Email this article Numerical scheme of the second order of accuracy for vortex methods for incompressible flow simulation around airfoils
- Authors: Kuz’mina K.S.1, Marchevskii I.K.1, Moreva V.S.1, Ryatina E.P.1
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Affiliations:
- Bauman Moscow State Technical University
- Issue: Vol 60, No 3 (2017)
- Pages: 398-405
- Section: Aero- and Gas-Dynamics of Flight Vehicles and Their Engines
- URL: https://journal-vniispk.ru/1068-7998/article/view/229955
- DOI: https://doi.org/10.3103/S1068799816030114
- ID: 229955
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Abstract
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.
About the authors
K. S. Kuz’mina
Bauman Moscow State Technical University
Email: iliamarchevsky@mail.ru
Russian Federation, ul. Vtoraya Baumanskaya 5, Moscow, 105005
I. K. Marchevskii
Bauman Moscow State Technical University
Author for correspondence.
Email: iliamarchevsky@mail.ru
Russian Federation, ul. Vtoraya Baumanskaya 5, Moscow, 105005
V. S. Moreva
Bauman Moscow State Technical University
Email: iliamarchevsky@mail.ru
Russian Federation, ul. Vtoraya Baumanskaya 5, Moscow, 105005
E. P. Ryatina
Bauman Moscow State Technical University
Email: iliamarchevsky@mail.ru
Russian Federation, ul. Vtoraya Baumanskaya 5, Moscow, 105005
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