foilC.afl
$GLOBAL,
	TITLE = 'Flow past a NACA0012 airfoil (C-Grid)',
	FOLDER = 'Cairfoil',
	SIMTYPE = 2,
	MACH = 0.799,
	REYNOLDS = 9000000.0,
	$END

$TURB,
	TURBTYPE = 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 = 0,	0,	0,
	VISCHEME = 0,
	VISCMON = 0,
	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 = 0.01,
	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 = 'foilC.PLOT3D',
	FILETYPE = 'PLOT3DF',
	ORDER = 3,
	ISIZE = 315,
	JSIZE = 40,
	KSIZE = 3,
	PERIODIC = 0, 0, 0,
	$END

comment:	Slip wall at J = 1
$FACEBC,
	BLOCK = 'mesh0',
	TYPE = 71,
	SIDE = 5,
	IBCS = 40,
	IBCE = 276,
	ISPLANE = 0,
	$END

comment:	C-condition at J = 1
$FACEBC,
	BLOCK = 'mesh0',
	TYPE = 9,
	SIDE = 5,
	IBCS = 40,
	IBCE = -40,
	$END

comment:	Free stream condition at I= 1
$FACEBC,
	BLOCK = 'mesh0',
	TYPE = 31,
	SIDE = 4,
	$END

comment:	Free stream condition at I= IE
$FACEBC,
	BLOCK = 'mesh0',
	TYPE = 31,
	SIDE = 2,
	$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 = 40-275
$FACEBC,
	BLOCK = 'mesh0',
	TYPE = 10,
	SIDE = 6,
	VARIABLE = 2,
	VALUE = 0.99875443478,
	IBCS = 40,
	IBCE = 275,
	$END


comment:	(Inlet) Dirichlett on v-vel at J = JE, i = 40-275
$FACEBC,
	BLOCK = 'mesh0',
	TYPE = 10,
	SIDE = 6,
	VARIABLE = 3,
	VALUE = 0.04989569016,
	IBCS = 40,
	IBCE = 275,
	$END

comment:	(Inlet) Dirichlett on W-vel at J = JE, i = 40-275
$FACEBC,
	BLOCK = 'mesh0',
	TYPE = 10,
	SIDE = 6,
	VARIABLE = 4,
	VALUE = 0.0,
	IBCS = 40,
	IBCE = 275,
	$END

comment:	(Inlet and Outlet) P = Pinfinity at J = JE, 
$FACEBC,
	BLOCK = 'mesh0',
	TYPE = 10,
	SIDE = 6,
	VARIABLE = 5,
	VALUE = 1.11886684746,
	$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