https://doi.org/10.1051/epjconf/20134501121
Numerical Solution of Compressible Steady Flows around the NACA 0012 Airfoil
1 Technical University of Liberec, Faculty of Mechanical Engineering, Czech Republic
2 Czech Technical University in Prague, Faculty of Mechanical Engineering, Czech Republic
The article presents results of a numerical solution of subsonic and transonic flows described by the system of Navier-Stokes equations in 2D laminar compressible flows around the NACA 0012 airfoil. Authors used Runge-Kutta method to numerically solve the flows around the NACA 0012 airfoil.
© Owned by the authors, published by EDP Sciences, 2013
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 2.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
