Coupled CFD/CSD simulation of the helicopter main rotor in high-speed forward flight
- 作者: Dehaeze F.1, Barakos G.N.2, Garipova L.I.3, Kusyumov A.N.3, Mikhailov S.A.3
-
隶属关系:
- University of Liverpool
- University of Glasgow
- Tupolev Kazan National Research Technical University
- 期: 卷 60, 编号 2 (2017)
- 页面: 198-205
- 栏目: Aero- and Gas-Dynamics of Flight Vehicles and Their Engines
- URL: https://journals.rcsi.science/1068-7998/article/view/230074
- DOI: https://doi.org/10.3103/S1068799817020064
- ID: 230074
如何引用文章
详细
The helicopter main rotor in forward flight is considered in this paper. The results for rigid blades and elastic blades are compared by the method of coupled simulation. The influence of the structural damping coefficient on the blade in-flight deformation is also considered.
作者简介
F. Dehaeze
University of Liverpool
Email: info@pleiadesonline.com
英国, Liverpool, L69 3BX
G. Barakos
University of Glasgow
Email: info@pleiadesonline.com
英国, Glasgow, G12 8QQ
L. Garipova
Tupolev Kazan National Research Technical University
Email: info@pleiadesonline.com
俄罗斯联邦, ul. Karla Marksa 10, Kazan, 420111 Tatarstan
A. Kusyumov
Tupolev Kazan National Research Technical University
Email: info@pleiadesonline.com
俄罗斯联邦, ul. Karla Marksa 10, Kazan, 420111 Tatarstan
S. Mikhailov
Tupolev Kazan National Research Technical University
Email: info@pleiadesonline.com
俄罗斯联邦, ul. Karla Marksa 10, Kazan, 420111 Tatarstan
补充文件
