M. Volgina
NPO Saturn
Email: arkhipov.48@list.ru
Ресей, ul. Lenina 163, Rybinsk, 152903
A. Matushkin
Moscow Aviation Institute (National Research University)
Email: arkhipov.48@list.ru
Ресей, Volokolamskoe sh. 4, Moscow, 125993
Yu. Ravikovich
Moscow Aviation Institute (National Research University)
Email: arkhipov.48@list.ru
Ресей, Volokolamskoe sh. 4, Moscow, 125993
D. Kholobtsev
Moscow Aviation Institute (National Research University)
Email: arkhipov.48@list.ru
Ресей, Volokolamskoe sh. 4, Moscow, 125993
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