####### Case Information #######
Restart = True
InputFile = OUT/FlatPlate_RANS_SA2d_DIC_TEST_P3_Primal_0.pxa
SavePrefix = OUT/FlatPlate_RANS_SA2d_ADC_TEST
BCFile = BCFile/FlatPlate_RANS_SA2d
FuncFile = FuncFile/FlatPlate_RANS_SA2d
BasisType = Lagrange
SolutionOrder = 3
PSequencing = False
QuadratureOrder = -1
####### General Solver Information #######
NonlinearSolver = Newton
nIter = 500
UnderRelaxFactor = 1.0
NonlinearResidual = 1e-12
LocalUpdateFraction = True
UpdateFractionMin = 1e-1
SaveUpdateFraction = True
####### Linear Solver Information ####
Preconditioner = ILU
PreconditionerSide = Left
ReorderingType = MDF
GMRES_Outer = 20
GMRES_Inner = 100
###### Temporal parameters #######
LocalTimeStepping = True
CFLIncreaseFactor = 2.5
CFLStart = 1e10
CFLDecreaseFactor = 10
CFLMin = 1e-5
ScalarSourceCFLLimit = False
LineSearchFlag = Global_l2
####### Equation Set Specific #######
EquationSet = RANS_SA2d
TurbulenceModel = SA
FluxType = Roe
SpecificHeatRatio = 1.4
GasConstant = 0.4
Viscosity = 1.0e-7
ConstantViscosity = False
SutherlandRefTemp = 2.857142857142858e+01
SutherlandConstant = 8.903966538155421e+00
PrandtlNumber = 0.71
SA_ct3 = 0.0
SA_ct4 = 0.0
SA_chi_max_NDF = 1.0
InitState = 1.0 1.0 0.0 2.907142857142858e+01 5.0
####### Discretization Specific ######
ViscEtaParameter = 6.0
SADCTermFlux = LaxFriedrichs
RansSourceDisc = AsymDualConsistent
SourceDiscretization = AsymDualConsistent
ViscAuxVariable = Gradient
####### Output Parameters #######
Verbosity = Verbose