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
Cite item
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.
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
D. M. Yusupov
Tupolev Kazan National Research Technical University
Email: diskolet@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan Tatarstan, 420111