Мақаланы E-mail арқылы жіберу Coupled CFD/CSD simulation of the helicopter main rotor in high-speed forward flight
- Авторлар: Dehaeze F.1, Barakos G.N.2, Garipova L.I.3, Kusyumov A.N.3, Mikhailov S.A.3
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Мекемелер:
- University of Liverpool
- University of Glasgow
- Tupolev Kazan National Research Technical University
- Шығарылым: Том 60, № 2 (2017)
- Беттер: 198-205
- Бөлім: 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
Дәйексөз келтіру
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Рұқсат берілді
Тек жазылушылар үшін
Аннотация
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.
Негізгі сөздер
Авторлар туралы
F. Dehaeze
University of Liverpool
Email: info@pleiadesonline.com
Ұлыбритания, Liverpool, L69 3BX
G. Barakos
University of Glasgow
Email: info@pleiadesonline.com
Ұлыбритания, Glasgow, G12 8QQ
L. Garipova
Tupolev Kazan National Research Technical University
Email: info@pleiadesonline.com
Ресей, ul. Karla Marksa 10, Kazan, 420111 Tatarstan
A. Kusyumov
Tupolev Kazan National Research Technical University
Email: info@pleiadesonline.com
Ресей, ul. Karla Marksa 10, Kazan, 420111 Tatarstan
S. Mikhailov
Tupolev Kazan National Research Technical University
Email: info@pleiadesonline.com
Ресей, ul. Karla Marksa 10, Kazan, 420111 Tatarstan
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