Email this article Design and Experimental Analysis of Aircrew Design Parameters to Vertical Takeoff and Landing
- Authors: Gainutdinova T.Y.1, Gainutdinov V.G.2
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Affiliations:
- Kazan (Volga region) Federal University
- Tupolev Kazan National Research Technical University
- Issue: Vol 61, No 1 (2018)
- Pages: 8-13
- Section: Flight Vehicle Design
- URL: https://journal-vniispk.ru/1068-7998/article/view/230376
- DOI: https://doi.org/10.3103/S1068799818010026
- ID: 230376
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Abstract
The calculation of the design parameters of lifting airscrew systems with fixed and tilted rotor, including the investigation of the operation schemes of actuators for the propeller control system, is carried out.
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About the authors
T. Yu. Gainutdinova
Kazan (Volga region) Federal University
Author for correspondence.
Email: tgainut@mail.ru
Russian Federation, ul. Kremlevskaya 18, Kazan Tatarstan, 420008
V. G. Gainutdinov
Tupolev Kazan National Research Technical University
Email: tgainut@mail.ru
Russian Federation, ul. Karla Marksa 10 Tatarstan, Kazan, 420111
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