Calculation of a safety factor of damaged composite main rotor blade according to limit equilibrium theory
- Авторы: Gorelov A.1, Nikolaev E.2, Sidorov I.3
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Учреждения:
- Chistopol branch “Vostok”
- PAO Kazan Helicopters
- Tupolev Kazan National Research Technical University
- Выпуск: Том 59, № 3 (2016)
- Страницы: 308-315
- Раздел: Structural Mechanics and Strength of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/229739
- DOI: https://doi.org/10.3103/S106879981603003X
- ID: 229739
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Аннотация
Safety factors of the Ansat helicopter main rotor blade are determined in the root section at various flight modes with taking into account the possible damages.
Об авторах
A. Gorelov
Chistopol branch “Vostok”
Автор, ответственный за переписку.
Email: a.gorelov-kai@yandex.ru
Россия, ul. Engelsa 127a, Chistopol, Tatarstan, 422981
E. Nikolaev
PAO Kazan Helicopters
Email: a.gorelov-kai@yandex.ru
Россия, ul. Tetsevskaya 14, Kazan, Tatarstan, 420085
I. Sidorov
Tupolev Kazan National Research Technical University
Email: a.gorelov-kai@yandex.ru
Россия, ul. Karla Marksa 10, Kazan, Tatarstan, 420111