Coupled CFD/CSD simulation of the helicopter main rotor in high-speed forward flight

Dehaeze, F., Barakos, G.N. , Garipova, L.I., Kusyumov, A.N. and Mikhailov, S.A. (2017) Coupled CFD/CSD simulation of the helicopter main rotor in high-speed forward flight. Russian Aeronautics (Iz VUZ), 60(2), pp. 198-205. (doi: 10.3103/S1068799817020064)

151137.pdf - Accepted Version



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.

Item Type:Articles
Additional Information:This work was supported by the Ministry of Education and Science of the Russian Federation in the framework of project no. 9.1577.2017/PCh.
Glasgow Author(s) Enlighten ID:Barakos, Professor George and Dehaeze, Dr Florent
Authors: Dehaeze, F., Barakos, G.N., Garipova, L.I., Kusyumov, A.N., and Mikhailov, S.A.
College/School:College of Science and Engineering > School of Engineering > Autonomous Systems and Connectivity
Journal Name:Russian Aeronautics (Iz VUZ)
Publisher:MAIK Nauka/Interperiodica and Springer Verlag
ISSN (Online):1934-7901
Published Online:17 October 2017
Copyright Holders:Copyright © 2017 Allerton Press, Inc.
First Published:First published in Russian Aeronautics (Iz VUZ) 60(2):198-205
Publisher Policy:Reproduced in accordance with the copyright policy of the publisher

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