https://doi.org/10.1051/epjconf/201611402109
Numerical solution of inviscid and viscous laminar and turbulent flow around the airfoil
1 Dept. of Technical Mathematics, Faculty of Mechanical Eng., CTU in Prague, 121 35 Prague 1, Czech Rep.
2 Institute of Thermomechanics, Academy of Science CR, 182 00 Prague 8, Czech Rep.
a Corresponding author: m.slouka@seznam.cz
Published online: 28 March 2016
This work deals with the 2D numerical solution of inviscid compressible flow and viscous compressible laminar and turbulent flow around the profile. In a case of turbulent flow algebraic Baldwin-Lomax model is used and compared with Wilcox k-omega model. Calculations are done for NACA 0012 and RAE 2822 airfoil profile for the different angles of upstream flow. Numerical results are compared and discussed with experimental data.
© Owned by the authors, published by EDP Sciences, 2016
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
