Email this article Disk wing to main rotor conversion mechanics
- Authors: Pavlov V.V.1, Gasilov M.S.1
-
Affiliations:
- Tupolev Kazan National Research Technical University
- Issue: Vol 59, No 2 (2016)
- Pages: 161-167
- Section: Flight Vehicle Design
- URL: https://journals.rcsi.science/1068-7998/article/view/229640
- DOI: https://doi.org/10.3103/S1068799816020021
- ID: 229640
Cite item
Open Access
Access granted
Subscription Access
Abstract
A mathematical model of spatial motion of the disk wing blades converted to the main rotor is presented. The system linkage parameters are defined.
Keywords
About the authors
V. V. Pavlov
Tupolev Kazan National Research Technical University
Author for correspondence.
Email: diskolet@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
M. S. Gasilov
Tupolev Kazan National Research Technical University
Email: diskolet@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
