Development of the discrete vortex cylinders method for calculating the helicopter rotor induced velocity
- Авторлар: Nikolaev E.1, Nikolaeva M.2
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Мекемелер:
- OAO Kazan Helicopters
- Tupolev Kazan National Research Technical University
- Шығарылым: Том 59, № 1 (2016)
- Беттер: 8-14
- Бөлім: 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
Дәйексөз келтіру
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.
Негізгі сөздер
Авторлар туралы
E. Nikolaev
OAO Kazan Helicopters
Хат алмасуға жауапты Автор.
Email: nikjhon@yandex.ru
Ресей, ul. Tetsevskaya 87, Kazan, 420085
M. Nikolaeva
Tupolev Kazan National Research Technical University
Email: nikjhon@yandex.ru
Ресей, ul. Karla Marksa 10, Kazan, 420111