enum

const (
	Computable Adapt = iota
	ComputableRobust
	Full
	FullAdjoint
	FullFlow
	FullLinear
	GradAdjoint
	GradFlow
	GradFlowAdj
	NoAdapt
	Remaining
	Robust
	Smoothing
	SupersonicShock
	Twophase
	Wake
)

const (
	XAxis AxisOrientation = iota
	YAxis
	ZAxis
)

const (
	Jst Centered = iota
	JstKe
	Lax
	NoCentered
)

const (
	EulerEqns ContinuousEqns = iota
	NavierStokesEqns
)

const (
	Cauchy ConvergeCrit = iota
	Residual
)

const (
	ConstantStiffness DeformStiffness = iota
	InverseVolume
	WallDistance
)

const (
	NoneEqns DiscreteEqns = iota
	SaEqns
	SstEqns
)

const (
	GreenGauss FlowGradient = iota
	WeightedLeastSquares
)

const (
	Air21 Gasmodel = iota
	Air5
	Air7
	Argon
	ArgonSid
	N2
	NoModel
	O2
	Onespecies
)

const (
	Biparabolic GeoAnalytic = iota
	Cylinder
	Naca0012Airfoil
	Naca4412Airfoil
	NoGeoAnalytic
)

const (
	Function GeometryMode = iota
	Gradient
)

const (
	Aeroelastic Gridmovement = iota
	AeroelasticRigidMotion
	Deforming
	Elasticity
	External
	ExternalRotation
	FluidStructure
	MovingWall
	NoMovement
	RigidMotion
	RotatingFrame
)

const (
	XDir GustDir = iota
	YDir
)

const (
	Eog GustType = iota
	NoGust
	OneMCosine
	Sine
	TopHat
	Vortex
)

const (
	MassFlow InletType = iota
	TotalConditions
)

const (
	Cgns Input = iota
	NetcdfAscii
	Su2
)

const (
	Minmod Limiter = iota
	SharpEdges
	Venkatakrishnan
)

const (
	DeltaDragCoefficient LinearObj = iota
	DeltaLiftCoefficient
)

const (
	Bcgstab LinearSolver = iota
	ConjugateGradient
	Fgmres
	Newton
	QuasiNewton
	Rfgmres
	SteepestDescent
)

const (
	Jacobi LinearSolverPrec = iota
	Linelet
	LuSgs
)

const (
	AdjointProblem MathProblem = iota
	DirectProblem
	LinearizedProblem
)

const (
	DragCoefficient Objective = iota
	Efficiency
	EquivalentArea
	FigureOfMerit
	ForceXCoefficient
	ForceYCoefficient
	ForceZCoefficient
	FreeSurface
	InverseDesignHeatflux
	InverseDesignPressure
	LiftCoefficient
	MaxThickSec1
	MaxThickSec2
	MaxThickSec3
	MaxThickSec4
	MaxThickSec5
	MaxThickness
	MaximumHeatflux
	MinThickness
	MomentXCoefficient
	MomentYCoefficient
	MomentZCoefficient
	NearfieldPressure
	SideforceCoefficient
	ThrustCoefficient
	TorqueCoefficient
	TotalHeatflux
)

const (
	CgnsSol Output = iota
	Csv
	Excel
	Paraview
	Tecplot
	TecplotBinary
)

const (
	Density OutputVars = iota
	EddyVisc
	LamVisc
	Mach
	Pressure
	Temperature
	VelX
	VelY
	VelZ
)

const (
	Airfoil Param = iota
	CosineBump
	Displacement
	FfdCamber
	FfdCamber2d
	FfdControlPoint
	FfdControlPoint2d
	FfdDihedralAngle
	FfdRotation
	FfdSetting
	FfdThickness
	FfdThickness2d
	FfdTwistAngle
	Fourier
	HicksHenne
	Naca4digits
	Obstacle
	Parabolic
	Rotation
	Spherical
	Stretch
	SurfaceFile
)

const (
	Compressible Regime = iota
	Freesurface
	Incompressible
)

const (
	SensAoa Sens = iota
	SensAos
	SensGeometry
	SensMach
)

const (
	Bigrid SensSmoothing = iota
	NoSmooth
	Sobolev
)

const (
	AdjEuler Solver = iota
	AdjNavierStokes
	AdjRans
	AdjTne2Euler
	AdjTne2NavierStokes
	Euler
	FluidStructureEuler
	FluidStructureNavierStokes
	FluidStructureRans
	HeatEquation
	LinEuler
	LinNavierStokes
	LinearElasticity
	NavierStokes
	NoSolver
	PoissonEquation
	Rans
	TemplateSolver
	Tne2Euler
	Tne2NavierStokes
	WaveEquation
)

const (
	ChargeDist Source = iota
	NoSource
	PiecewiseConstant
	SourceTemplate
)

const (
	AutoDiff Sourcejac = iota
	FiniteDiff
	NoJacobian
)

const (
	NoConvective Space = iota
	SpaceCentered
	SpaceUpwind
)

const (
	FirstOrder SpatialOrder = iota
	SecondOrder
	SecondOrderLimiter
)

const (
	EulerExplicit TimeInt = iota
	EulerImplicit
	RungeKuttaExplicit
)

const (
	Lm TransModel = iota
	NoTransModel
)

const (
	Ml TurbModel = iota
	NoTurbModel
	Sa
	Sst
)

const (
	DtStepping1st Unsteady = iota
	DtStepping2nd
	RotationalFrame
	Steady
	TimeSpectral
	TimeStepping
)

const (
	Ausm Upwind = iota
	Ausmpwplus
	ConvectiveTemplate
	Cusp
	Hllc
	Msw
	NoUpwind
	Roe
	ScalarUpwind
	Sw
	Turkel
)

const (
	AvgGrad Viscous = iota
	AvgGradCorrected
	Galerkin
	NoViscous
)