Analysis of stress state in a root-airfoil transition zone of hollow wide chord fan blades
- Авторы: Berdin V.K.1, Smyslov A.M.1, Berdin N.V.1, Luk’yanov V.V.1
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Учреждения:
- Ufa State Aviation Technical University
- Выпуск: Том 59, № 1 (2016)
- Страницы: 134-137
- Раздел: Aircraft and Rocket Engine Design and Development
- URL: https://journals.rcsi.science/1068-7998/article/view/229618
- DOI: https://doi.org/10.3103/S1068799816010219
- ID: 229618
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Аннотация
In this paper, under consideration is the complex approach to analyzing the operation of a simulator for the hollow blade made from the VT6 titanium alloy. The stress state parameters in the hollow-monolithic part transition zone of the cantilevered simulator at bending under the distributed load are determined.
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Об авторах
V. Berdin
Ufa State Aviation Technical University
Автор, ответственный за переписку.
Email: berdinvk@mail.ru
Россия, ul. Karla Marksa 12, Ufa, 450000
A. Smyslov
Ufa State Aviation Technical University
Email: berdinvk@mail.ru
Россия, ul. Karla Marksa 12, Ufa, 450000
N. Berdin
Ufa State Aviation Technical University
Email: berdinvk@mail.ru
Россия, ul. Karla Marksa 12, Ufa, 450000
V. Luk’yanov
Ufa State Aviation Technical University
Email: berdinvk@mail.ru
Россия, ul. Karla Marksa 12, Ufa, 450000
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