电邮这篇文章 Numerical scheme of the second order of accuracy for vortex methods for incompressible flow simulation around airfoils
- 作者: Kuz’mina K.1, Marchevskii I.1, Moreva V.1, Ryatina E.1
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隶属关系:
- Bauman Moscow State Technical University
- 期: 卷 60, 编号 3 (2017)
- 页面: 398-405
- 栏目: 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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详细
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.
作者简介
K. Kuz’mina
Bauman Moscow State Technical University
Email: iliamarchevsky@mail.ru
俄罗斯联邦, ul. Vtoraya Baumanskaya 5, Moscow, 105005
I. Marchevskii
Bauman Moscow State Technical University
编辑信件的主要联系方式.
Email: iliamarchevsky@mail.ru
俄罗斯联邦, ul. Vtoraya Baumanskaya 5, Moscow, 105005
V. Moreva
Bauman Moscow State Technical University
Email: iliamarchevsky@mail.ru
俄罗斯联邦, ul. Vtoraya Baumanskaya 5, Moscow, 105005
E. Ryatina
Bauman Moscow State Technical University
Email: iliamarchevsky@mail.ru
俄罗斯联邦, ul. Vtoraya Baumanskaya 5, Moscow, 105005
