####### Case Information #######
Restart = False
InputFile = ../Grids/rae2822n462q3.gri
SurfaceMesh = ../Grids/rae2822_simple_BC.ebg
SavePrefix = OUT/RAE2822_RANS_Transonic_UniAdapt_TEST
BCFile = BCFile/RAE2822_RANS_Transonic
FuncFile = FuncFile/RAE2822_RANS_Transonic
BasisType = Lagrange
SolutionOrder = 2
PSequencing = False
CheckTruthMetricFileRoot = TrueMetric/RAE2822_RANS_Transonic_UniAdapt_TEST
###### NonLinear Solver ######
NonlinearSolver = Newton
nIter = 1000
NonlinearResidual = 1e-9
LocalUpdateFraction = True
UpdateFractionMin = 1e-1
SaveUpdateFraction = True
LineSearchFlag = Equation_l2_4and1andNone
###### Linear Solver ######
Preconditioner = ILU
PreconditionerSide = Right
ReorderingType = MDF
GMRES_Outer = 20
GMRES_Inner = 200
MinimumDecreaseFactor = 1e-3
AdaptiveResidualDecreaseFactorFlag = True
###### Temporal Parameters ######
LocalTimeStepping = True
CFLStart = 1e-1
CFLMin = 1e-2
CFLMax = 1e30
CFLIncreaseFactor = 2.0
CFLDecreaseFactor = 10.0
ScalarSourceCFLLimit = False
###### Shock capturing ######
ShockModel = PDE
ShockIndicator = Jump
ShockIntegrand = SpeedOfSound
ShockViscosityMatrix = Physical
###### Discretization Options ######
QuadratureOrder = -1
SourceDiscretization = AsymDualConsistent
###### Equation Set Parameters ######
EquationSet = RANS_SA2d
SutherlandRefTemp = 3.360136469926645E+00
SutherlandConstant = 1.288052313471881E+00
SpecificHeatRatio = 1.4
GasConstant = 0.4
PrandtlNumber = 0.71
FluxType = Roe
Viscosity = 1.538461538461538e-07
TurbulenceModel = SA
RansSourceDisc = AsymDualConsistent
SADCTermFlux = LaxFriedrichs
ViscEtaParameter = 6.000000
SA_ct3 = 0.0
SA_ct4 = 0.0
SA_chi_max_NDF = 400.0
ConstantViscosity = False
InitState = 1.000 0.9991 0.0403 3.8601 5.0 0.0
###### Output Parameters ######
Verbosity = Normal
LinearSolverVerbosity = Normal
WriteInterval = 0
######## Adjoint #############
Adjoint = Drag
InitAdjState = 0.0 0.0 0.0 0.0 0.0 0.0
AdjointResidual = 1e-8
####### ErrEst Parameters #######
nSmoothIter = 0
CFLSmoothStart = 1.0
PatchReconstructionH1 = False
NonlinearSmoother = Newton
SolvePrimalTruthSurrogate = False
SolveAdjointTruthSurrogate = True
NonlinearSmootherResidual = 1e-6
AdjointSmootherResidual = 1e-6
##### Adaptation specific #####
AdaptIter = 2
AdaptSpace = hp
AdaptMethod = Direct
OutputAdapted = Drag
CurvedMeshType = Elasticity
Mesher = Bamg
MaxRefineHFactor = 4.0
MaxCoarseHFactor = 2.0
MaxAnisotropy = 1000
InitialTargetDof = 3000
TargetDofIncreaseFactor = 1.0
#### Bamg ########
BamgRatio = 6.0
NbSmooth = 250
MaxVertices = 5000000
ViscAuxVariable = Hybrid
DualErrorFlag = False
ErrorEstimateFixP = True
MetricGradient = AffineInvariant
AnisotropicSampling = True
IsotropicSampling = True
ExtendedAnisotropicSampling = False
ExtendedIsotropicSampling = False
LocalSolveTruthSurrogate = False