Simulation of flow around oscillating rotor blade section with aeroelastic flap

Steijl, R. , Dehaeze, F., Barakos, G.N. , Garipova, L.I., Kusyumov, A.N. and Mikhailov, S.A. (2015) Simulation of flow around oscillating rotor blade section with aeroelastic flap. Russian Aeronautics (Iz VUZ), 58(4), pp. 419-425. (doi: 10.3103/S1068799815040108)

Abstract

Flows around rotor blade sections equipped with active flaps with a degree of freedom in the flap deflection angle are considered in this paper. Results for oscillating flaps are presented. The resultant flap motion was found to couple with the unsteady air loads for cases of blade section in oscillatory translation.

• Item Type: Articles
• Additional Information: Original Russian Text© R. Steijl, F. Dehaeze,, G.N. Barakos, L.I. Garipova, A.N. Kusyumov, S.A. Mikhailov, 2015, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2015, No. 4, pp. 55–61.
• Status: Published
• Refereed: Yes
• Glasgow Author(s) Enlighten ID: Barakos, Professor George and Steijl, Dr Rene and Dehaeze, Dr Florent
• Authors: Steijl, R., 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
• ISSN: 1068-7998
• ISSN (Online): 1934-7901
• Published Online: 05 April 2016
• Copyright Holders: Copyright © 2015 Allerton Press, Inc.
• First Published: First published in Russian Aeronautics (Iz VUZ) 58(4): 419-425
• Publisher Policy: Reproduced in accordance with the publisher copyright policy