Example simulation of a wing
A rectangular wing of aspect ratio
with a NACA0015 airfoil is considered. Experiments of such wing were performed by McAlister and Takahashi  at an angle of attack
deg and Reynolds number
. A structured grid with 1680 elements is used. The grid is scaled so that the chord of the wing is
m and the span
m. The freestream velocity is set to
m/s. The image below shows the pressure coefficient distribution.
The images below show the pressure coefficient at
. The experimental results from McAlister and Takahashi  are shown for comparison.
Good agreement between the simulation and the experimental results is observed.
 McAlister, K.W. and Takahashi, R.K., "NACA 0015 Wing Pressure and Trailing Vortex Measurements", 1991