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)
|
Text
151137.pdf - Accepted Version 1MB |
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.
| 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. |
| Status: | Published |
| Refereed: | Yes |
| 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: | 1068-7998 |
| 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 |
University Staff: Request a correction | Enlighten Editors: Update this record
Deposit and Record Details
Deposit and Record Details