Stepanov, R., Pakhov, V., Bozhenko, A., Batrakov, A., Garipova, L., Kusyumov, A., Mikhailov, S. and Barakos, G. N. (2017) Experimental and numerical study of rotor aeroacoustics. International Journal of Aeroacoustics, 16(6), pp. 460-475. (doi: 10.1177/1475472X17730447)
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Abstract
The work documents recent experiments at the Kazan National Research Technical University named after A.N. Tupolev (Kazan Aviation Institute), related to helicopter acoustics. The objective is to measure nar-field acoustics of rotors in hover and provide data suitable for computational fluid dynamics validation. The obtained set of data corresponds to a scaled rotor of known planform and the results are of high resolution. An advantage of the current dataset is that direct near-field acoustic data is made available and this allows for easy and direct comparisons with computational fluid dynamics predictions, without the need to use far-field aeroacoustic methods.
Item Type: | Articles |
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Additional Information: | Special issue after the Fourth International Workshop on Computational Experiments in Aeroacoustics (CEAA), Svetlogorsk, Russia, 21-24 September 2016. This work was supported by the grant ‘Numerical and physical modelling of aerodynamic and aeroacoustic characteristics of rotor systems of future concept aircarft' (No. 9.1577.2017/ P Ch) of the Ministry of Education and Science of the Russian Federation. |
Status: | Published |
Refereed: | Yes |
Glasgow Author(s) Enlighten ID: | Barakos, Professor George |
Authors: | Stepanov, R., Pakhov, V., Bozhenko, A., Batrakov, A., Garipova, L., Kusyumov, A., Mikhailov, S., and Barakos, G. N. |
College/School: | College of Science and Engineering > School of Engineering > Autonomous Systems and Connectivity |
Journal Name: | International Journal of Aeroacoustics |
Publisher: | SAGE Publications |
ISSN: | 1475-472X |
ISSN (Online): | 2048-4003 |
Published Online: | 21 September 2017 |
Copyright Holders: | Copyright © 2017 The Authors |
First Published: | First published in International Journal of Aeroacoustics 16(6): 460-475 |
Publisher Policy: | Reproduced in accordance with the publisher copyright policy |
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