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