| nacaAirfoil | |
| ~~~~~~~~~~~ | |
| * large domain with airfoil section near centre | |
| * extremely non-orthogonal, highly skew mesh refined around the airfoil | |
| * running at Mach 1.78 | |
| * limited corrected 0.5 on all laplacianSchemes because the mesh is so poor | |
| * run to t = 0.02 with nextWrite; change to stopAt endTime to continue running | |
| * deltaT can be increased later in the run to 2e-07 | |