Enviar artigo por via de e-mail Computational modeling of interference between helicopter main and tail rotors based on nonlinear blade vortex model
- Autores: Ignatkin Y.M.1, Makeev P.V.1, Shomov A.I.1
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Afiliações:
- Moscow Aviation Institute (National Research University)
- Edição: Volume 59, Nº 1 (2016)
- Páginas: 44-50
- Seção: Aero- and Gas-Dynamics of Flight Vehicles and Their Engines
- URL: https://journals.rcsi.science/1068-7998/article/view/229553
- DOI: https://doi.org/10.3103/S1068799816010074
- ID: 229553
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Resumo
The Mi-2 helicopter was taken as an example for modeling the main and tail rotors operation with account for the interference at low speed sliding flight. Aerodynamic characteristics were calculated. The form of nonlinear vortical wake was obtained.
Sobre autores
Yu. Ignatkin
Moscow Aviation Institute (National Research University)
Autor responsável pela correspondência
Email: k102@mai.ru
Rússia, Volokolamskoe shosse 4, Moscow, 125993
P. Makeev
Moscow Aviation Institute (National Research University)
Email: k102@mai.ru
Rússia, Volokolamskoe shosse 4, Moscow, 125993
A. Shomov
Moscow Aviation Institute (National Research University)
Email: k102@mai.ru
Rússia, Volokolamskoe shosse 4, Moscow, 125993
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