电邮这篇文章 Effect of a Model and Boundary Conditions on the Results of Analyzing the Stress-Strain State of a Low-Pressure Compressor Rotor
- 作者: Arkhipov A.N.1, Volgina M.V.2, Matushkin A.A.1, Ravikovich Y.A.1, Kholobtsev D.P.1
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隶属关系:
- Moscow Aviation Institute (National Research University)
- NPO Saturn
- 期: 卷 61, 编号 4 (2018)
- 页面: 509-516
- 栏目: 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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详细
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.
作者简介
A. Arkhipov
Moscow Aviation Institute (National Research University)
编辑信件的主要联系方式.
Email: arkhipov.48@list.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993
M. Volgina
NPO Saturn
Email: arkhipov.48@list.ru
俄罗斯联邦, ul. Lenina 163, Rybinsk, 152903
A. Matushkin
Moscow Aviation Institute (National Research University)
Email: arkhipov.48@list.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993
Yu. Ravikovich
Moscow Aviation Institute (National Research University)
Email: arkhipov.48@list.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993
D. Kholobtsev
Moscow Aviation Institute (National Research University)
Email: arkhipov.48@list.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993
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