Email this article Effect of a Model and Boundary Conditions on the Results of Analyzing the Stress-Strain State of a Low-Pressure Compressor Rotor
- Authors: Arkhipov A.N.1, Volgina M.V.2, Matushkin A.A.1, Ravikovich Y.A.1, Kholobtsev D.P.1
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Affiliations:
- Moscow Aviation Institute (National Research University)
- NPO Saturn
- Issue: Vol 61, No 4 (2018)
- Pages: 509-516
- Section: 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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Abstract
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.
About the authors
A. N. Arkhipov
Moscow Aviation Institute (National Research University)
Author for correspondence.
Email: arkhipov.48@list.ru
Russian Federation, Volokolamskoe sh. 4, Moscow, 125993
M. V. Volgina
NPO Saturn
Email: arkhipov.48@list.ru
Russian Federation, ul. Lenina 163, Rybinsk, 152903
A. A. Matushkin
Moscow Aviation Institute (National Research University)
Email: arkhipov.48@list.ru
Russian Federation, Volokolamskoe sh. 4, Moscow, 125993
Yu. A. Ravikovich
Moscow Aviation Institute (National Research University)
Email: arkhipov.48@list.ru
Russian Federation, Volokolamskoe sh. 4, Moscow, 125993
D. P. Kholobtsev
Moscow Aviation Institute (National Research University)
Email: arkhipov.48@list.ru
Russian Federation, Volokolamskoe sh. 4, Moscow, 125993
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