Email this article Coupled CFD/CSD simulation of the helicopter main rotor in high-speed forward flight
- Authors: Dehaeze F.1, Barakos G.N.2, Garipova L.I.3, Kusyumov A.N.3, Mikhailov S.A.3
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Affiliations:
- University of Liverpool
- University of Glasgow
- Tupolev Kazan National Research Technical University
- Issue: Vol 60, No 2 (2017)
- Pages: 198-205
- Section: 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
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Abstract
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.
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About the authors
F. Dehaeze
University of Liverpool
Email: info@pleiadesonline.com
United Kingdom, Liverpool, L69 3BX
G. N. Barakos
University of Glasgow
Email: info@pleiadesonline.com
United Kingdom, Glasgow, G12 8QQ
L. I. Garipova
Tupolev Kazan National Research Technical University
Email: info@pleiadesonline.com
Russian Federation, ul. Karla Marksa 10, Kazan, 420111 Tatarstan
A. N. Kusyumov
Tupolev Kazan National Research Technical University
Email: info@pleiadesonline.com
Russian Federation, ul. Karla Marksa 10, Kazan, 420111 Tatarstan
S. A. Mikhailov
Tupolev Kazan National Research Technical University
Email: info@pleiadesonline.com
Russian Federation, ul. Karla Marksa 10, Kazan, 420111 Tatarstan
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