Numerical Solution of Compressible Steady Flows around the RAE 2822 Airfoil
1 Technical University of Liberec, Faculty of Mechanical Engineering, Czech Republic
2 Czech Technical University in Prague, Faculty of Mechanical Engineering, Czech Republic
a Corresponding author: email@example.com
Published online: 25 March 2014
The article presents results of a numerical solution of subsonic, transonic and supersonic flows described by the system of Navier-Stokes equations in 2D laminar compressible flows around the RAE 2822 airfoil. Authors used FVM multistage Runge-Kutta method to numerically solve the flows around the RAE 2822 airfoil.
© Owned by the authors, published by EDP Sciences, 2014
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.