Мақаланы E-mail арқылы жіберу Computational modeling of interference between helicopter main and tail rotors based on nonlinear blade vortex model
- Авторлар: Ignatkin Y.M.1, Makeev P.V.1, Shomov A.I.1
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Мекемелер:
- Moscow Aviation Institute (National Research University)
- Шығарылым: Том 59, № 1 (2016)
- Беттер: 44-50
- Бөлім: 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.
Авторлар туралы
Yu. Ignatkin
Moscow Aviation Institute (National Research University)
Хат алмасуға жауапты Автор.
Email: k102@mai.ru
Ресей, Volokolamskoe shosse 4, Moscow, 125993
P. Makeev
Moscow Aviation Institute (National Research University)
Email: k102@mai.ru
Ресей, Volokolamskoe shosse 4, Moscow, 125993
A. Shomov
Moscow Aviation Institute (National Research University)
Email: k102@mai.ru
Ресей, Volokolamskoe shosse 4, Moscow, 125993
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