Мақаланы E-mail арқылы жіберу Exploring the Detached-Eddy Simulation for Main Rotor Flows
- Авторлар: Dehaeze F.1, Barakos G.N.1, Kusyumov A.N.2, Kusyumov S.A.2, Mikhailov S.A.2
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Мекемелер:
- University of Glasgow, Glasgow G12 8QQ
- Tupolev Kazan National Research Technical University, ul. Karla Marksa 10
- Шығарылым: Том 61, № 1 (2018)
- Беттер: 37-44
- Бөлім: Aero- and Gas-Dynamics of Flight Vehicles and Their Engines
- URL: https://journals.rcsi.science/1068-7998/article/view/230392
- DOI: https://doi.org/10.3103/S1068799818010063
- ID: 230392
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Аннотация
This paper applies the Detached-Eddy Simulation (DES) method to resolve a larger part of the flow spectrum around rotor blades in hover and forward flight. A comparison between DES and Unsteady Reynolds–Averaged Navier–Stokes simulation was carried out for the case of a forward flying rotor suggesting that DES has great potential for rotor applications.
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Авторлар туралы
F. Dehaeze
University of Glasgow, Glasgow G12 8QQ
Email: postbox7@mail.ru
Ұлыбритания, Scotland
G. Barakos
University of Glasgow, Glasgow G12 8QQ
Email: postbox7@mail.ru
Ұлыбритания, Scotland
A. Kusyumov
Tupolev Kazan National Research Technical University, ul. Karla Marksa 10
Хат алмасуға жауапты Автор.
Email: postbox7@mail.ru
Ресей, Kazan Tatarstan, 420111
S. Kusyumov
Tupolev Kazan National Research Technical University, ul. Karla Marksa 10
Email: postbox7@mail.ru
Ресей, Kazan Tatarstan, 420111
S. Mikhailov
Tupolev Kazan National Research Technical University, ul. Karla Marksa 10
Email: postbox7@mail.ru
Ресей, Kazan Tatarstan, 420111
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