电邮这篇文章 Dynamics of Main Rotor to Disk Wing Conversion
- 作者: Pavlov V.1, Gasilov M.1, Yusupov D.1
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隶属关系:
- Tupolev Kazan National Research Technical University
- 期: 卷 61, 编号 1 (2018)
- 页面: 56-63
- 栏目: 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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详细
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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作者简介
V. Pavlov
Tupolev Kazan National Research Technical University
编辑信件的主要联系方式.
Email: diskolet@mail.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan Tatarstan, 420111
M. Gasilov
Tupolev Kazan National Research Technical University
Email: diskolet@mail.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan Tatarstan, 420111
D. Yusupov
Tupolev Kazan National Research Technical University
Email: diskolet@mail.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan Tatarstan, 420111
