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: firstname.lastname@example.org
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.
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