Email this article Disk wing to main rotor conversion mechanics
- Authors: Pavlov V.V.1, Gasilov M.S.1
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Affiliations:
- Tupolev Kazan National Research Technical University
- Issue: Vol 59, No 2 (2016)
- Pages: 161-167
- Section: Flight Vehicle Design
- URL: https://journal-vniispk.ru/1068-7998/article/view/229640
- DOI: https://doi.org/10.3103/S1068799816020021
- ID: 229640
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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.
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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
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