Email this article Dynamics of Main Rotor to Disk Wing Conversion
- Authors: Pavlov V.V.1, Gasilov M.S.1, Yusupov D.M.1
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Affiliations:
- Tupolev Kazan National Research Technical University
- Issue: Vol 61, No 1 (2018)
- Pages: 56-63
- Section: Aircraft and Rocket Engine Design and Development
- URL: https://journals.rcsi.science/1068-7998/article/view/230400
- DOI: https://doi.org/10.3103/S1068799818010099
- ID: 230400
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Abstract
The accelerations that emerge in the disk wing during rotation have been found. The loading of wing elements have been determined when the blades are extended and retracted.
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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
D. M. Yusupov
Tupolev Kazan National Research Technical University
Email: diskolet@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan Tatarstan, 420111
