Simulation of flow around blade section with one degree of freedom aeroelastic flap

Steijl, R., Dehaeze, F., Barakos, G.N. , Garipova, L.I., Kusyumov, A.N. and Mikhailov, S.A. (2015) Simulation of flow around blade section with one degree of freedom aeroelastic flap. Russian Aeronautics (Iz VUZ), 58(2), pp. 193-198. (doi:10.3103/S1068799815020099)

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Abstract

In this paper, simulation is considered of flow around flapped rotor sections with a degree of freedom in the flap deflection angle. For steady state validation, comparisons one made of numerical results for the flow around a flapped wing with experimental data. Modelling of a blade section with an 1-DOF aeroelastic flap is also considered.

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. 2, pp. 54–59.
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
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:03 September 2015

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