电邮这篇文章 Development of the discrete vortex cylinders method for calculating the helicopter rotor induced velocity
- 作者: Nikolaev E.1, Nikolaeva M.2
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隶属关系:
- OAO Kazan Helicopters
- Tupolev Kazan National Research Technical University
- 期: 卷 59, 编号 1 (2016)
- 页面: 8-14
- 栏目: 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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详细
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.
作者简介
E. Nikolaev
OAO Kazan Helicopters
编辑信件的主要联系方式.
Email: nikjhon@yandex.ru
俄罗斯联邦, ul. Tetsevskaya 87, Kazan, 420085
M. Nikolaeva
Tupolev Kazan National Research Technical University
Email: nikjhon@yandex.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, 420111
