foilm.afl
$GLOBAL,
	TITLE = 'Flow past a NACA0012 airfoil (multiblock)',
	FOLDER = 'airfoilm',
	SIMTYPE = 2,
	MACH = 0.799,
	REYNOLDS = 9000000.0,
	$END

$OVERSET,
	TYPE = 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 = 30000,
	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 = 0.0001,
	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,
	TECANIM = 0,
	TRANGE = 0,10000,5,
	$END

$DEBUG,
	POINT = 26, 4, 2,
	$END

$BLOCK,
	NAME = 'mesh0',
	MESHFILE = 'mesh0.plot3D',
	FILETYPE = 'PLOT3DF',
	ORDER = 3,
	ISIZE = 128,
	JSIZE = 50,
	KSIZE = 3,
	PERIODIC = 0, 0, 1,
	DONORS = 'mesh1',
	$END

$BLOCK,
	NAME = 'mesh1',
	MESHFILE = 'mesh1.plot3D',
	FILETYPE = 'PLOT3DF',
	ORDER = 3,
	ISIZE = 128,
	JSIZE = 50,
	KSIZE = 3,
	PERIODIC = 0, 0, 1,
	DONORS = 'mesh0',
	$END


comment:	BLOCK 1

comment:	1 (Inlet) Dirichlett on u-vel at J = JE; I = 48-128
comment:	@ 2.86 degree attack angle
$FACEBC,
	BLOCK = 'mesh0',
	TYPE = 10,
	SIDE = 6,
	VARIABLE = 2,
	VALUE = 0.99875443478,
	IBCS = 48,
	IBCE = 128,
	$END

comment:	2 (Inlet) Dirichlett on v-vel at J = JE; I = 48-128
comment:	@ 2.86 degree attack angle
$FACEBC,
	BLOCK = 'mesh0',
	TYPE = 10,
	SIDE = 6,
	VARIABLE = 3,
	VALUE = 0.04989569016,
	IBCS = 48,
	IBCE = 128,
	$END

comment:	3 (Inlet) Dirichlett on W-vel at J = JE, i = 48-128
$FACEBC,
	BLOCK = 'mesh0',
	TYPE = 10,
	SIDE = 6,
	VARIABLE = 4,
	VALUE = 0.0,
	IBCS = 48,
	IBCE = 128,
	$END

comment:	4 (Inlet and Outlet) P = Pinfinity at J = JE, i = 48-128
$FACEBC,
	BLOCK = 'mesh0',
	TYPE = 10,
	SIDE = 6,
	VARIABLE = 5,
	VALUE = 1.11886684746,
	IBCS = 48,
	IBCE = 128,
	$END

comment:	5 Characteristic Inflow at J = JE; I = 48-128
FACEBC,
	BLOCK = 'mesh0',
	TYPE = 41,
	SIDE = 6,
	IBCS = 48,
	IBCE = 128,
	ISPLANE = 0,
	CNORM = -1.0, -1.0, 0.0,
	$END


comment:	6 (Outlet) Freestream at J = JE; I = 1-47
$FACEBC,
	BLOCK = 'mesh0',
	TYPE = 32,
	SIDE = 6,
	IBCS = 1,
	IBCE = 47,
	$END


comment:	7 No-Slip wall at J = 1; I = 1-128
$FACEBC,
	BLOCK = 'mesh0',
	TYPE = 1,
	SIDE = 5,
	IBCS = 1,
	IBCE = 128,
	ISNORMAL = 1,
	ISPLANE = 0,
	$END


comment:	8 Overset boundary at i = 1
$FACEBC,
	BLOCK = 'mesh0',
	TYPE = 3,
	SIDE = 4,
	DEPTH = 3,
	$END

comment:	9 Overset boundary at i = IE
$FACEBC,
	BLOCK = 'mesh0',
	TYPE = 3,
	SIDE = 2,
	DEPTH = 3,
	$END



comment:	BLOCK 2

comment:	10 (Inlet) Dirichlett on u-vel at J = JE; I = 1-80
comment:	@ 2.86 degree attack angle
$FACEBC,
	BLOCK = 'mesh1',
	TYPE = 10,
	SIDE = 6,
	VARIABLE = 2,
	VALUE = 0.99875443478,
	IBCS = 1,
	IBCE = 80,
	$END

comment:	11 (Inlet) Dirichlett on v-vel at J = JE; I = 1-80
comment:	@ 2.86 degree attack angle
$FACEBC,
	BLOCK = 'mesh1',
	TYPE = 10,
	SIDE = 6,
	VARIABLE = 3,
	VALUE = 0.04989569016,
	IBCS = 1,
	IBCE = 80,
	$END

comment:	12 (Inlet) Dirichlett on W-vel at J = JE, i = 1-80
$FACEBC,
	BLOCK = 'mesh1',
	TYPE = 10,
	SIDE = 6,
	VARIABLE = 4,
	VALUE = 0.0,
	IBCS = 1,
	IBCE = 80,
	$END

comment:	13 (Inlet and Outlet) P = Pinfinity at J = JE, i = 1-80
$FACEBC,
	BLOCK = 'mesh1',
	TYPE = 10,
	SIDE = 6,
	VARIABLE = 5,
	VALUE = 1.11886684746,
	IBCS = 1,
	IBCE = 80,
	$END

comment:	14 Characteristic Inflow at J = 1; I = 1-80
FACEBC,
	BLOCK = 'mesh1',
	TYPE = 41,
	SIDE = 6,
	IBCS = 1,
	IBCE = 80,
	ISPLANE = 0,
	CNORM = -1.0, -1.0, 0.0,
	$END


comment:	15 (Outlet) Freestream at J = 1; I = 81-128
$FACEBC,
	BLOCK = 'mesh1',
	TYPE = 32,
	SIDE = 6,
	IBCS = 81,
	IBCE = 128,
	$END


comment:	16 No-Slip wall at J = JE; I = 1-128
$FACEBC,
	BLOCK = 'mesh1',
	TYPE = 1,
	SIDE = 5,
	IBCS = 1,
	IBCE = 128,
	ISNORMAL = 1,
	ISPLANE = 0,
	$END


comment:	17 Overset boundary at i = 1
$FACEBC,
	BLOCK = 'mesh1',
	TYPE = 3,
	SIDE = 4,
	DEPTH = 3,
	$END

comment:	18 Overset boundary at i = IE
$FACEBC,
	BLOCK = 'mesh1',
	TYPE = 3,
	SIDE = 2,
	DEPTH = 3,
	$END



comment:	Initial conditions on u-vel
comment:	@ 2.86 degree attack angle
$INITIAL,
	VARIABLE = 2,
	VALUE = 0.99875443478,
	$END

comment:	Initial Conditions on v-vel
comment:	@ 2.86 degree attack angle
$INITIAL,
	VARIABLE = 3,
	VALUE = 0.04989569016,
	$END