Email this article Development of the discrete vortex cylinders method for calculating the helicopter rotor induced velocity
- Authors: Nikolaev E.I.1, Nikolaeva M.N.2
-
Affiliations:
- OAO Kazan Helicopters
- Tupolev Kazan National Research Technical University
- Issue: Vol 59, No 1 (2016)
- Pages: 8-14
- Section: 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
Cite item
Open Access
Access granted
Subscription Access
Abstract
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.
About the authors
E. I. Nikolaev
OAO Kazan Helicopters
Author for correspondence.
Email: nikjhon@yandex.ru
Russian Federation, ul. Tetsevskaya 87, Kazan, 420085
M. N. Nikolaeva
Tupolev Kazan National Research Technical University
Email: nikjhon@yandex.ru
Russian Federation, ul. Karla Marksa 10, Kazan, 420111
