Calculation of a safety factor of damaged composite main rotor blade according to limit equilibrium theory
- Авторлар: Gorelov A.1, Nikolaev E.2, Sidorov I.3
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Мекемелер:
- Chistopol branch “Vostok”
- PAO Kazan Helicopters
- Tupolev Kazan National Research Technical University
- Шығарылым: Том 59, № 3 (2016)
- Беттер: 308-315
- Бөлім: 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
Дәйексөз келтіру
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.
Авторлар туралы
A. Gorelov
Chistopol branch “Vostok”
Хат алмасуға жауапты Автор.
Email: a.gorelov-kai@yandex.ru
Ресей, ul. Engelsa 127a, Chistopol, Tatarstan, 422981
E. Nikolaev
PAO Kazan Helicopters
Email: a.gorelov-kai@yandex.ru
Ресей, ul. Tetsevskaya 14, Kazan, Tatarstan, 420085
I. Sidorov
Tupolev Kazan National Research Technical University
Email: a.gorelov-kai@yandex.ru
Ресей, ul. Karla Marksa 10, Kazan, Tatarstan, 420111