Computational modeling of interference between helicopter main and tail rotors based on nonlinear blade vortex model
- Авторы: Ignatkin Y.M.1, Makeev P.V.1, Shomov A.I.1
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Учреждения:
- Moscow Aviation Institute (National Research University)
- Выпуск: Том 59, № 1 (2016)
- Страницы: 44-50
- Раздел: 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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Аннотация
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.
Об авторах
Yu. Ignatkin
Moscow Aviation Institute (National Research University)
Автор, ответственный за переписку.
Email: k102@mai.ru
Россия, Volokolamskoe shosse 4, Moscow, 125993
P. Makeev
Moscow Aviation Institute (National Research University)
Email: k102@mai.ru
Россия, Volokolamskoe shosse 4, Moscow, 125993
A. Shomov
Moscow Aviation Institute (National Research University)
Email: k102@mai.ru
Россия, Volokolamskoe shosse 4, Moscow, 125993
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