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 |
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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 > Autonomous Systems and Connectivity |
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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