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
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