Estimates of hover aerodynamics performance of rotor model

Garipova, L.I., Batrakov, A.S., Kusyumov, A.N., Mikhailov, S.A. and Barakos, G.N. (2014) Estimates of hover aerodynamics performance of rotor model. Russian Aeronautics (Iz VUZ), 57(3), pp. 223-231. (doi:10.3103/S1068799814030027)

Full text not currently available from Enlighten.

Abstract

Hover computations were undertaken for a helicopter model rotor using Computational Fluid Dynamics (CFD). The influence of CFD mesh construction peculiarities and mesh parameters on the results was considered. Aerodynamics performance of the rotor were obtained including the rotor polar, loads per unit length, and vortical flow below the rotor disk was also visualized.

Item Type:Articles
Additional Information:Original Russian Text © L.I. Garipova, A.S. Batrakov, A.N. Kusyumov, S.A. Mikhailov, G.N. Barakos, 2014, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2014, No. 3, pp. 7–13.
Status:Published
Refereed:Yes
Glasgow Author(s) Enlighten ID:Barakos, Professor George
Authors: Garipova, L.I., Batrakov, A.S., Kusyumov, A.N., Mikhailov, S.A., and Barakos, G.N.
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:10 January 2015

University Staff: Request a correction | Enlighten Editors: Update this record