Numerical Solution of Compressible Steady Flows around the RAE 2822 Airfoil

P. Kryštůfek; K. Kozel

doi:10.1051/epjconf/20146702061

EPJ

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Proceedings

Open Access

EPJ Web of Conferences 67, 02061 (2014)
https://doi.org/10.1051/epjconf/20146702061

Numerical Solution of Compressible Steady Flows around the RAE 2822 Airfoil

P. Kryštůfek¹^a and K. Kozel²

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: pavel.krystufek@tul.cz

Published online: 25 March 2014

Abstract

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.