foil.afl $GLOBAL, TITLE = 'Flow past a NACA0012 airfoil', FOLDER = 'airfoil', SIMTYPE = 2, MACH = 0.799, REYNOLDS = 9000000.0, GLOBINI = 1, $END $TURB, TURBTYPE = 5, NUMTRIPS = 2, POINT = 0.00001297455, 0.0004873857, 1.0, POINT = 0.0001298, -0.0016266, 1.0, PLANE = 0.0, 0.0, 1.0, PLANE = 30.0, 0.0, 0.0, PLANE = 15.0, 0.0, 2.0, $END $SPATIAL, SCHEME = 5, 5, -999, METRIC = 0, CUTOFFI = 0.05, CUTOFFJ = 0.05, CUTOFFK = 0.05, ISOTROPI = 0, ISOTROPJ = 0, ISOTROPK = 0, ICUT = 0, 0, 0, JCUT = 0, 0, 0, KCUT = 0, 0, 0, VISCOUS = 1, 1, 1, VISCHEME = 0, VISCMON = 1, SUTHERLN = 0.38, $END $TIMESTEP, SCHEME = 'BW2', MAXITER = 10000, GLOBALDT = 0.5E-3, SUBDT = 0.5E-3, $END $DAMPING, TYPE = 3, ES4 = 0.01, ES2 = 0.20, MAXRED = 1, FES4 = 2.0, FES2 = 1.0, OMGAV = 0.01, SRCONST = 0.0, FILTER = 0, 0, 0, NFILTER = 1, 1, 0, ALPHAN = 0.3, 0.3, 0.3, ALPHA2 = 0.3, 0.3, 0.3, ALPHA3 = 0.3, 0.3, 0.3, ALPHA4 = 0.3, 0.3, 0.3, ALPHA5 = 0.3, 0.3, 0.3, $END $OUTPUT, PRINTFRQ = 100, $END $DEBUG, POINT = 26, 4, 2, $END $BLOCK, NAME = 'mesh0', MESHFILE = 'foil.in', FILETYPE = 'AEROFLO', ORDER = 3, ISIZE = 245, JSIZE = 50, KSIZE = 3, PERIODIC = 1, 0, 1, $END comment: Solid wall at J = 1 $FACEBC, BLOCK = 'mesh0', TYPE = 1, SIDE = 5, $END comment: Free stream condition at J= JE $FACEBC, BLOCK = 'mesh0', TYPE = 32, SIDE = 6, $END comment: (Inlet) Dirichlett on u-vel at J = JE, i = 32-213 $FACEBC, BLOCK = 'mesh0', TYPE = 10, SIDE = 6, VARIABLE = 2, VALUE = 0.99875443478, IBCS = 32, IBCE = 213, $END comment: (Inlet) Dirichlett on v-vel at J = JE, i = 32-213 $FACEBC, BLOCK = 'mesh0', TYPE = 10, SIDE = 6, VARIABLE = 3, VALUE = 0.04989569016, IBCS = 32, IBCE = 213, $END comment: (Inlet) Dirichlett on W-vel at J = JE, i = 32-213 $FACEBC, BLOCK = 'mesh0', TYPE = 10, SIDE = 6, VARIABLE = 4, VALUE = 0.0, IBCS = 32, IBCE = 213, $END comment: (Inlet and Outlet) P = Pinfinity at J = JE, $FACEBC, BLOCK = 'mesh0', TYPE = 10, SIDE = 6, VARIABLE = 5, VALUE = 1.11886684746, $END $INITIAL VARIABLE = 2, VALUE = 0.99875443478, $END $INITIAL VARIABLE = 3, VALUE = 0.04989569016, $END