EPJ Web of Conferences
Volume 67, 2014EFM13 – Experimental Fluid Mechanics 2013
|Number of page(s)||4|
|Published online||25 March 2014|
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: firstname.lastname@example.org
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
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