Мақаланы E-mail арқылы жіберу Numerical scheme of the second order of accuracy for vortex methods for incompressible flow simulation around airfoils
- Авторлар: Kuz’mina K.S.1, Marchevskii I.K.1, Moreva V.S.1, Ryatina E.P.1
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Мекемелер:
- Bauman Moscow State Technical University
- Шығарылым: Том 60, № 3 (2017)
- Беттер: 398-405
- Бөлім: Aero- and Gas-Dynamics of Flight Vehicles and Their Engines
- URL: https://journals.rcsi.science/1068-7998/article/view/229955
- DOI: https://doi.org/10.3103/S1068799816030114
- ID: 229955
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Аннотация
A high-accuracy numerical scheme is proposed for vortex methods of flow simulation around airfoils of arbitrary shape including airfoils with sharp edges, because it does not require the solution continuity on the airfoil.
Авторлар туралы
K. Kuz’mina
Bauman Moscow State Technical University
Email: iliamarchevsky@mail.ru
Ресей, ul. Vtoraya Baumanskaya 5, Moscow, 105005
I. Marchevskii
Bauman Moscow State Technical University
Хат алмасуға жауапты Автор.
Email: iliamarchevsky@mail.ru
Ресей, ul. Vtoraya Baumanskaya 5, Moscow, 105005
V. Moreva
Bauman Moscow State Technical University
Email: iliamarchevsky@mail.ru
Ресей, ul. Vtoraya Baumanskaya 5, Moscow, 105005
E. Ryatina
Bauman Moscow State Technical University
Email: iliamarchevsky@mail.ru
Ресей, ul. Vtoraya Baumanskaya 5, Moscow, 105005
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