Enviar artigo por via de e-mail Calculation of a safety factor of damaged composite main rotor blade according to limit equilibrium theory
- Autores: Gorelov A.V.1, Nikolaev E.I.2, Sidorov I.N.3
-
Afiliações:
- Chistopol branch “Vostok”
- PAO Kazan Helicopters
- Tupolev Kazan National Research Technical University
- Edição: Volume 59, Nº 3 (2016)
- Páginas: 308-315
- Seção: 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
Citar
Acesso aberto
Acesso está concedido
Somente assinantes
Resumo
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.
Sobre autores
A. Gorelov
Chistopol branch “Vostok”
Autor responsável pela correspondência
Email: a.gorelov-kai@yandex.ru
Rússia, ul. Engelsa 127a, Chistopol, Tatarstan, 422981
E. Nikolaev
PAO Kazan Helicopters
Email: a.gorelov-kai@yandex.ru
Rússia, ul. Tetsevskaya 14, Kazan, Tatarstan, 420085
I. Sidorov
Tupolev Kazan National Research Technical University
Email: a.gorelov-kai@yandex.ru
Rússia, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
Arquivos suplementares
