all[] 0 0 0.1 LEFT or RIGHT 0.1 25 1 1 5 1e-06 1 10 1e-06 velocity[0] = 0.; velocity[1] = 0.; velocity[2] = 0.; 101325 1 288.15 1 2 1 0 1.225 1.781e-05 1017.24 0.02495 0 0 0 0 0 0 AIRFOIL INLET OUTLET 1.45358 1.0 0. 0 1

250 all[] all[] 1 1

0.00001 1000 0 192