Computational Research of the Main Rotor Hover and Vertical Descent States Based on the Nonlinear Blade Vortex Model
- Autores: Ignatkin Y.M.1, Makeev P.V.1, Shaidakov V.I.1, Shomov A.I.1
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Afiliações:
- Moscow Aviation Institute (National Research University)
- Edição: Volume 61, Nº 3 (2018)
- Páginas: 396-403
- Seção: Aero- and Gas-Dynamics of Flight Vehicles and Their Engines
- URL: https://journals.rcsi.science/1068-7998/article/view/230606
- DOI: https://doi.org/10.3103/S1068799818030121
- ID: 230606
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Resumo
The research is conducted of aerodynamic performance of the Mi-8 helicopter main rotor in the hover state and the vertical descent state, including vortex ring states (VRSs). Total and distributed aerodynamic performance, wake patterns, and main rotor flow patterns are calculated. The findings and results were compared with those provided by other researchers.
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Sobre autores
Yu. Ignatkin
Moscow Aviation Institute (National Research University)
Email: makeevpv@mail.ru
Rússia, Volokolamskoe sh. 4, Moscow, 125993
P. Makeev
Moscow Aviation Institute (National Research University)
Autor responsável pela correspondência
Email: makeevpv@mail.ru
Rússia, Volokolamskoe sh. 4, Moscow, 125993
V. Shaidakov
Moscow Aviation Institute (National Research University)
Email: makeevpv@mail.ru
Rússia, Volokolamskoe sh. 4, Moscow, 125993
A. Shomov
Moscow Aviation Institute (National Research University)
Email: makeevpv@mail.ru
Rússia, Volokolamskoe sh. 4, Moscow, 125993
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