Development of the discrete vortex cylinders method for calculating the helicopter rotor induced velocity
- Авторы: Nikolaev E.1, Nikolaeva M.2
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Учреждения:
- OAO Kazan Helicopters
- Tupolev Kazan National Research Technical University
- Выпуск: Том 59, № 1 (2016)
- Страницы: 8-14
- Раздел: 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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Аннотация
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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Об авторах
E. Nikolaev
OAO Kazan Helicopters
Автор, ответственный за переписку.
Email: nikjhon@yandex.ru
Россия, ul. Tetsevskaya 87, Kazan, 420085
M. Nikolaeva
Tupolev Kazan National Research Technical University
Email: nikjhon@yandex.ru
Россия, ul. Karla Marksa 10, Kazan, 420111