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)

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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 > Aerospace Sciences
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

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