Отправить статью по E-mail Numerical scheme of the second order of accuracy for vortex methods for incompressible flow simulation around airfoils
- Авторы: Kuz’mina K.1, Marchevskii I.1, Moreva V.1, Ryatina E.1
-
Учреждения:
- Bauman Moscow State Technical University
- Выпуск: Том 60, № 3 (2017)
- Страницы: 398-405
- Раздел: 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
Цитировать
Открытый доступ
Доступ предоставлен
Только для подписчиков
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.
Об авторах
K. Kuz’mina
Bauman Moscow State Technical University
Email: iliamarchevsky@mail.ru
Россия, ul. Vtoraya Baumanskaya 5, Moscow, 105005
I. Marchevskii
Bauman Moscow State Technical University
Автор, ответственный за переписку.
Email: iliamarchevsky@mail.ru
Россия, ul. Vtoraya Baumanskaya 5, Moscow, 105005
V. Moreva
Bauman Moscow State Technical University
Email: iliamarchevsky@mail.ru
Россия, ul. Vtoraya Baumanskaya 5, Moscow, 105005
E. Ryatina
Bauman Moscow State Technical University
Email: iliamarchevsky@mail.ru
Россия, ul. Vtoraya Baumanskaya 5, Moscow, 105005
