Enviar artigo por via de e-mail Development of the discrete vortex cylinders method for calculating the helicopter rotor induced velocity
- Autores: Nikolaev E.1, Nikolaeva M.2
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Afiliações:
- OAO Kazan Helicopters
- Tupolev Kazan National Research Technical University
- Edição: Volume 59, Nº 1 (2016)
- Páginas: 8-14
- Seção: Structural Mechanics and Strength of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/229533
- DOI: https://doi.org/10.3103/S1068799816010025
- ID: 229533
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Resumo
The numerical method for calculating the induced velocities of the helicopter rotor was developed based on Shaidakov’s disk theory. The numerical experiments were performed to test and estimate the method developed.
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Sobre autores
E. Nikolaev
OAO Kazan Helicopters
Autor responsável pela correspondência
Email: nikjhon@yandex.ru
Rússia, ul. Tetsevskaya 87, Kazan, 420085
M. Nikolaeva
Tupolev Kazan National Research Technical University
Email: nikjhon@yandex.ru
Rússia, ul. Karla Marksa 10, Kazan, 420111
