NACA 0012 mesh file
I am wondering if anyone knows how SU2 got their coordinates for the airfoil shape because i am trying to edit the mesh file to use for a different airfoil shape. However, when using the normal NACA airfoil equation and the x coordinates given in the mesh file i am getting drastically different values. any info will be helpful thanks in advance
|
All times are GMT -4. The time now is 00:08. |