Отправить статью по E-mail Computational Research of the Main Rotor Hover and Vertical Descent States Based on the Nonlinear Blade Vortex Model
- Авторы: Ignatkin Y.M.1, Makeev P.V.1, Shaidakov V.I.1, Shomov A.I.1
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Учреждения:
- Moscow Aviation Institute (National Research University)
- Выпуск: Том 61, № 3 (2018)
- Страницы: 396-403
- Раздел: 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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Аннотация
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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Об авторах
Yu. Ignatkin
Moscow Aviation Institute (National Research University)
Email: makeevpv@mail.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
P. Makeev
Moscow Aviation Institute (National Research University)
Автор, ответственный за переписку.
Email: makeevpv@mail.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
V. Shaidakov
Moscow Aviation Institute (National Research University)
Email: makeevpv@mail.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
A. Shomov
Moscow Aviation Institute (National Research University)
Email: makeevpv@mail.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
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