Enviar artigo por via de e-mail Dynamics of Main Rotor to Disk Wing Conversion
- Autores: Pavlov V.V.1, Gasilov M.S.1, Yusupov D.M.1
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Afiliações:
- Tupolev Kazan National Research Technical University
- Edição: Volume 61, Nº 1 (2018)
- Páginas: 56-63
- Seção: Aircraft and Rocket Engine Design and Development
- URL: https://journals.rcsi.science/1068-7998/article/view/230400
- DOI: https://doi.org/10.3103/S1068799818010099
- ID: 230400
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Resumo
The accelerations that emerge in the disk wing during rotation have been found. The loading of wing elements have been determined when the blades are extended and retracted.
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Sobre autores
V. Pavlov
Tupolev Kazan National Research Technical University
Autor responsável pela correspondência
Email: diskolet@mail.ru
Rússia, ul. Karla Marksa 10, Kazan Tatarstan, 420111
M. Gasilov
Tupolev Kazan National Research Technical University
Email: diskolet@mail.ru
Rússia, ul. Karla Marksa 10, Kazan Tatarstan, 420111
D. Yusupov
Tupolev Kazan National Research Technical University
Email: diskolet@mail.ru
Rússia, ul. Karla Marksa 10, Kazan Tatarstan, 420111
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