Numerical Solution of Inviscid 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
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Published online: 6 May 2015
The article presents results of a numerical solution of subsonic, transonic and supersonic flows described by the system of Euler equations in 2D compressible flows around the RAE 2822 airfoil. Authors used FVM multistage Runge-Kutta method to numerically solve the flows around the RAE 2822 airfoil. The results are compared with the solution using the software Ansys Fluent 15.0.7.
© Owned by the authors, published by EDP Sciences, 2015
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