CIncEulerSolver Class Reference

Main class for defining the incompressible Euler flow solver. More...

#include <CIncEulerSolver.hpp>

Inheritance diagram for CIncEulerSolver:

Public Member Functions
	CIncEulerSolver ()=delete
	CIncEulerSolver (CGeometry *geometry, CConfig *config, unsigned short iMesh, const bool navier_stokes=false)
	Constructor of the class.
	~CIncEulerSolver (void) override
	Destructor of the class.
CFluidModel *	GetFluidModel (void) const final
	Compute the pressure at the infinity.
void	SetTime_Step (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh, unsigned long Iteration) final
	Compute the time step for solving the Euler equations.
void	Centered_Residual (CGeometry *geometry, CSolver **solver_container, CNumerics **numerics_container, CConfig *config, unsigned short iMesh, unsigned short iRKStep) final
	Compute the spatial integration using a centered scheme.
void	Upwind_Residual (CGeometry *geometry, CSolver **solver_container, CNumerics **numerics_container, CConfig *config, unsigned short iMesh) final
	Compute the spatial integration using a upwind scheme.
void	Source_Residual (CGeometry *geometry, CSolver **solver_container, CNumerics **numerics_container, CConfig *config, unsigned short iMesh) final
	Source term integration.
void	Source_Template (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short iMesh) final
	Source term integration.
void	Preprocessing (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh, unsigned short iRKStep, unsigned short RunTime_EqSystem, bool Output) override
	Compute primitive variables and their gradients.
void	Evaluate_ObjFunc (const CConfig *config, CSolver **solver) final
	Compute weighted-sum "combo" objective output.
void	BC_Far_Field (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) final
	Impose the far-field boundary condition using characteristics.
void	BC_Inlet (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) final
	Impose a subsonic inlet boundary condition.
void	BC_Outlet (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) final
	Impose the outlet boundary condition.
void	ExplicitRK_Iteration (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iRKStep) final
	Update the solution using a Runge-Kutta scheme.
void	ClassicalRK4_Iteration (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iRKStep) final
	Update the solution using the classical Runge-Kutta 4 scheme.
void	ExplicitEuler_Iteration (CGeometry *geometry, CSolver **solver_container, CConfig *config) final
	Update the solution using the explicit Euler scheme.
void	PrepareImplicitIteration (CGeometry *geometry, CSolver **, CConfig *config) final
	Prepare an implicit iteration.
void	SetResidual_DualTime (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iRKStep, unsigned short iMesh, unsigned short RunTime_EqSystem) final
	Set the total residual adding the term that comes from the Dual Time Strategy.
void	LoadRestart (CGeometry **geometry, CSolver ***solver, CConfig *config, int val_iter, bool val_update_geo) final
	Load a solution from a restart file.
void	SetFreeStream_Solution (const CConfig *config) final
	Set the solution using the Freestream values.
void	PrintVerificationError (const CConfig *config) const final
	Print verification error to screen.
bool	GetHasHybridParallel () const final
	The incompressible Euler and NS solvers support MPI+OpenMP.
StreamwisePeriodicValues	GetStreamwisePeriodicValues () const final
	Get values for streamwise periodic flow: delta P, m_dot, inlet T, integrated heat, etc.
unsigned long	RegisterSolutionExtra (bool input, const CConfig *config) final
	Register In- or Output.
void	SetAdjoint_SolutionExtra (const su2activevector &adj_sol, const CConfig *config) final
	Seed the adjoint of the extra solution at the output.
void	ExtractAdjoint_SolutionExtra (su2activevector &adj_sol, const CConfig *config) final
	Extract the adjoint of the extra solution at the input.
void	ComputeEdgeMassFluxesRhieChow (CGeometry *geometry, CSolver **solver_container, CConfig *config) final
	Compute the spatial integration using a centered scheme.
void	ApplyPressureVelocityCorrection (CGeometry *geometry, CSolver **solver_container, CConfig *config) final
	Compute the spatial integration using a centered scheme.
Public Member Functions inherited from CFVMFlowSolverBase< CIncEulerVariable, ENUM_REGIME::INCOMPRESSIBLE >
void	Set_NewSolution () final
	Set the new solution variables to the current solution value for classical RK.
void	SetInitialCondition (CGeometry **geometry, CSolver ***solver_container, CConfig *config, unsigned long ExtIter) override
	Set the initial condition for the Euler Equations.
void	SetPrimitive_Gradient_GG (CGeometry *geometry, const CConfig *config, bool reconstruction=false) override
	Compute the gradient of the primitive variables using Green-Gauss method, and stores the result in the Gradient_Primitive variable.
void	SetPrimitive_Gradient_LS (CGeometry *geometry, const CConfig *config, bool reconstruction=false) final
	Compute the gradient of the primitive variables using a Least-Squares method, and stores the result in the Gradient_Primitive variable.
void	SetPrimitive_Limiter (CGeometry *geometry, const CConfig *config) final
	Compute the limiter of the primitive variables.
void	ImplicitEuler_Iteration (CGeometry *geometry, CSolver **solver_container, CConfig *config) final
	Implementation of implicit Euler iteration.
void	CompleteImplicitIteration (CGeometry *geometry, CSolver **, CConfig *config) final
	Complete an implicit iteration.
void	SetUniformInlet (const CConfig *config, unsigned short iMarker) final
	Set a uniform inlet profile.
void	SetInletAtVertex (const su2double *val_inlet, unsigned short iMarker, unsigned long iVertex) final
	Store of a set of provided inlet profile values at a vertex.
su2double	GetInletAtVertex (unsigned short iMarker, unsigned long iVertex, const CGeometry *geometry, su2double *val_inlet) const final
	Get the set of values imposed at an inlet.
void	BC_Euler_Wall (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) final
	Impose via the residual the Euler wall boundary condition.
void	MultigridProjectEulerWall (CGeometry *geometry, const CConfig *config, bool use_solution_old) override
	Enforce Euler wall BC on a restricted or prolongated multigrid solution by projecting the momentum to the tangent plane of the wall.
void	BC_Sym_Plane (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) override
	Impose the symmetry boundary condition using the residual.
void	BC_Periodic (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config) final
	Impose a periodic boundary condition by summing contributions from the complete control volume.
void	BC_Fluid_Interface (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config) final
	Impose the interface state across sliding meshes.
void	BC_Custom (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) final
	Impose a custom or verification boundary condition.
su2double	GetDensity_Inf (void) const final
	Compute the density at the infinity.
su2double	GetModVelocity_Inf (void) const final
	Compute 2-norm of the velocity at the infinity.
su2double	GetPressure_Inf (void) const final
	Compute the pressure at the infinity.
su2double	GetTemperature_Inf (void) const
	Get the temperature value at infinity.
su2double	GetVelocity_Inf (unsigned short val_dim) const final
	Get the velocity at the infinity.
su2double *	GetVelocity_Inf (void) final
	Get the velocity at the infinity.
void	SetVelocity_Inf (unsigned short val_dim, su2double val_velocity) final
	Set the velocity at infinity.
su2double	GetDensity_Energy_Inf (void) const final
	Compute the density multiply by energy at the infinity.
void	SetPressure_Inf (su2double p_inf) final
	Set the freestream pressure.
void	SetTemperature_Inf (su2double t_inf) final
	Set the freestream temperature.
void	SetDensity_Inf (su2double rho_inf) final
	Set the freestream temperature.
su2double	GetViscosity_Inf (void) const final
	Compute the viscosity at the infinity.
su2double	GetTke_Inf (void) const final
	Get the turbulent kinetic energy at the infinity.
su2double	GetOmega_Max (void) const final
	Get the max Omega.
su2double	GetStrainMag_Max (void) const final
	Get the max Strain rate magnitude.
su2double	GetCL_Inv (unsigned short val_marker) const final
	Provide the non dimensional lift coefficient (inviscid contribution).
su2double	GetCD_Inv (unsigned short val_marker) const final
	Provide the non dimensional drag coefficient (inviscid contribution).
su2double	GetSurface_CL (unsigned short val_marker) const final
	Provide the non dimensional lift coefficient.
su2double	GetSurface_CD (unsigned short val_marker) const final
	Provide the non dimensional drag coefficient.
su2double	GetSurface_CSF (unsigned short val_marker) const final
	Provide the non dimensional side-force coefficient.
su2double	GetSurface_CEff (unsigned short val_marker) const final
	Provide the non dimensional side-force coefficient.
su2double	GetSurface_CFx (unsigned short val_marker) const final
	Provide the non dimensional x force coefficient.
su2double	GetSurface_CFy (unsigned short val_marker) const final
	Provide the non dimensional y force coefficient.
su2double	GetSurface_CFz (unsigned short val_marker) const final
	Provide the non dimensional z force coefficient.
su2double	GetSurface_CMx (unsigned short val_marker) const final
	Provide the non dimensional x moment coefficient.
su2double	GetSurface_CMy (unsigned short val_marker) const final
	Provide the non dimensional y moment coefficient.
su2double	GetSurface_CMz (unsigned short val_marker) const final
	Provide the non dimensional z moment coefficient.
su2double	GetSurface_CL_Inv (unsigned short val_marker) const final
	Provide the non dimensional lift coefficient.
su2double	GetSurface_CD_Inv (unsigned short val_marker) const final
	Provide the non dimensional drag coefficient.
su2double	GetSurface_CSF_Inv (unsigned short val_marker) const final
	Provide the non dimensional side-force coefficient.
su2double	GetSurface_CEff_Inv (unsigned short val_marker) const final
	Provide the non dimensional side-force coefficient.
su2double	GetSurface_CFx_Inv (unsigned short val_marker) const final
	Provide the non dimensional x force coefficient.
su2double	GetSurface_CFy_Inv (unsigned short val_marker) const final
	Provide the non dimensional y force coefficient.
su2double	GetSurface_CFz_Inv (unsigned short val_marker) const final
	Provide the non dimensional z force coefficient.
su2double	GetSurface_CMx_Inv (unsigned short val_marker) const final
	Provide the non dimensional x moment coefficient.
su2double	GetSurface_CMy_Inv (unsigned short val_marker) const final
	Provide the non dimensional y moment coefficient.
su2double	GetSurface_CMz_Inv (unsigned short val_marker) const final
	Provide the non dimensional z moment coefficient.
su2double	GetSurface_CL_Mnt (unsigned short val_marker) const final
	Provide the non dimensional lift coefficient.
su2double	GetSurface_CD_Mnt (unsigned short val_marker) const final
	Provide the non dimensional drag coefficient.
su2double	GetSurface_CSF_Mnt (unsigned short val_marker) const final
	Provide the non dimensional side-force coefficient.
su2double	GetSurface_CEff_Mnt (unsigned short val_marker) const final
	Provide the non dimensional side-force coefficient.
su2double	GetSurface_CFx_Mnt (unsigned short val_marker) const final
	Provide the non dimensional x force coefficient.
su2double	GetSurface_CFy_Mnt (unsigned short val_marker) const final
	Provide the non dimensional y force coefficient.
su2double	GetSurface_CFz_Mnt (unsigned short val_marker) const final
	Provide the non dimensional z force coefficient.
su2double	GetSurface_CMx_Mnt (unsigned short val_marker) const final
	Provide the non dimensional x moment coefficient.
su2double	GetSurface_CMy_Mnt (unsigned short val_marker) const final
	Provide the non dimensional y moment coefficient.
su2double	GetSurface_CMz_Mnt (unsigned short val_marker) const final
	Provide the non dimensional z moment coefficient.
su2double	GetCSF_Inv (unsigned short val_marker) const final
	Provide the non dimensional sideforce coefficient (inviscid contribution).
su2double	GetCEff_Inv (unsigned short val_marker) const final
	Provide the non dimensional efficiency coefficient (inviscid contribution).
su2double	GetTotal_CSF () const final
	Provide the total (inviscid + viscous) non dimensional sideforce coefficient.
su2double	GetTotal_CEff () const final
	Provide the total (inviscid + viscous) non dimensional efficiency coefficient.
su2double	GetAeroCoeffsReferenceForce () const final
	Get the reference force used to compute CL, CD, etc.
su2double	GetReferenceDynamicPressure () const final
	Get the reference dynamic pressure, for Cp, Cf, etc.
su2double	GetTotal_CL () const final
	Provide the total (inviscid + viscous) non dimensional lift coefficient.
su2double	GetTotal_CD () const final
	Provide the total (inviscid + viscous) non dimensional drag coefficient.
su2double	GetTotal_CMx () const final
	Provide the total (inviscid + viscous) non dimensional x moment coefficient.
su2double	GetTotal_CMy () const final
	Provide the total (inviscid + viscous) non dimensional y moment coefficient.
su2double	GetTotal_CMz () const final
	Provide the total (inviscid + viscous) non dimensional z moment coefficient.
su2double	GetTotal_CoPx () const final
	Provide the total (inviscid + viscous) non dimensional x moment coefficient.
su2double	GetTotal_CoPy () const final
	Provide the total (inviscid + viscous) non dimensional y moment coefficient.
su2double	GetTotal_CoPz () const final
	Provide the total (inviscid + viscous) non dimensional z moment coefficient.
su2double	GetTotal_CFx () const final
	Provide the total (inviscid + viscous) non dimensional x force coefficient.
su2double	GetTotal_CFy () const final
	Provide the total (inviscid + viscous) non dimensional y force coefficient.
su2double	GetTotal_CFz () const final
	Provide the total (inviscid + viscous) non dimensional z force coefficient.
su2double	GetTotal_CT () const final
	Provide the total (inviscid + viscous) non dimensional thrust coefficient.
void	SetTotal_CT (su2double val_Total_CT) final
	Store the total (inviscid + viscous) non dimensional thrust coefficient.
su2double	GetTotal_CQ () const final
	Provide the total (inviscid + viscous) non dimensional torque coefficient.
void	SetTotal_CQ (su2double val_Total_CQ) final
	Store the total (inviscid + viscous) non dimensional torque coefficient.
su2double	GetTotal_CMerit () const final
	Provide the total (inviscid + viscous) non dimensional rotor Figure of Merit.
void	SetTotal_CD (su2double val_Total_CD) final
	Store the total (inviscid + viscous) non dimensional drag coefficient.
void	SetTotal_CL (su2double val_Total_CL) final
	Store the total (inviscid + viscous) non dimensional lift coefficient.
su2double	GetAllBound_CL_Inv () const final
	Get the inviscid contribution to the lift coefficient.
su2double	GetAllBound_CD_Inv () const final
	Get the inviscid contribution to the drag coefficient.
su2double	GetAllBound_CSF_Inv () const final
	Get the inviscid contribution to the sideforce coefficient.
su2double	GetAllBound_CEff_Inv () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CMx_Inv () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CMy_Inv () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CMz_Inv () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CoPx_Inv () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CoPy_Inv () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CoPz_Inv () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CFx_Inv () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CFy_Inv () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CFz_Inv () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CL_Mnt () const final
	Get the inviscid contribution to the lift coefficient.
su2double	GetAllBound_CD_Mnt () const final
	Get the inviscid contribution to the drag coefficient.
su2double	GetAllBound_CSF_Mnt () const final
	Get the inviscid contribution to the sideforce coefficient.
su2double	GetAllBound_CEff_Mnt () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CMx_Mnt () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CMy_Mnt () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CMz_Mnt () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CoPx_Mnt () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CoPy_Mnt () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CoPz_Mnt () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CFx_Mnt () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CFy_Mnt () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CFz_Mnt () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetSurface_CL_Visc (unsigned short val_marker) const final
	Provide the non dimensional lift coefficient.
su2double	GetSurface_CD_Visc (unsigned short val_marker) const final
	Provide the non dimensional drag coefficient.
su2double	GetSurface_CSF_Visc (unsigned short val_marker) const final
	Provide the non dimensional side-force coefficient.
su2double	GetSurface_CEff_Visc (unsigned short val_marker) const final
	Provide the non dimensional side-force coefficient.
su2double	GetSurface_CFx_Visc (unsigned short val_marker) const final
	Provide the non dimensional x force coefficient.
su2double	GetSurface_CFy_Visc (unsigned short val_marker) const final
	Provide the non dimensional y force coefficient.
su2double	GetSurface_CFz_Visc (unsigned short val_marker) const final
	Provide the non dimensional z force coefficient.
su2double	GetSurface_CMx_Visc (unsigned short val_marker) const final
	Provide the non dimensional x moment coefficient.
su2double	GetSurface_CMy_Visc (unsigned short val_marker) const final
	Provide the non dimensional y moment coefficient.
su2double	GetSurface_CMz_Visc (unsigned short val_marker) const final
	Provide the non dimensional z moment coefficient.
su2double	GetAllBound_CL_Visc () const final
	Get the inviscid contribution to the lift coefficient.
su2double	GetAllBound_CD_Visc () const final
	Get the inviscid contribution to the drag coefficient.
su2double	GetAllBound_CSF_Visc () const final
	Get the inviscid contribution to the sideforce coefficient.
su2double	GetAllBound_CEff_Visc () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CMx_Visc () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CMy_Visc () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CMz_Visc () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CoPx_Visc () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CoPy_Visc () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CoPz_Visc () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CFx_Visc () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CFy_Visc () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CFz_Visc () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetCL_Visc (unsigned short val_marker) const final
	Get the non dimensional lift coefficient (viscous contribution).
su2double	GetCSF_Visc (unsigned short val_marker) const final
	Get the non dimensional sideforce coefficient (viscous contribution).
su2double	GetCD_Visc (unsigned short val_marker) const final
	Get the non dimensional drag coefficient (viscous contribution).
su2double	GetSurface_HF_Visc (unsigned short val_marker) const final
	Get the total heat flux.
su2double	GetSurface_MaxHF_Visc (unsigned short val_marker) const final
	Get the maximum (per surface) heat flux.
void	SetTotal_CpDiff (su2double val_pressure) final
	Set the value of the Equivalent Area coefficient.
void	SetTotal_HeatFluxDiff (su2double val_heat) final
	Set the value of the Equivalent Area coefficient.
void	SetTotal_CEquivArea (su2double val_equiv) final
	Set the value of the Equivalent Area coefficient.
void	SetTotal_CNearFieldOF (su2double val_cnearfieldpress) final
	Set the value of the Near-Field pressure oefficient.
su2double	GetTotal_CpDiff () const final
	Provide the total (inviscid + viscous) non dimensional Equivalent Area coefficient.
su2double	GetTotal_HeatFluxDiff () const final
	Provide the total (inviscid + viscous) non dimensional Equivalent Area coefficient.
su2double	GetTotal_CEquivArea () const final
	Provide the total (inviscid + viscous) non dimensional Equivalent Area coefficient.
su2double	GetTotal_HeatFlux () const final
	Provide the total heat load.
su2double	GetTotal_MaxHeatFlux () const final
	Provide the total heat load.
void	SetTotal_HeatFlux (su2double val_Total_Heat) final
	Store the total heat load.
void	SetTotal_MaxHeatFlux (su2double val_Total_MaxHeat) final
	Store the total heat load.
su2double	GetCPressure (unsigned short val_marker, unsigned long val_vertex) const final
	Provide the Pressure coefficient.
su2double	GetCPressureTarget (unsigned short val_marker, unsigned long val_vertex) const final
	Provide the Target Pressure coefficient.
void	SetCPressureTarget (unsigned short val_marker, unsigned long val_vertex, su2double val_pressure) final
	Set the value of the target Pressure coefficient.
su2double *	GetCharacPrimVar (unsigned short val_marker, unsigned long val_vertex) final
	Value of the characteristic variables at the boundaries.
void	SetCharacPrimVar (unsigned short val_marker, unsigned long val_vertex, unsigned short val_var, su2double val_value) final
	Value of the characteristic variables at the boundaries.
su2double	GetInletTtotal (unsigned short val_marker, unsigned long val_vertex) const final
	Value of the total temperature at an inlet boundary.
su2double	GetInletPtotal (unsigned short val_marker, unsigned long val_vertex) const final
	Value of the total pressure at an inlet boundary.
su2double	GetInletFlowDir (unsigned short val_marker, unsigned long val_vertex, unsigned short val_dim) const final
	A component of the unit vector representing the flow direction at an inlet boundary.
void	SetInletTtotal (unsigned short val_marker, unsigned long val_vertex, su2double val_ttotal) final
	Set the value of the total temperature at an inlet boundary.
void	SetInletPtotal (unsigned short val_marker, unsigned long val_vertex, su2double val_ptotal) final
	Set the value of the total pressure at an inlet boundary.
void	SetInletFlowDir (unsigned short val_marker, unsigned long val_vertex, unsigned short val_dim, su2double val_flowdir) final
	Set a component of the unit vector representing the flow direction at an inlet boundary.
void	UpdateCustomBoundaryConditions (CGeometry **geometry_container, CSolver ***solver_container, CConfig *config) final
	Update the multi-grid structure for the customized boundary conditions.
void	UpdateFarfieldVelocity (const CConfig *config) final
	Updates the components of the farfield velocity vector.
void	ComputeVerificationError (CGeometry *geometry, CConfig *config) final
	Compute the global error measures (L2, Linf) for verification cases.
void	Pressure_Forces (const CGeometry *geometry, const CConfig *config) final
	Compute the pressure forces and all the adimensional coefficients.
void	Momentum_Forces (const CGeometry *geometry, const CConfig *config) final
	Compute the pressure forces and all the adimensional coefficients.
void	Friction_Forces (const CGeometry *geometry, const CConfig *config) final
	Compute the viscous forces and all the addimensional coefficients.
virtual void	Buffet_Monitoring (const CGeometry *geometry, const CConfig *config)
	Compute the buffet sensor.
void	SetSlidingStateStructure (unsigned short val_marker, unsigned long val_vertex) final
	Allocates the final pointer of SlidingState depending on how many donor vertex donate to it. That number is stored in SlidingStateNodes[val_marker][val_vertex].
void	SetSlidingState (unsigned short val_marker, unsigned long val_vertex, unsigned short val_state, unsigned long donor_index, su2double component) final
	Set the outer state for fluid interface nodes.
void	SetnSlidingStates (unsigned short val_marker, unsigned long val_vertex, int value) final
	Set the number of outer state for fluid interface nodes.
int	GetnSlidingStates (unsigned short val_marker, unsigned long val_vertex) const final
	Get the number of outer state for fluid interface nodes.
su2double	GetSlidingState (unsigned short val_marker, unsigned long val_vertex, unsigned short val_state, unsigned long donor_index) const final
	Get the outer state for fluid interface nodes.
void	SetConjugateHeatVariable (unsigned short val_marker, unsigned long val_vertex, unsigned short pos_var, su2double relaxation_factor, su2double val_var) final
	Set the conjugate heat variables.
su2double	GetConjugateHeatVariable (unsigned short val_marker, unsigned long val_vertex, unsigned short pos_var) const final
	Set the conjugate heat variables.
su2double	GetCSkinFriction (unsigned short val_marker, unsigned long val_vertex, unsigned short val_dim) const final
	Get the skin friction coefficient.
su2double	GetWallShearStress (unsigned short val_marker, unsigned long val_vertex) const final
	Get the wall shear stress.
su2double	GetHeatFlux (unsigned short val_marker, unsigned long val_vertex) const final
	Get the heat flux.
su2double	GetHeatFluxTarget (unsigned short val_marker, unsigned long val_vertex) const final
	Get the skin friction coefficient.
void	SetHeatFluxTarget (unsigned short val_marker, unsigned long val_vertex, su2double val_heat) final
	Set the value of the target Pressure coefficient.
su2double	GetYPlus (unsigned short val_marker, unsigned long val_vertex) const final
	Get the y plus.
su2double	GetUTau (unsigned short val_marker, unsigned long val_vertex) const final
	Get the u_tau .
su2double	GetEddyViscWall (unsigned short val_marker, unsigned long val_vertex) const final
	Get the eddy viscosity at the wall (wall functions).
const su2activevector *	GetEdgeMassFluxes () const final
	Get the mass fluxes across the edges (computed and stored during the discretization of convective fluxes).
Public Member Functions inherited from CSolver
	CSolver (LINEAR_SOLVER_MODE linear_solver_mode=LINEAR_SOLVER_MODE::STANDARD)
	Constructor of the class.
virtual	~CSolver (void)
	Destructor of the class.
CVariable *	GetNodes ()
	Allow outside access to the nodes of the solver, containing conservatives, primitives, etc.
const CVariable *	GetNodes () const
bool	HasPeriodicRotation (const CConfig &config) const
void	GetCommCountAndType (const CConfig *config, MPI_QUANTITIES commType, unsigned short &COUNT_PER_POINT, COMM_TYPE &MPI_TYPE) const
	Helper function to define the type and number of variables per point for each communication type.
void	InitiateComms (CGeometry *geometry, const CConfig *config, MPI_QUANTITIES commType)
	Routine to load a solver quantity into the data structures for MPI point-to-point communication and to launch non-blocking sends and recvs.
void	CompleteComms (CGeometry *geometry, const CConfig *config, MPI_QUANTITIES commType)
	Routine to complete the set of non-blocking communications launched by InitiateComms() and unpacking of the data in the solver class.
void	GetPeriodicCommCountAndType (const CConfig *config, unsigned short commType, unsigned short &COUNT_PER_POINT, COMM_TYPE &MPI_TYPE, unsigned short &ICOUNT, unsigned short &JCOUNT) const
	Helper function to define the type and number of variables per point for each communication type.
void	InitiatePeriodicComms (CGeometry *geometry, const CConfig *config, unsigned short val_periodic_index, unsigned short commType)
	Routine to load a solver quantity into the data structures for MPI periodic communication and to launch non-blocking sends and recvs.
void	CompletePeriodicComms (CGeometry *geometry, const CConfig *config, unsigned short val_periodic_index, unsigned short commType)
	Routine to complete the set of non-blocking periodic communications launched by InitiatePeriodicComms() and unpacking of the data in the solver class.
void	SetIterLinSolver (unsigned short val_iterlinsolver)
	Set number of linear solver iterations.
void	SetResLinSolver (su2double val_reslinsolver)
	Set the final linear solver residual.
void	SetResidual_RMS (const CGeometry *geometry, const CConfig *config, bool force=false)
	Set the value of the max residual and RMS residual.
void	SetResidual_BGS (const CGeometry *geometry, const CConfig *config)
	Communicate the value of the max residual and RMS residual.
void	ComputeResidual_Multizone (const CGeometry *geometry, const CConfig *config)
	Set the value of the max residual and RMS residual.
virtual void	SetDualTime_Mesh (void)
	Move the mesh in time.
bool	GetAdjoint (void) const
	Get information whether the initialization is an adjoint solver or not.
unsigned short	GetIterLinSolver (void) const
	Get number of linear solver iterations.
su2double	GetResLinSolver (void) const
	Get the final linear solver residual.
su2double	GetMax_Delta_Time (void) const
	Get the value of the maximum delta time.
su2double	GetMin_Delta_Time (void) const
	Get the value of the minimum delta time.
su2double	GetMax_CFL_Local (void) const
	Get the value of the maximum local CFL number.
su2double	GetMin_CFL_Local (void) const
	Get the value of the minimum local CFL number.
su2double	GetAvg_CFL_Local (void) const
	Get the value of the average local CFL number.
void	SetCFL_Local_Stats (su2double val_cfl)
	Set min/max/avg local CFL summary statistics.
unsigned short	GetnVar (void) const
	Get the number of variables of the problem.
unsigned short	GetnPrimVar (void) const
	Get the number of variables of the problem.
unsigned short	GetnPrimVarGrad (void) const
	Get the number of variables of the problem.
unsigned short	GetnSecondaryVar (void) const
	Get the number of variables of the problem.
unsigned short	GetnOutputVariables (void) const
	Get the number of variables of the problem.
su2double	GetRes_RMS (unsigned short val_var) const
	Get the maximal residual, this is useful for the convergence history.
su2double	GetRes_Max (unsigned short val_var) const
	Get the maximal residual, this is useful for the convergence history.
su2double	GetRes_BGS (unsigned short val_var) const
	Get the residual for BGS subiterations.
su2double	GetRes_Max_BGS (unsigned short val_var) const
	Get the maximal residual for BGS subiterations.
virtual su2double	GetRes_FEM (unsigned short val_var) const
	Get the residual for FEM structural analysis.
unsigned long	GetPoint_Max (unsigned short val_var) const
	Get the maximal residual, this is useful for the convergence history.
const su2double *	GetPoint_Max_Coord (unsigned short val_var) const
	Get the location of the maximal residual, this is useful for the convergence history.
unsigned long	GetPoint_Max_BGS (unsigned short val_var) const
	Get the maximal residual, this is useful for the convergence history.
const su2double *	GetPoint_Max_Coord_BGS (unsigned short val_var) const
	Get the location of the maximal residual, this is useful for the convergence history.
void	SetRotatingFrame_GCL (CGeometry *geometry, const CConfig *config)
	Set Value of the residual due to the Geometric Conservation Law (GCL) for steady rotating frame problems.
void	SetAuxVar_Gradient_GG (CGeometry *geometry, const CConfig *config)
	Compute the Green-Gauss gradient of the auxiliary variable.
void	SetAuxVar_Gradient_LS (CGeometry *geometry, const CConfig *config)
	Compute the Least Squares gradient of the auxiliary variable.
void	Add_External_To_Solution ()
	Add External to Solution vector.
void	Add_Solution_To_External ()
	Add the current Solution vector to External.
void	Update_Cross_Term (CConfig *config, su2passivematrix &cross_term)
	Update a given cross-term with relaxation and the running total (External).
void	SetSolution_Gradient_GG (CGeometry *geometry, const CConfig *config, short idxVel, bool reconstruction=false)
	Compute the Green-Gauss gradient of the solution.
void	SetSolution_Gradient_LS (CGeometry *geometry, const CConfig *config, short idxVel, bool reconstruction=false)
	Compute the Least Squares gradient of the solution.
void	SetGridVel_Gradient (CGeometry *geometry, const CConfig *config) const
	Compute the Least Squares gradient of the grid velocity.
void	SetSolution_Limiter (CGeometry *geometry, const CConfig *config)
	Compute slope limiter.
virtual su2double	GetFlameThickness () const
	A virtual member.
su2double	MUSCL_Reconstruction (const su2double *grad, const su2double *vector_ij, su2double delta_ij, su2double kappa, su2double ramp_val) const
	Compute the projection of a variable for MUSCL reconstruction.
virtual void	Set_OldSolution ()
	Set the old solution variables to the current solution value for Runge-Kutta iteration. It is a virtual function, because for the DG-FEM solver a different version is needed.
void	Restart_OldGeometry (CGeometry *geometry, CConfig *config) const
	Load the geometries at the previous time states n and nM1.
virtual void	CheckTimeSynchronization (CConfig *config, const su2double TimeSync, su2double &timeEvolved, bool &syncTimeReached)
	A virtual member.
virtual void	ProcessTaskList_DG (CGeometry *geometry, CSolver **solver_container, CNumerics **numerics, CConfig *config, unsigned short iMesh)
	A virtual member.
virtual void	ADER_SpaceTimeIntegration (CGeometry *geometry, CSolver **solver_container, CNumerics **numerics, CConfig *config, unsigned short iMesh, unsigned short RunTime_EqSystem)
	A virtual member.
virtual void	ComputeSpatialJacobian (CGeometry *geometry, CSolver **solver_container, CNumerics **numerics, CConfig *config, unsigned short iMesh, unsigned short RunTime_EqSystem)
	A virtual member.
virtual void	Postprocessing (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh)
	A virtual member.
virtual void	Postprocessing (CGeometry *geometry, CConfig *config, CNumerics **numerics, bool of_comp_mode=false)
	A virtual member, overloaded.
virtual void	Preprocessing (CGeometry *geometry, CSolver **solver_container, CConfig *config, CNumerics **numerics, unsigned short iMesh, unsigned long Iteration, unsigned short RunTime_EqSystem, bool Output)
	A virtual member overloaded.
virtual void	Set_Heatflux_Areas (CGeometry *geometry, CConfig *config)
	A virtual member.
virtual void	BC_Clamped (CGeometry *geometry, const CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_Clamped_Post (CGeometry *geometry, const CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_Sym_Plane (CGeometry *geometry, const CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_DispDir (CGeometry *geometry, const CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_Normal_Displacement (CGeometry *geometry, CNumerics *numerics, const CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_Normal_Load (CGeometry *geometry, const CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_Dir_Load (CGeometry *geometry, const CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_Sine_Load (CGeometry *geometry, const CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_Damper (CGeometry *geometry, const CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_ActDisk_Inlet (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_ActDisk_Outlet (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_ActDisk (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker, bool val_inlet_surface)
	A virtual member.
virtual void	BC_Isothermal_Wall (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_HeatFlux_Wall (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_HeatTransfer_Wall (const CGeometry *geometry, const CConfig *config, const unsigned short val_marker)
	Impose a heat flux by prescribing a heat transfer coefficient and a temperature at infinity.
virtual void	BC_Riemann (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_TurboRiemann (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	PreprocessBC_Giles (CGeometry *geometry, CConfig *config, CNumerics *conv_numerics, unsigned short marker_flag)
	It computes Fourier transformation for the needed quantities along the pitch for each span in turbomachinery analysis.
virtual void	BC_Giles (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	A virtual member.
virtual std::shared_ptr< CTurboOutput >	GetTurboBladePerformance () const
virtual void	BC_Inlet_Turbo (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_Inlet_MixingPlane (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_Supersonic_Inlet (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_Supersonic_Outlet (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_Engine_Inflow (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_Engine_Exhaust (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_ConjugateHeat_Interface (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_Smoluchowski_Maxwell (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	Impose_Fixed_Values (const CGeometry *geometry, const CConfig *config)
	Virtual function to apply something like a strong BC to the whole domain.
virtual su2double	GetMixingState (unsigned short val_marker, unsigned long val_span, unsigned short val_state) const
	Get a component of the donor-side averaged state at a mixing plane interface.
virtual void	SetMixingState (unsigned short val_marker, unsigned long val_span, unsigned short val_state, su2double component)
	Set a component of the donor-side averaged state at a mixing plane interface nodes.
void	AdaptCFLNumber (CGeometry **geometry, CSolver ***solver_container, CConfig *config)
	Adapt the CFL number based on the local under-relaxation parameters computed for each nonlinear iteration.
virtual void	IdentifySolutionOutliers (const CConfig *config, unsigned long iter)
	Identify points where the solution is an outlier (physics-specific concept) so that solvers can try to restore them to a stable condition.
void	ResetCFLAdapt ()
	Reset the local CFL adaption variables.
virtual void	ImplicitNewmark_Iteration (const CGeometry *geometry, CNumerics **numerics, const CConfig *config)
	A virtual member.
virtual void	ImplicitNewmark_Update (const CGeometry *geometry, const CConfig *config)
	A virtual member.
virtual void	ImplicitNewmark_Relaxation (const CGeometry *geometry, const CConfig *config)
	A virtual member.
virtual void	GeneralizedAlpha_Iteration (const CGeometry *geometry, CNumerics **numerics, const CConfig *config)
	A virtual member.
virtual void	GeneralizedAlpha_UpdateDisp (const CGeometry *geometry, const CConfig *config)
	A virtual member.
virtual void	GeneralizedAlpha_UpdateSolution (const CGeometry *geometry, const CConfig *config)
	A virtual member.
virtual void	GeneralizedAlpha_UpdateLoads (const CGeometry *geometry, const CConfig *config)
	A virtual member.
virtual void	Heat_Fluxes (CGeometry *geometry, CSolver **solver_container, CConfig *config)
	A virtual member.
virtual void	SetCSensitivity (unsigned short val_marker, unsigned long val_vertex, su2double val_sensitivity)
	A virtual member.
virtual void	SetForceProj_Vector (CGeometry *geometry, CSolver **solver_container, CConfig *config)
	A virtual member.
virtual void	SetTotal_NetThrust (su2double val_Total_NetThrust)
	A virtual member.
virtual void	SetTotal_Power (su2double val_Total_Power)
	A virtual member.
virtual void	SetTotal_SolidCD (su2double val_Total_SolidCD)
	A virtual member.
virtual void	SetTotal_ReverseFlow (su2double val_Total_ReverseFlow)
	A virtual member.
virtual void	SetTotal_MFR (su2double val_Total_MFR)
	A virtual member.
virtual void	SetTotal_Prop_Eff (su2double val_Total_Prop_Eff)
	A virtual member.
virtual void	SetTotal_ByPassProp_Eff (su2double val_Total_ByPassProp_Eff)
	A virtual member.
virtual void	SetTotal_Adiab_Eff (su2double val_Total_Adiab_Eff)
	A virtual member.
virtual void	SetTotal_Poly_Eff (su2double val_Total_Poly_Eff)
	A virtual member.
virtual void	SetTotal_IDC (su2double val_Total_IDC)
	A virtual member.
virtual void	SetTotal_IDC_Mach (su2double val_Total_IDC_Mach)
	A virtual member.
virtual void	SetTotal_IDR (su2double val_Total_IDR)
	A virtual member.
virtual void	SetTotal_DC60 (su2double val_Total_DC60)
	A virtual member.
virtual void	Inviscid_Sensitivity (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config)
	A virtual member.
virtual void	Smooth_Sensitivity (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config)
	A virtual member.
virtual void	Viscous_Sensitivity (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config)
	A virtual member.
su2double	GetTotal_ComboObj () const
	Provide the total "combo" objective (weighted sum of other values).
void	SetTotal_Custom_ObjFunc (su2double value)
	Sets the value of the custom objective function.
virtual su2double	GetSurface_Buffet_Metric (unsigned short val_marker) const
	A virtual member.
virtual su2double	GetInflow_MassFlow (unsigned short val_marker) const
	A virtual member.
virtual bool	FixedCL_Convergence (CConfig *config, bool convergence)
	A virtual member.
virtual bool	GetStart_AoA_FD (void) const
	A virtual member.
virtual bool	GetEnd_AoA_FD (void) const
	A virtual member.
virtual unsigned long	GetIter_Update_AoA (void) const
	A virtual member.
virtual su2double	GetPrevious_AoA (void) const
	A virtual member.
virtual su2double	GetAoA_inc (void) const
	A virtual member.
virtual su2double	GetExhaust_MassFlow (unsigned short val_marker) const
	A virtual member.
virtual su2double	GetInflow_Pressure (unsigned short val_marker) const
	A virtual member.
virtual su2double	GetInflow_Mach (unsigned short val_marker) const
	A virtual member.
virtual su2double	GetTotal_AvgTemperature () const
	A virtual member.
virtual su2double	GetTotal_AeroCD () const
	A virtual member.
virtual su2double	GetTotal_CFEA () const
	A virtual member.
virtual su2double	GetTotal_CNearFieldOF () const
	A virtual member.
virtual su2double	GetTotal_OFRefGeom () const
	A virtual member.
virtual su2double	GetTotal_OFRefNode () const
	A virtual member.
virtual su2double	GetTotal_OFVolFrac () const
	A virtual member.
virtual su2double	GetTotal_OFDiscreteness () const
	Retrieve the value of the discreteness objective function.
virtual su2double	GetTotal_OFCompliance () const
	A virtual member.
virtual su2double	GetTotal_OFStressPenalty () const
	A virtual member.
virtual bool	IsElementBased (void) const
	A virtual member.
virtual void	SetTotal_AeroCD (su2double val_aerocd)
	A virtual member.
virtual void	SetTotal_CFEA (su2double val_cfea)
	A virtual member.
virtual void	SetTotal_OFRefGeom (su2double val_ofrefgeom)
	A virtual member.
virtual void	SetTotal_OFRefNode (su2double val_ofrefnode)
	A virtual member.
virtual su2double	GetTotal_NetThrust () const
	A virtual member.
virtual su2double	GetTotal_Power () const
	A virtual member.
virtual su2double	GetTotal_SolidCD () const
	A virtual member.
virtual su2double	GetTotal_ReverseFlow () const
	A virtual member.
virtual su2double	GetTotal_MFR () const
	A virtual member.
virtual su2double	GetTotal_Prop_Eff () const
	A virtual member.
virtual su2double	GetTotal_ByPassProp_Eff () const
	A virtual member.
virtual su2double	GetTotal_Adiab_Eff () const
	A virtual member.
virtual su2double	GetTotal_Poly_Eff () const
	A virtual member.
virtual su2double	GetTotal_IDC () const
	A virtual member.
virtual su2double	GetTotal_IDC_Mach () const
	A virtual member.
virtual su2double	GetTotal_IDR () const
	A virtual member.
virtual su2double	GetTotal_DC60 () const
	A virtual member.
virtual su2double	GetTotal_Buffet_Metric () const
	A virtual member.
virtual unsigned long	GetDonorGlobalIndex (unsigned short val_marker, unsigned long val_vertex) const
	A virtual member.
virtual void	SetDonorGlobalIndex (unsigned short val_marker, unsigned long val_vertex, unsigned long val_index)
	A virtual member.
virtual void	SetCustomBoundaryScalar (unsigned short val_marker, unsigned long val_vertex, vector< passivedouble > val_customBoundaryScalar)
	Set the value of the customized normal scalar values/flux at a specified vertex on a specified marker.
virtual void	SetInlet_TurbVar (unsigned short val_marker, unsigned long val_vertex, unsigned short val_dim, su2double val_turb_var)
	A virtual member.
virtual su2double	GetBuffetSensor (unsigned short val_marker, unsigned long val_vertex) const
	A virtual member.
virtual su2double	GetPsiRho_Inf (void) const
	A virtual member.
virtual su2double	GetPsiE_Inf (void) const
	A virtual member.
virtual su2double	GetPhi_Inf (unsigned short val_dim) const
	A virtual member.
virtual su2double	GetTotal_Sens_Geo () const
	A virtual member.
virtual su2double	GetTotal_Sens_Mach () const
	A virtual member.
virtual su2double	GetTotal_Sens_AoA () const
	A virtual member.
virtual su2double	GetTotal_Sens_Press () const
	Set the total farfield pressure sensitivity coefficient.
virtual su2double	GetTotal_Sens_Temp () const
	Set the total farfield temperature sensitivity coefficient.
virtual su2double	GetTotal_Sens_BPress () const
	Get the total back pressure sensitivity coefficient.
virtual su2double	GetTotal_Sens_Density () const
	A virtual member.
virtual su2double	GetTotal_Sens_ModVel () const
	A virtual member.
virtual su2double	GetNuTilde_Inf (void) const
	A virtual member.
virtual su2double	GetOmega_Inf (void) const
	A virtual member.
virtual su2double	GetIntermittency_Inf () const
	Get value of the Intermittency.
virtual su2double	GetReThetaT_Inf () const
	Get value of the momentum thickness Reynolds number.
virtual su2double	GetTotal_Sens_E (unsigned short iVal) const
	A virtual member.
virtual su2double	GetTotal_Sens_Nu (unsigned short iVal) const
	A virtual member.
virtual su2double	GetTotal_Sens_Rho (unsigned short iVal) const
	A virtual member.
virtual su2double	GetTotal_Sens_Rho_DL (unsigned short iVal) const
	A virtual member.
virtual su2double	GetTotal_Sens_EField (unsigned short iEField) const
	A virtual member.
virtual su2double	GetTotal_Sens_DVFEA (unsigned short iDVFEA) const
	A virtual member.
virtual su2double	GetVal_Young (unsigned short iVal) const
	A virtual member.
virtual su2double	GetVal_Poisson (unsigned short iVal) const
	A virtual member.
virtual su2double	GetVal_Rho (unsigned short iVal) const
	A virtual member.
virtual su2double	GetVal_Rho_DL (unsigned short iVal) const
	A virtual member.
virtual unsigned short	GetnEField (void) const
	A virtual member.
virtual unsigned short	GetnDVFEA (void) const
	A virtual member.
virtual su2double	GetVal_EField (unsigned short iVal) const
	A virtual member.
virtual su2double	GetVal_DVFEA (unsigned short iVal) const
	A virtual member.
virtual su2double	GetCSensitivity (unsigned short val_marker, unsigned long val_vertex) const
	A virtual member.
virtual const su2double *	GetConstants () const
	A virtual member.
virtual void	SetForceCoeff (su2double val_forcecoeff_history)
	A virtual member.
virtual void	SetRelaxCoeff (su2double val_relaxcoeff_history)
	A virtual member.
virtual void	SetFSI_Residual (su2double val_FSI_residual)
	A virtual member.
virtual su2double	GetForceCoeff (void) const
	A virtual member.
virtual su2double	GetRelaxCoeff (void) const
	A virtual member.
virtual su2double	GetFSI_Residual (void) const
	A virtual member.
virtual void	PredictStruct_Displacement (CGeometry *geometry, const CConfig *config)
	A virtual member.
virtual void	ComputeAitken_Coefficient (CGeometry *geometry, const CConfig *config, unsigned long iOuterIter)
	A virtual member.
virtual void	SetAitken_Relaxation (CGeometry *geometry, const CConfig *config)
	A virtual member.
void	BasicLoadRestart (CGeometry *geometry, const CConfig *config, const string &filename, unsigned long skipVars)
	Loads the solution from the restart file.
void	Read_SU2_Restart_ASCII (CGeometry *geometry, const CConfig *config, string val_filename)
	Read a native SU2 restart file in ASCII format.
void	Read_SU2_Restart_Binary (CGeometry *geometry, const CConfig *config, string val_filename)
	Read a native SU2 restart file in binary format.
void	Read_SU2_Restart_Metadata (CGeometry *geometry, CConfig *config, bool adjoint_run, const string &val_filename) const
	Read the metadata from a native SU2 restart file (ASCII or binary).
void	LoadInletProfile (CGeometry **geometry, CSolver ***solver, CConfig *config, int val_iter, unsigned short val_kind_solver, unsigned short val_kind_marker) const
	Load a inlet profile data from file into a particular solver.
virtual void	LoadRestart_FSI (CGeometry *geometry, CConfig *config, int val_iter)
	A virtual member.
virtual unsigned short	Get_iElem_iDe (unsigned long iElem) const
	A virtual member.
virtual void	Set_DV_Val (su2double val_EField, unsigned short i_DV)
	A virtual member.
virtual su2double	Get_DV_Val (unsigned short i_DV) const
	A virtual member.
void	GaussElimination (su2double **A, su2double *rhs, unsigned short nVar)
	Gauss method for solving a linear system.
void	Aeroelastic (CSurfaceMovement *surface_movement, CGeometry *geometry, CConfig *config, unsigned long TimeIter)
	Prepares and solves the aeroelastic equations.
void	SetUpTypicalSectionWingModel (vector< vector< su2double > > &PHI, vector< su2double > &w, CConfig *config)
	Sets up the generalized eigenvectors and eigenvalues needed to solve the aeroelastic equations.
void	SolveTypicalSectionWingModel (CGeometry *geometry, su2double Cl, su2double Cm, CConfig *config, unsigned short val_Marker, vector< su2double > &displacements)
	Solve the typical section wing model.
virtual void	RegisterSolution (CGeometry *geometry_container, CConfig *config)
	A virtual member.
virtual void	RegisterOutput (CGeometry *geometry_container, CConfig *config)
	A virtual member.
virtual void	SetAdjoint_Output (CGeometry *geometry, CConfig *config)
	A virtual member.
virtual void	ExtractAdjoint_Solution (CGeometry *geometry, CConfig *config, bool CrossTerm)
	A virtual member.
virtual void	SetSurface_Sensitivity (CGeometry *geometry, CConfig *config)
	A virtual member.
virtual void	SetSensitivity (CGeometry *geometry, CConfig *config, CSolver *target_solver=nullptr)
	A virtual member. Extract and set the geometrical sensitivity.
virtual void	SetFSI_ConvValue (unsigned short val_index, su2double val_criteria)
	A virtual member.
virtual su2double	GetFSI_ConvValue (unsigned short val_index) const
	A virtual member.
virtual su2double	Compute_LoadCoefficient (su2double CurrentTime, su2double RampTime, const CConfig *config)
	A virtual member.
virtual void	Compute_StiffMatrix (CGeometry *geometry, CNumerics **numerics, const CConfig *config)
	A virtual member.
virtual void	Compute_StiffMatrix_NodalStressRes (CGeometry *geometry, CNumerics **numerics, const CConfig *config)
	A virtual member.
virtual void	Compute_MassMatrix (const CGeometry *geometry, CNumerics **numerics, const CConfig *config)
	A virtual member.
virtual void	Compute_MassRes (const CGeometry *geometry, CNumerics **numerics, const CConfig *config)
	A virtual member.
virtual void	Compute_NodalStressRes (CGeometry *geometry, CNumerics **numerics, const CConfig *config)
	A virtual member.
virtual void	Compute_BodyForces (CGeometry *geometry, CNumerics **numerics, const CConfig *config)
	A virtual member.
virtual void	SetVolumetricHeatSource (CGeometry *geometry, CConfig *config)
	A virtual member. Set the volumetric heat source.
virtual void	Solve_System (CGeometry *geometry, CConfig *config)
	A virtual member.
virtual void	SetWAitken_Dyn_tn1 ()
	A virtual member.
virtual void	SetLoad_Increment (unsigned long iInc, su2double loadInc)
	A virtual member.
virtual su2double	GetLoad_Increment () const
	A virtual member.
virtual void	SetRecording (CGeometry *geometry, CConfig *config)
	A virtual member.
virtual void	RegisterVariables (CGeometry *geometry, CConfig *config, bool reset=false)
	A virtual member.
virtual void	ExtractAdjoint_Variables (CGeometry *geometry, CConfig *config)
	A virtual member.
virtual su2double *	GetVecSolDOFs (void)
	A virtual member.
virtual unsigned long	GetnDOFsGlobal (void) const
	A virtual member.
virtual void	InitTurboContainers (CGeometry *geometry, CConfig **config, unsigned short iZone)
	A virtual member.
virtual vector< su2double >	GetTurboPrimitive (unsigned short iBlade, unsigned short iSpan, bool Inlet)
	Get Primal variables for turbo performance computation iteration can be executed by multiple threads.
virtual void	PreprocessAverage (CSolver **solver, CGeometry *geometry, CConfig *config, unsigned short marker_flag)
	virtual member.
virtual void	TurboAverageProcess (CSolver **solver, CGeometry *geometry, CConfig *config, unsigned short marker_flag)
	virtual member.
virtual void	GatherInOutAverageValues (CConfig *config, CGeometry *geometry)
	virtual member.
virtual void	ComputeTurboBladePerformance (CGeometry *geometry, CConfig *config, unsigned short iBlade)
virtual su2double	GetAverageDensity (unsigned short valMarker, unsigned short valSpan) const
	A virtual member.
virtual su2double	GetAverageMassFlowRate (unsigned short valMarker) const
	virtual member
virtual su2double	GetAveragePressure (unsigned short valMarker, unsigned short valSpan) const
	A virtual member.
virtual const su2double *	GetAverageTurboVelocity (unsigned short valMarker, unsigned short valSpan) const
	A virtual member.
virtual su2double	GetAverageNu (unsigned short valMarker, unsigned short valSpan) const
	A virtual member.
virtual su2double	GetAverageKine (unsigned short valMarker, unsigned short valSpan) const
	A virtual member.
virtual su2double	GetAverageOmega (unsigned short valMarker, unsigned short valSpan) const
	A virtual member.
virtual su2double	GetDensityIn (unsigned short inMarkerTP, unsigned short valSpan) const
	A virtual member.
virtual su2double	GetPressureIn (unsigned short inMarkerTP, unsigned short valSpan) const
	A virtual member.
virtual const su2double *	GetTurboVelocityIn (unsigned short inMarkerTP, unsigned short valSpan) const
	A virtual member.
virtual su2double	GetDensityOut (unsigned short inMarkerTP, unsigned short valSpan) const
	A virtual member.
virtual su2double	GetPressureOut (unsigned short inMarkerTP, unsigned short valSpan) const
	A virtual member.
virtual const su2double *	GetTurboVelocityOut (unsigned short inMarkerTP, unsigned short valSpan) const
	A virtual member.
virtual su2double	GetKineIn (unsigned short inMarkerTP, unsigned short valSpan) const
	A virtual member.
virtual su2double	GetOmegaIn (unsigned short inMarkerTP, unsigned short valSpan) const
	A virtual member.
virtual su2double	GetNuIn (unsigned short inMarkerTP, unsigned short valSpan) const
	A virtual member.
virtual su2double	GetKineOut (unsigned short inMarkerTP, unsigned short valSpan) const
	A virtual member.
virtual su2double	GetOmegaOut (unsigned short inMarkerTP, unsigned short valSpan) const
	A virtual member.
virtual su2double	GetNuOut (unsigned short inMarkerTP, unsigned short valSpan) const
	A virtual member.
virtual void	SetDensityIn (su2double value, unsigned short inMarkerTP, unsigned short valSpan)
	A virtual member.
virtual void	SetPressureIn (su2double value, unsigned short inMarkerTP, unsigned short valSpan)
	A virtual member.
virtual void	SetTurboVelocityIn (const su2double *value, unsigned short inMarkerTP, unsigned short valSpan)
	A virtual member.
virtual void	SetDensityOut (su2double value, unsigned short inMarkerTP, unsigned short valSpan)
	A virtual member.
virtual void	SetPressureOut (su2double value, unsigned short inMarkerTP, unsigned short valSpan)
	A virtual member.
virtual void	SetTurboVelocityOut (const su2double *value, unsigned short inMarkerTP, unsigned short valSpan)
	A virtual member.
virtual void	SetKineIn (su2double value, unsigned short inMarkerTP, unsigned short valSpan)
	A virtual member.
virtual void	SetOmegaIn (su2double value, unsigned short inMarkerTP, unsigned short valSpan)
	A virtual member.
virtual void	SetNuIn (su2double value, unsigned short inMarkerTP, unsigned short valSpan)
	A virtual member.
virtual void	SetKineOut (su2double value, unsigned short inMarkerTP, unsigned short valSpan)
	A virtual member.
virtual void	SetOmegaOut (su2double value, unsigned short inMarkerTP, unsigned short valSpan)
	A virtual member.
virtual void	SetNuOut (su2double value, unsigned short inMarkerTP, unsigned short valSpan)
	A virtual member.
virtual void	SetFreeStream_TurboSolution (CConfig *config)
	A virtual member.
virtual void	DeformMesh (CGeometry **geometry, CNumerics **numerics, CConfig *config)
	A virtual member.
virtual void	DeformMesh (CGeometry *geometry, CNumerics **numerics, CConfig *config)
	A virtual member.
virtual void	SetMesh_Stiffness (CNumerics **numerics, CConfig *config)
	A virtual member.
virtual void	ApplyGradientSmoothingVolume (CGeometry *geometry, CNumerics *numerics, const CConfig *config)
	A virtual member.
virtual void	ApplyGradientSmoothingSurface (CGeometry *geometry, CNumerics *numerics, const CConfig *config)
	A virtual member.
virtual void	ApplyGradientSmoothingDV (CGeometry *geometry, CNumerics *numerics, CSurfaceMovement *surface_movement, CVolumetricMovement *grid_movement, CConfig *config, su2double **Gradient)
	All steps required for smoothing the whole system on DV level in an iterative way.
virtual void	RecordTapeAndCalculateOriginalGradient (CGeometry *geometry, CSurfaceMovement *surface_movement, CVolumetricMovement *grid_movement, CConfig *config, su2double **Gradient)
	A virtual member.
virtual void	ReadSensFromGeometry (const CGeometry *geometry)
	A virtual member.
virtual void	WriteSensToGeometry (CGeometry *geometry) const
	A virtual member.
void	SetImplicitPeriodic (bool val_implicit_periodic)
	Routine that sets the flag controlling implicit treatment for periodic BCs.
void	SetRotatePeriodic (bool val_rotate_periodic)
	Routine that sets the flag controlling solution rotation for periodic BCs.
su2activematrix *	GetPeriodicProjections (const CGeometry &geometry, const CConfig &config)
	Storage for the limiters with rotational periodicity: the min and max, over the edges of the periodic matches of each point, of the reconstruction increments (communicated with PERIODIC_LIM_PRIM_1).
su2double *	GetPeriodicProjection (unsigned long iPoint)
	Reconstruction increment bounds for a periodic receive point, nullptr for other points.
const string &	GetSolverName () const
	Retrieve the solver name for output purposes.
vector< string >	GetSolutionFields () const
	Get the solution fields.
void	ComputeVertexTractions (CGeometry *geometry, const CConfig *config)
	Compute the tractions at the vertices.
su2double	GetVertexTractions (unsigned short iMarker, unsigned long iVertex, unsigned short iDim) const
	Set the adjoints of the vertex tractions.
void	RegisterVertexTractions (CGeometry *geometry, const CConfig *config)
	Register the vertex tractions as output.
void	StoreVertexTractionsAdjoint (unsigned short iMarker, unsigned long iVertex, unsigned short iDim, su2double val_adjoint)
	Store the adjoints of the vertex tractions.
void	SetVertexTractionsAdjoint (CGeometry *geometry, const CConfig *config)
	Set the adjoints of the vertex tractions to the AD structure.
virtual su2double	GetMinimum_Volume () const
	Get minimun volume in the mesh.
virtual su2double	GetMaximum_Volume () const
	Get maximum volume in the mesh.
virtual void	SetMomCoeff (CGeometry *geometry, CSolver **solver_container, CConfig *config, bool periodic, unsigned short iMesh)
	A virtual member.
virtual void	ComputeHbyA (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh)
	A virtual member.
void	SavelibROM (CGeometry *geometry, CConfig *config, bool converged)
	Save snapshot or POD data using libROM.
void	CustomSourceResidual (CGeometry *geometry, CSolver **solver_container, CNumerics **numerics_container, CConfig *config, unsigned short iMesh)

Static Public Member Functions
static void	ComputeConsistentExtrapolation (CFluidModel *fluidModel, unsigned short nDim, const su2double *scalar, su2double *primitive)
	Recompute the extrapolated quantities, after MUSCL reconstruction, in a more thermodynamically consistent way.
Static Public Member Functions inherited from CSolver
static void	MultigridRestriction (const CGeometry &geoFine, const su2activematrix &varsFine, const CGeometry &geoCoarse, su2activematrix &varsCoarse)
	Interpolate variables to a coarser grid level.

Protected Member Functions
void	CommonPreprocessing (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh, unsigned short iRKStep, unsigned short RunTime_EqSystem, bool Output)
	Preprocessing actions common to the Euler and NS solvers.
void	SetPreconditioner (const CConfig *config, unsigned long iPoint, su2double delta, su2activematrix &preconditioner) const
	Compute the preconditioner for low-Mach flows.
void	SetCentered_Dissipation_Sensor (CGeometry *geometry, const CConfig *config)
	Compute a pressure sensor switch.
void	SetMax_Eigenvalue (CGeometry *geometry, const CConfig *config)
	Compute the max eigenvalue.
virtual unsigned long	SetPrimitive_Variables (CSolver **solver_container, const CConfig *config)
	Compute the velocity^2, SoundSpeed, Pressure, Enthalpy, Viscosity.
void	RecomputeDensity_time_n (CSolver **solver_container, const CConfig *config)
	Recompute the dual-time density history (rho_n, rho_n-1) from the stored solution histories (Solution_time_n[,1], and the species histories for flamelet/variable-density) via the fluid model.
void	SetBeta_Parameter (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh)
	Update the Beta parameter for the incompressible preconditioner.
void	SetRangePressure (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh)
	Update the pressure range P_max - P_min for target mass flow rate.
void	GetOutlet_Properties (CGeometry *geometry, CConfig *config, unsigned short iMesh, bool Output)
	A virtual member.
void	SetNondimensionalization (CConfig *config, unsigned short iMesh)
	Set the solver nondimensionalization.
template<ENUM_TIME_INT IntegrationType>
void	Explicit_Iteration (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iRKStep)
	Generic implementation of explicit iterations with preconditioner.
void	SetReferenceValues (const CConfig &config) final
	Set reference values for pressure, forces, etc.
void	CorrectPressureGradient (su2double *corrected_grad_pressure, const su2double *avg_grad_pressure, const su2double val_pressure_i, const su2double val_pressure_j, const su2double *val_edge_vector, const su2double val_dist_ij_2)
	Apply a correction to the pressure or pressure deviation gradient to align with the edges.
Protected Member Functions inherited from CFVMFlowSolverBase< CIncEulerVariable, ENUM_REGIME::INCOMPRESSIBLE >
CVariable *	GetBaseClassPointerToNodes () final
	Return nodes to allow CSolver::base_nodes to be set.
	CFVMFlowSolverBase (const CGeometry &geometry, const CConfig &config)
	Protected constructor, this class is not directly instantiable.
void	Allocate (const CConfig &config)
	Allocate member variables.
void	AllocateTerribleLegacyTemporaryVariables ()
	Allocate small member variables that ideally should not be used.
void	CommunicateInitialState (CGeometry *geometry, const CConfig *config)
	Communicate the initial solver state.
void	HybridParallelInitialization (const CConfig &config, CGeometry &geometry)
	Initialize thread parallel variables.
void	PushSolutionBackInTime (unsigned long TimeIter, bool restart, bool rans, CSolver ***solver_container, CGeometry **geometry, CConfig *config)
	Move solution to previous time levels (for restarts).
su2double	EvaluateCommonObjFunc (const CConfig &config) const
	Evaluate common part of objective function to all solvers.
void	EdgeFluxResidual (const CGeometry *geometry, const CSolver *const *solvers, CConfig *config)
	Method to compute convective and viscous residual contribution using vectorized numerics.
void	SumEdgeFluxes (const CGeometry *geometry)
	Sum the edge fluxes for each cell to populate the residual vector, only used on coarse grids.
void	FinalizeResidualComputation (const CGeometry *geometry, bool pausePreacc, unsigned long localCounter, CConfig *config)
	Sums edge fluxes (if required) and computes the global error counter.
void	ComputeAxisymmetricAuxGradients (CGeometry *geometry, const CConfig *config)
	Computes and sets the required auxilliary vars (and gradients) for axisymmetric flow.
virtual void	InstantiateEdgeNumerics (const CSolver *const *solvers, const CConfig *config)
	Instantiate a SIMD numerics object.
virtual CNumerics::ResidualType	Viscous_Residual (unsigned long iEdge, CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config)
	Compute the viscous contribution for a particular edge.
virtual void	Viscous_Residual (CGeometry *geometry, CSolver **solver_container, CNumerics **numerics_container, CConfig *config, unsigned short iMesh, unsigned short iRKStep)
	A virtual member.
CNumerics::ResidualType	Viscous_Residual_impl (unsigned long iEdge, CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config)
void	UpdateJacobian (unsigned long iEdge, unsigned long iPoint, unsigned long jPoint, const CNumerics::ResidualType<> &conv, const CNumerics::ResidualType<> &visc)
	Update the Jacobian for one edge with the fused convective and viscous contributions.
virtual void	ComputeUnderRelaxationFactor (const CConfig *config)
	Compute a suitable under-relaxation parameter to limit the change in the solution variables over a nonlinear iteration for stability.
void	LoadRestart_impl (CGeometry **geometry, CSolver ***solver, CConfig *config, int iter, bool update_geo, su2double *RestartSolution=nullptr, unsigned short nVar_Restart=0)
	General implementation to load a flow solution from a restart file.
void	SetTime_Step_impl (const SoundSpeedFunc &soundSpeed, const LambdaViscFunc &lambdaVisc, CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh, unsigned long Iteration)
	Generic implementation to compute the time step based on CFL and conv/visc eigenvalues.
void	SetMax_Eigenvalue_impl (const SoundSpeedFunc &soundSpeed, CGeometry *geometry, const CConfig *config)
	Compute the max eigenvalue, gemeric implementation.
void	SetCentered_Dissipation_Sensor_impl (const SensVarFunc &sensVar, CGeometry *geometry, const CConfig *config)
	Compute the dissipation sensor for centered schemes.
void	Explicit_Iteration_impl (ResidualPrecond &preconditioner, CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iRKStep)
	Generic implementation of explicit iterations with a preconditioner.
void	Explicit_Iteration (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iRKStep)
	Generic implementation of explicit iterations without preconditioner.
void	PrepareImplicitIteration_impl (DiagonalPrecond &preconditioner, CGeometry *geometry, CConfig *config)
	Generic implementation to prepare an implicit iteration with an optional preconditioner applied to the diagonal.
void	ComputeVorticityAndStrainMag (const CConfig &config, const CGeometry *geometry, unsigned short iMesh)
	Evaluate the vorticity and strain rate magnitude.
	~CFVMFlowSolverBase ()
	Destructor.
Protected Member Functions inherited from CSolver
void	SetBaseClassPointerToNodes ()
	Call this method to set "base_nodes" after the "nodes" variable of the derived solver is instantiated.
void	SetUndivided_Laplacian (CGeometry *geometry, const CConfig *config)
	Compute the undivided laplacian for the solution variables.
void	SetVerificationSolution (unsigned short nDim, unsigned short nVar, CConfig *config)
	Allocate the memory for the verification solution, if necessary.
void	ResidualReductions_FromAllThreads (const CGeometry *geometry, const CConfig *config, const su2double *resRMS, const su2double *resMax, const unsigned long *idxMax)
	"Add" local residual variables of all threads to compute global residual variables.
void	SetResToZero ()
	Set the RMS and MAX residual to zero.
void	AddRes_Max (unsigned short val_var, su2double val_residual, unsigned long val_point, const su2double *val_coord)
	Adds the maximal residual, this is useful for the convergence history.
void	AddRes_Max_BGS (unsigned short val_var, su2double val_residual, unsigned long val_point, const su2double *val_coord)
	Adds the maximal residual for BGS subiterations.

Protected Attributes
vector< CFluidModel * >	FluidModel
	fluid model used in the solver.
StreamwisePeriodicValues	SPvals
StreamwisePeriodicValues	SPvalsUpdated
bool	pressure_based
su2activevector	alpha_p
su2activevector	pressureCorrection
su2activematrix	momentumCorrection
su2activevector	EdgeMassFluxCorrection
Protected Attributes inherited from CFVMFlowSolverBase< CIncEulerVariable, ENUM_REGIME::INCOMPRESSIBLE >
const VariableType::template CIndices< unsigned short >	prim_idx
	Object with indices of primitive variables.
unsigned long	omp_chunk_size
	Chunk size used in light point loops.
su2activevector	EdgeMassFluxes
	Mass fluxes across each edge, for discretization of transported scalars.
su2double	Mach_Inf
	Mach number at the infinity.
su2double	Density_Inf
	Density at the infinity.
su2double	Energy_Inf
	Energy at the infinity.
su2double	Temperature_Inf
	Temperature at the infinity.
su2double	Enthalpy_Inf
	Enthalpy at the infinity.
su2double	Pressure_Inf
	Pressure at the infinity.
su2double *	Velocity_Inf
	Flow Velocity vector at the infinity.
su2double	Viscosity_Inf
	Viscosity at the infinity.
su2double	Tke_Inf
	Turbulent kinetic energy at the infinity.
su2double	StrainMag_Max
	Maximum Strain Rate magnitude.
su2double	Omega_Max
	Maximum Omega.
su2double	Global_Delta_Time
	Time-step for TIME_STEPPING time marching strategy.
su2double	Global_Delta_UnstTimeND
	Unsteady time step for the dual time strategy.
unsigned long	ErrorCounter
	Counter for number of un-physical states.
AeroCoeffsArray	InvCoeff
	Inviscid pressure contributions for each boundary.
AeroCoeffsArray	SurfaceInvCoeff
	Inviscid pressure contributions for each monitoring boundary.
AeroCoeffs	AllBoundInvCoeff
	Total pressure contribution for all the boundaries.
AeroCoeffsArray	MntCoeff
	Inviscid momentum contributions for each boundary.
AeroCoeffsArray	SurfaceMntCoeff
	Inviscid momentum contributions for each monitoring boundary.
AeroCoeffs	AllBoundMntCoeff
	Total momentum contribution for all the boundaries.
AeroCoeffsArray	ViscCoeff
	Viscous contributions for each boundary.
AeroCoeffsArray	SurfaceViscCoeff
	Viscous contributions for each monitoring boundary.
AeroCoeffs	AllBoundViscCoeff
	Total pressure contribution for all the boundaries.
AeroCoeffsArray	SurfaceCoeff
	Totals for each monitoring surface.
AeroCoeffs	TotalCoeff
	Totals for all boundaries.
su2double	AeroCoeffForceRef
	Reference force for aerodynamic coefficients.
su2double	DynamicPressureRef
	Reference dynamic pressure.
su2double	Total_CpDiff
	Total Equivalent Area coefficient for all the boundaries.
su2double	Total_HeatFluxDiff
	Total Equivalent Area coefficient for all the boundaries.
su2double	Total_CEquivArea
	Total Equivalent Area coefficient for all the boundaries.
su2double	Total_MassFlowRate
	Total Mass Flow Rate on monitored boundaries.
su2double	Total_CNearFieldOF
	Total Near-Field Pressure coefficient for all the boundaries.
su2double	Total_Heat
	Total heat load for all the boundaries.
su2double	Total_MaxHeat
	Maximum heat flux on all boundaries.
su2double	AllBound_CNearFieldOF_Inv
	Near-Field press coeff (inviscid) for all the boundaries.
vector< su2double >	CNearFieldOF_Inv
	Near field pressure (inviscid) for each boundary.
vector< su2double >	Surface_HF_Visc
	Total (integrated) heat flux for each monitored surface.
vector< su2double >	Surface_MaxHF_Visc
	Maximum heat flux for each monitored surface.
vector< su2double >	HF_Visc
	Heat load (viscous contribution) for each boundary.
vector< su2double >	MaxHF_Visc
	Maximum heat flux (viscous contribution) for each boundary.
su2double	AllBound_HF_Visc
	Heat load (viscous contribution) for all the boundaries.
su2double	AllBound_MaxHF_Visc
	Maximum heat flux (viscous contribution) for all boundaries.
vector< vector< su2double > >	Inlet_Ptotal
	Value of the Total P.
vector< vector< su2double > >	Inlet_Ttotal
	Value of the Total T.
vector< su2activematrix >	Inlet_FlowDir
	Value of the Flow Direction.
vector< vector< su2double > >	HeatFlux
	Heat transfer coefficient for each boundary and vertex.
vector< vector< su2double > >	HeatFluxTarget
	Heat transfer coefficient for each boundary and vertex.
vector< su2activematrix >	CharacPrimVar
	Value of the characteristic variables at each boundary.
vector< su2activematrix >	CSkinFriction
	Skin friction coefficient for each boundary and vertex.
vector< vector< su2double > >	WallShearStress
	Wall Shear Stress for each boundary and vertex.
vector< su2activematrix >	HeatConjugateVar
	CHT variables for each boundary and vertex.
vector< vector< su2double > >	CPressure
	Pressure coefficient for each boundary and vertex.
vector< vector< su2double > >	CPressureTarget
	Target Pressure coefficient for each boundary and vertex.
vector< vector< su2double > >	YPlus
	Yplus for each boundary and vertex.
vector< vector< su2double > >	UTau
	UTau for each boundary and vertex.
vector< vector< su2double > >	EddyViscWall
	Eddy viscosuty at the wall for each boundary and vertex.
bool	space_centered
	True if space centered scheme used.
bool	euler_implicit
	True if euler implicit scheme used.
bool	least_squares
	True if computing gradients by least squares.
su2double	Gamma
	Fluid's Gamma constant (ratio of specific heats).
su2double	Gamma_Minus_One
	Fluids's Gamma - 1.0 .
vector< su2matrix< su2double * > >	SlidingState
vector< vector< int > >	SlidingStateNodes
array< DummyGridColor<>, 1 >	EdgeColoring
CSysVector< su2double >	EdgeFluxes
	Flux across each edge.
CNumericsSIMD *	edgeNumerics
	Object for edge flux computation.
CIncEulerVariable *	nodes
	The highest level in the variable hierarchy the DERIVED solver can safely use.
Protected Attributes inherited from CSolver
int	rank
	MPI Rank.
int	size
	MPI Size.
bool	adjoint
	Boolean to determine whether solver is initialized as a direct or an adjoint solver.
unsigned short	MGLevel
	Multigrid level of this solver object.
unsigned short	IterLinSolver
	Linear solver iterations.
su2double	ResLinSolver
	Final linear solver residual.
unsigned short	NonLinRes_Counter
	Number of elements of the nonlinear residual indicator series.
vector< su2double >	NonLinRes_Series
	Vector holding the nonlinear residual indicator series.
su2double	Old_Func
	Old value of the nonlinear residual indicator.
su2double	New_Func
	Current value of the nonlinear residual indicator.
unsigned short	nVar
	Number of variables of the problem.
unsigned short	nPrimVar
	Number of primitive variables of the problem.
unsigned short	nPrimVarGrad
	Number of primitive variables of the problem in the gradient computation.
unsigned short	nSecondaryVar
	Number of primitive variables of the problem.
unsigned short	nVarGrad
	Number of variables for deallocating the LS Cvector.
unsigned short	nDim
	Number of dimensions of the problem.
unsigned long	nPoint
	Number of points of the computational grid.
unsigned long	nPointDomain
	Number of points of the computational grid.
su2double	Max_Delta_Time
	Maximum value of the delta time for all the control volumes.
su2double	Min_Delta_Time
	Minimum value of the delta time for all the control volumes.
su2double	Max_CFL_Local
	Maximum value of the CFL across all the control volumes.
su2double	Min_CFL_Local
	Minimum value of the CFL across all the control volumes.
su2double	Avg_CFL_Local
	Average value of the CFL across all the control volumes.
vector< su2double >	Residual_RMS
	Vector with the mean residual for each variable.
vector< su2double >	Residual_Max
	Vector with the maximal residual for each variable.
vector< su2double >	Residual_BGS
	Vector with the mean residual for each variable for BGS subiterations.
vector< su2double >	Residual_Max_BGS
	Vector with the maximal residual for each variable for BGS subiterations.
vector< unsigned long >	Point_Max
	Vector with the maximal residual for each variable.
vector< unsigned long >	Point_Max_BGS
	Vector with the maximal residual for each variable.
su2activematrix	Point_Max_Coord
	Vector with pointers to the coords of the maximal residual for each variable.
su2activematrix	Point_Max_Coord_BGS
	Vector with pointers to the coords of the maximal residual for each variable.
su2double	Total_Custom_ObjFunc = 0.0
	Total custom objective function.
su2double	Total_ComboObj = 0.0
	Total 'combo' objective for all monitored boundaries.
su2double *	Residual
	Auxiliary nVar vector.
su2double *	Residual_i
	Auxiliary nVar vector for storing the residual at point i.
su2double *	Residual_j
	Auxiliary nVar vector for storing the residual at point j.
su2double *	Solution
	Auxiliary nVar vector.
su2double *	Solution_i
	Auxiliary nVar vector for storing the solution at point i.
su2double *	Solution_j
	Auxiliary nVar vector for storing the solution at point j.
su2double *	Vector
	Auxiliary nDim vector.
su2double *	Vector_i
	Auxiliary nDim vector to do the reconstruction of the variables at point i.
su2double *	Vector_j
	Auxiliary nDim vector to do the reconstruction of the variables at point j.
su2double *	Res_Conv
	Auxiliary nVar vector for storing the convective residual.
su2double *	Res_Visc
	Auxiliary nVar vector for storing the viscous residual.
su2double *	Res_Sour
	Auxiliary nVar vector for storing the viscous residual.
su2double *	Res_Conv_i
	Auxiliary vector for storing the convective residual at point i.
su2double *	Res_Visc_i
	Auxiliary vector for storing the viscous residual at point i.
su2double *	Res_Conv_j
	Auxiliary vector for storing the convective residual at point j.
su2double *	Res_Visc_j
	Auxiliary vector for storing the viscous residual at point j.
su2double **	Jacobian_i
	Auxiliary matrices for storing point to point Jacobians at point i.
su2double **	Jacobian_j
	Auxiliary matrices for storing point to point Jacobians at point j.
su2double **	Jacobian_ii
	Auxiliary matrices for storing point to point Jacobians.
su2double **	Jacobian_ij
	Auxiliary matrices for storing point to point Jacobians.
su2double **	Jacobian_ji
	Auxiliary matrices for storing point to point Jacobians.
su2double **	Jacobian_jj
	Auxiliary matrices for storing point to point Jacobians.
su2activevector	iPoint_UndLapl
	Auxiliary variable for the undivided Laplacians.
su2activevector	jPoint_UndLapl
	Auxiliary variable for the undivided Laplacians.
vector< int >	Restart_Vars
	Auxiliary structure for holding the number of variables and points in a restart.
int	Restart_ExtIter
	Auxiliary structure for holding the external iteration offset from a restart.
vector< passivedouble >	Restart_Data
	Auxiliary structure for holding the data values from a restart.
unsigned short	nOutputVariables
	Number of variables to write.
unsigned long	nMarker
	Total number of markers using the grid information.
vector< unsigned long >	nVertex
	Store nVertex at each marker for deallocation.
bool	rotate_periodic
	Flag that controls whether the periodic solution needs to be rotated for the solver.
bool	implicit_periodic
	Flag that controls whether the implicit system should be treated by the periodic BC comms.
su2activematrix	PeriodicProj
	Min/max reconstruction increments at periodic receive points (for limiters).
std::unordered_map< unsigned long, size_t >	PeriodicProjIndex
	Local point to compact projection row.
bool	dynamic_grid
	Flag that determines whether the grid is dynamic (moving or deforming + grid velocities).
vector< su2activematrix >	VertexTraction
vector< su2activematrix >	VertexTractionAdjoint
std::shared_ptr< CTurboOutput >	TurbomachineryPerformance
	turbo performance calculator.
string	SolverName
	Store the name of the solver for output purposes.

Additional Inherited Members
Public Attributes inherited from CSolver
CSysVector< su2double >	LinSysSol
	vector to store iterative solution of implicit linear system.
CSysVector< su2double >	LinSysRes
	vector to store iterative residual of implicit linear system.
CSysMatrix< su2mixedfloat >	Jacobian
	Complete sparse Jacobian structure for implicit computations.
CSysSolve< su2mixedfloat >	System
	Linear solver/smoother.
CSysVector< su2double >	OutputVariables
	vector to store the extra variables to be written.
string *	OutputHeadingNames
	vector of strings to store the headings for the exra variables
CVerificationSolution *	VerificationSolution
	Verification solution class used within the solver.
vector< string >	fields
Protected Types inherited from CSolver
enum	: size_t { OMP_MIN_SIZE = 32 }
Static Protected Member Functions inherited from CFVMFlowSolverBase< CIncEulerVariable, ENUM_REGIME::INCOMPRESSIBLE >
static void	ompMasterAssignBarrier (Ts &&... lhsRhsPairs)
	Utility to set the value of a member variables safely, and so that the new values are seen by all threads.
Static Protected Member Functions inherited from CSolver
static void	ResidualReductions_PerThread (unsigned long iPoint, unsigned short iVar, su2double res, su2double *resRMS, su2double *resMax, unsigned long *idxMax)
	"Add" residual at (iPoint,iVar) to residual variables local to the thread.
Static Protected Attributes inherited from CFVMFlowSolverBase< CIncEulerVariable, ENUM_REGIME::INCOMPRESSIBLE >
static constexpr size_t	MAXNDIM
	Max number of space dimensions, used in some static arrays.
static constexpr size_t	MAXNVAR
	Max number of variables, for static arrays.
static constexpr size_t	OMP_MAX_SIZE
	Max chunk size for light point loops.
static constexpr size_t	OMP_MIN_SIZE
	Min chunk size for edge loops (max is color group size).
static constexpr bool	ReducerStrategy

Detailed Description

Main class for defining the incompressible Euler flow solver.

Author

F. Palacios, T. Economon, T. Albring

Constructor & Destructor Documentation

CIncEulerSolver() [1/2]

CIncEulerSolver::CIncEulerSolver ( )

delete

CIncEulerSolver() [2/2]

CIncEulerSolver::CIncEulerSolver	(	CGeometry *	geometry,
		CConfig *	config,
		unsigned short	iMesh,
		const bool	navier_stokes = false
	)

Constructor of the class.

Parameters

[in]	geometry	- Geometrical definition of the problem.
[in]	config	- Definition of the particular problem.
[in]	iMesh	- Grid level.
[in]	navier_stokes	- True when the constructor is called by the derived class CIncNSSolver.

~CIncEulerSolver()

CIncEulerSolver::~CIncEulerSolver ( void  )

override

Destructor of the class.

Member Function Documentation

ApplyPressureVelocityCorrection()

void CIncEulerSolver::ApplyPressureVelocityCorrection ( CGeometry *  geometry, CSolver **  solver_container, CConfig *  config  )

finalvirtual

Compute the spatial integration using a centered scheme.

Parameters

[in]	geometry	- Geometrical definition of the problem.
[in]	solver_container	- Container vector with all the solutions.
[in]	config	- Definition of the particular problem.

Reimplemented from CSolver.

BC_Far_Field()

void CIncEulerSolver::BC_Far_Field ( CGeometry *  geometry, CSolver **  solver_container, CNumerics *  conv_numerics, CNumerics *  visc_numerics, CConfig *  config, unsigned short  val_marker  )

finalvirtual

Impose the far-field boundary condition using characteristics.

Parameters

[in]	geometry	- Geometrical definition of the problem.
[in]	solver_container	- Container vector with all the solutions.
[in]	conv_numerics	- Description of the numerical method.
[in]	visc_numerics	- Description of the numerical method.
[in]	config	- Definition of the particular problem.
[in]	val_marker	- Surface marker where the boundary condition is applied.

Reimplemented from CSolver.

BC_Inlet()

void CIncEulerSolver::BC_Inlet ( CGeometry *  geometry, CSolver **  solver_container, CNumerics *  conv_numerics, CNumerics *  visc_numerics, CConfig *  config, unsigned short  val_marker  )

finalvirtual

Impose a subsonic inlet boundary condition.

Parameters

[in]	geometry	- Geometrical definition of the problem.
[in]	solver_container	- Container vector with all the solutions.
[in]	conv_numerics	- Description of the numerical method.
[in]	visc_numerics	- Description of the numerical method.
[in]	config	- Definition of the particular problem.
[in]	val_marker	- Surface marker where the boundary condition is applied.

Reimplemented from CSolver.

BC_Outlet()

void CIncEulerSolver::BC_Outlet ( CGeometry *  geometry, CSolver **  solver_container, CNumerics *  conv_numerics, CNumerics *  visc_numerics, CConfig *  config, unsigned short  val_marker  )

finalvirtual

Impose the outlet boundary condition.

Parameters

[in]	geometry	- Geometrical definition of the problem.
[in]	solver_container	- Container vector with all the solutions.
[in]	conv_numerics	- Description of the numerical method.
[in]	visc_numerics	- Description of the numerical method.
[in]	config	- Definition of the particular problem.
[in]	val_marker	- Surface marker where the boundary condition is applied.

Reimplemented from CSolver.

Centered_Residual()

void CIncEulerSolver::Centered_Residual ( CGeometry *  geometry, CSolver **  solver_container, CNumerics **  numerics_container, CConfig *  config, unsigned short  iMesh, unsigned short  iRKStep  )

finalvirtual

Compute the spatial integration using a centered scheme.

Parameters

[in]	geometry	- Geometrical definition of the problem.
[in]	solver_container	- Container vector with all the solutions.
[in]	numerics_container	- Description of the numerical method.
[in]	config	- Definition of the particular problem.
[in]	iMesh	- Index of the mesh in multigrid computations.
[in]	iRKStep	- Current step of the Runge-Kutta iteration.

Reimplemented from CSolver.

ClassicalRK4_Iteration()

void CIncEulerSolver::ClassicalRK4_Iteration ( CGeometry *  geometry, CSolver **  solver_container, CConfig *  config, unsigned short  iRKStep  )

finalvirtual

Update the solution using the classical Runge-Kutta 4 scheme.

Parameters

[in]	geometry	- Geometrical definition of the problem.
[in]	solver_container	- Container vector with all the solutions.
[in]	config	- Definition of the particular problem.
[in]	iRKStep	- Current step of the Runge-Kutta iteration.

Reimplemented from CSolver.

CommonPreprocessing()

void CIncEulerSolver::CommonPreprocessing ( CGeometry *  geometry, CSolver **  solver_container, CConfig *  config, unsigned short  iMesh, unsigned short  iRKStep, unsigned short  RunTime_EqSystem, bool  Output  )

protected

Preprocessing actions common to the Euler and NS solvers.

Parameters

[in]	geometry	- Geometrical definition of the problem.
[in]	solver_container	- Container vector with all the solutions.
[in]	config	- Definition of the particular problem.
[in]	iRKStep	- Current step of the Runge-Kutta iteration.
[in]	RunTime_EqSystem	- System of equations which is going to be solved.
[in]	Output	- boolean to determine whether to print output.

ComputeConsistentExtrapolation()

void CIncEulerSolver::ComputeConsistentExtrapolation ( CFluidModel *  fluidModel, unsigned short  nDim, const su2double *  scalar, su2double *  primitive  )

static

Recompute the extrapolated quantities, after MUSCL reconstruction, in a more thermodynamically consistent way.

Note

This method is static to improve the chances of it being used in a thread-safe manner.

Parameters

[in,out]	fluidModel	- The fluid model.
[in]	nDim	- Number of physical dimensions.
[in]	scalar	- scalar variable.
[in,out]	primitive	- Primitive variables.

ComputeEdgeMassFluxesRhieChow()

void CIncEulerSolver::ComputeEdgeMassFluxesRhieChow ( CGeometry *  geometry, CSolver **  solver_container, CConfig *  config  )

finalvirtual

Compute the spatial integration using a centered scheme.

Parameters

[in]	geometry	- Geometrical definition of the problem.
[in]	solver_container	- Container vector with all the solutions.

Reimplemented from CSolver.

CorrectPressureGradient()

void CIncEulerSolver::CorrectPressureGradient ( su2double *  corrected_grad_pressure, const su2double *  avg_grad_pressure, const su2double  val_pressure_i, const su2double  val_pressure_j, const su2double *  val_edge_vector, const su2double  val_dist_ij_2  )

protected

Apply a correction to the pressure or pressure deviation gradient to align with the edges.

Parameters

[in]	corrected_grad_pressure	- The corrected gradient at the edge
[in]	avg_grad_pressure	- The average gradient at the edge
[in]	val_pressure_i	- variable at point i
[in]	val_pressure_j	- variable at point j
[in]	val_edge_vector	- The vector between points i and j
[in]	val_dist_ij_2	- The distance between points i and j, squared

Evaluate_ObjFunc()

void CIncEulerSolver::Evaluate_ObjFunc ( const CConfig *  config, CSolver **  solver  )

inlinefinalvirtual

Compute weighted-sum "combo" objective output.

Author

H. Kline

Parameters

[in]	config	- Definition of the particular problem.
[in]	solver	- Container vector with all the solutions.

Reimplemented from CSolver.

Explicit_Iteration()

template<ENUM_TIME_INT IntegrationType>

void CIncEulerSolver::Explicit_Iteration ( CGeometry *  geometry, CSolver **  solver_container, CConfig *  config, unsigned short  iRKStep  )

inlineprotected

Generic implementation of explicit iterations with preconditioner.

ExplicitEuler_Iteration()

void CIncEulerSolver::ExplicitEuler_Iteration ( CGeometry *  geometry, CSolver **  solver_container, CConfig *  config  )

finalvirtual

Update the solution using the explicit Euler scheme.

Parameters

[in]	geometry	- Geometrical definition of the problem.
[in]	solver_container	- Container vector with all the solutions.
[in]	config	- Definition of the particular problem.

Reimplemented from CSolver.

ExplicitRK_Iteration()

void CIncEulerSolver::ExplicitRK_Iteration ( CGeometry *  geometry, CSolver **  solver_container, CConfig *  config, unsigned short  iRKStep  )

finalvirtual

Update the solution using a Runge-Kutta scheme.

Parameters

[in]	geometry	- Geometrical definition of the problem.
[in]	solver_container	- Container vector with all the solutions.
[in]	config	- Definition of the particular problem.
[in]	iRKStep	- Current step of the Runge-Kutta iteration.

Reimplemented from CSolver.

ExtractAdjoint_SolutionExtra()

void CIncEulerSolver::ExtractAdjoint_SolutionExtra ( su2activevector &  adj_sol, const CConfig *  config  )

finalvirtual

Extract the adjoint of the extra solution at the input.

Parameters

[out]	adj_sol	- Vector to store the adjoint into.
[in]	config	- The particular config.

Reimplemented from CSolver.

GetFluidModel()

CFluidModel * CIncEulerSolver::GetFluidModel ( void  ) const

inlinefinalvirtual

Compute the pressure at the infinity.

Returns

Value of the pressure at the infinity.

Reimplemented from CSolver.

GetHasHybridParallel()

bool CIncEulerSolver::GetHasHybridParallel ( ) const

inlinefinalvirtual

The incompressible Euler and NS solvers support MPI+OpenMP.

Reimplemented from CSolver.

GetOutlet_Properties()

void CIncEulerSolver::GetOutlet_Properties ( CGeometry *  geometry, CConfig *  config, unsigned short  iMesh, bool  Output  )

protected

A virtual member.

GetStreamwisePeriodicValues()

StreamwisePeriodicValues CIncEulerSolver::GetStreamwisePeriodicValues ( ) const

inlinefinalvirtual

Get values for streamwise periodic flow: delta P, m_dot, inlet T, integrated heat, etc.

Returns

Struct holding streamwise periodic values.

Reimplemented from CSolver.

LoadRestart()

void CIncEulerSolver::LoadRestart ( CGeometry **  geometry, CSolver ***  solver, CConfig *  config, int  val_iter, bool  val_update_geo  )

finalvirtual

Load a solution from a restart file.

Parameters

[in]	geometry	- Geometrical definition of the problem.
[in]	solver	- Container vector with all of the solvers.
[in]	config	- Definition of the particular problem.
[in]	val_iter	- Current external iteration number.
[in]	val_update_geo	- Flag for updating coords and grid velocity.

Reimplemented from CFVMFlowSolverBase< CIncEulerVariable, ENUM_REGIME::INCOMPRESSIBLE >.

PrepareImplicitIteration()

void CIncEulerSolver::PrepareImplicitIteration ( CGeometry *  geometry, CSolver **  , CConfig *  config  )

finalvirtual

Prepare an implicit iteration.

Parameters

[in]	geometry	- Geometrical definition of the problem.
[in]	config	- Definition of the particular problem.

Reimplemented from CSolver.

Preprocessing()

void CIncEulerSolver::Preprocessing ( CGeometry *  geometry, CSolver **  solver_container, CConfig *  config, unsigned short  iMesh, unsigned short  iRKStep, unsigned short  RunTime_EqSystem, bool  Output  )

overridevirtual

Compute primitive variables and their gradients.

Parameters

[in]	geometry	- Geometrical definition of the problem.
[in]	solver_container	- Container vector with all the solutions.
[in]	config	- Definition of the particular problem.
[in]	iRKStep	- Current step of the Runge-Kutta iteration.
[in]	RunTime_EqSystem	- System of equations which is going to be solved.
[in]	Output	- boolean to determine whether to print output.

Reimplemented from CSolver.

Reimplemented in CIncNSSolver.

PrintVerificationError()

void CIncEulerSolver::PrintVerificationError ( const CConfig *  config ) const

finalvirtual

Print verification error to screen.

Parameters

[in]

config

- Definition of the particular problem.

Implements CFVMFlowSolverBase< CIncEulerVariable, ENUM_REGIME::INCOMPRESSIBLE >.

RecomputeDensity_time_n()

void CIncEulerSolver::RecomputeDensity_time_n ( CSolver **  solver_container, const CConfig *  config  )

protected

Recompute the dual-time density history (rho_n, rho_n-1) from the stored solution histories (Solution_time_n[,1], and the species histories for flamelet/variable-density) via the fluid model.

Called once per physical time step (InnerIter == 0), after the solution push-back. This keeps the density history consistent with the primitive state at time n (also after restart).

Parameters

[in]	solver_container	- Container vector with all the solutions.
[in]	config	- Definition of the particular problem.

RegisterSolutionExtra()

unsigned long CIncEulerSolver::RegisterSolutionExtra ( bool  input, const CConfig *  config  )

finalvirtual

Register In- or Output.

Parameters

[in]	input	- Boolean whether In- or Output should be registered.
[in]	config	- The particular config.

Returns

The number of extra variables.

Reimplemented from CSolver.

SetAdjoint_SolutionExtra()

void CIncEulerSolver::SetAdjoint_SolutionExtra ( const su2activevector &  adj_sol, const CConfig *  config  )

finalvirtual

Seed the adjoint of the extra solution at the output.

Parameters

[in]	adj_sol	- Vector containing the adjoint solution to seed.
[in]	config	- The particular config.

Reimplemented from CSolver.

SetBeta_Parameter()

void CIncEulerSolver::SetBeta_Parameter ( CGeometry *  geometry, CSolver **  solver_container, CConfig *  config, unsigned short  iMesh  )

protected

Update the Beta parameter for the incompressible preconditioner.

Parameters

[in]	geometry	- Geometrical definition of the problem.
[in]	solver_container	- Container vector with all the solutions.
[in]	config	- Definition of the particular problem.
[in]	iMesh	- current mesh level for the multigrid.

SetCentered_Dissipation_Sensor()

void CIncEulerSolver::SetCentered_Dissipation_Sensor ( CGeometry *  geometry, const CConfig *  config  )

protected

Compute a pressure sensor switch.

Parameters

[in]	geometry	- Geometrical definition of the problem.
[in]	solver_container	- Container vector with all the solutions.
[in]	config	- Definition of the particular problem.

SetFreeStream_Solution()

void CIncEulerSolver::SetFreeStream_Solution ( const CConfig *  config )

finalvirtual

Set the solution using the Freestream values.

Parameters

[in]

config

- Definition of the particular problem.

Reimplemented from CSolver.

SetMax_Eigenvalue()

void CIncEulerSolver::SetMax_Eigenvalue ( CGeometry *  geometry, const CConfig *  config  )

protected

Compute the max eigenvalue.

Parameters

[in]	geometry	- Geometrical definition of the problem.
[in]	config	- Definition of the particular problem.

SetNondimensionalization()

void CIncEulerSolver::SetNondimensionalization ( CConfig *  config, unsigned short  iMesh  )

protected

Set the solver nondimensionalization.

Parameters

[in]	config	- Definition of the particular problem.
[in]	iMesh	- Index of the mesh in multigrid computations.

SetPreconditioner()

void CIncEulerSolver::SetPreconditioner ( const CConfig *  config, unsigned long  iPoint, su2double  delta, su2activematrix &  preconditioner  ) const

protected

Compute the preconditioner for low-Mach flows.

Parameters

[in]	iPoint	- Index of the grid point
[in]	config	- Definition of the particular problem.
[in]	delta	- Volume over delta time, does not matter for explicit.
[out]	preconditioner	- The preconditioner matrix.

SetPrimitive_Variables()

unsigned long CIncEulerSolver::SetPrimitive_Variables ( CSolver **  solver_container, const CConfig *  config  )

protectedvirtual

Compute the velocity^2, SoundSpeed, Pressure, Enthalpy, Viscosity.

Parameters

[in]	solver_container	- Container vector with all the solutions.
[in]	config	- Definition of the particular problem.

Returns

- The number of non-physical points.

SetRangePressure()

void CIncEulerSolver::SetRangePressure ( CGeometry *  geometry, CSolver **  solver_container, CConfig *  config, unsigned short  iMesh  )

protected

Update the pressure range P_max - P_min for target mass flow rate.

Parameters

[in]	geometry	- Geometrical definition of the problem.
[in]	solver_container	- Container vector with all the solutions.
[in]	config	- Definition of the particular problem.
[in]	iMesh	- current mesh level for the multigrid.

SetReferenceValues()

void CIncEulerSolver::SetReferenceValues ( const CConfig &  config )

finalprotectedvirtual

Set reference values for pressure, forces, etc.

Implements CFVMFlowSolverBase< CIncEulerVariable, ENUM_REGIME::INCOMPRESSIBLE >.

SetResidual_DualTime()

void CIncEulerSolver::SetResidual_DualTime ( CGeometry *  geometry, CSolver **  solver_container, CConfig *  config, unsigned short  iRKStep, unsigned short  iMesh, unsigned short  RunTime_EqSystem  )

finalvirtual

Set the total residual adding the term that comes from the Dual Time Strategy.

Parameters

[in]	geometry	- Geometrical definition of the problem.
[in]	solver_container	- Container vector with all the solutions.
[in]	config	- Definition of the particular problem.
[in]	iRKStep	- Current step of the Runge-Kutta iteration.
[in]	iMesh	- Index of the mesh in multigrid computations.
[in]	RunTime_EqSystem	- System of equations which is going to be solved.

Reimplemented from CFVMFlowSolverBase< CIncEulerVariable, ENUM_REGIME::INCOMPRESSIBLE >.

SetTime_Step()

void CIncEulerSolver::SetTime_Step ( CGeometry *  geometry, CSolver **  solver_container, CConfig *  config, unsigned short  iMesh, unsigned long  Iteration  )

finalvirtual

Compute the time step for solving the Euler equations.

Parameters

[in]	geometry	- Geometrical definition of the problem.
[in]	solver_container	- Container vector with all the solutions.
[in]	config	- Definition of the particular problem.
[in]	iMesh	- Index of the mesh in multigrid computations.
[in]	Iteration	- Value of the current iteration.

Reimplemented from CSolver.

Source_Residual()

void CIncEulerSolver::Source_Residual ( CGeometry *  geometry, CSolver **  solver_container, CNumerics **  numerics_container, CConfig *  config, unsigned short  iMesh  )

finalvirtual

Source term integration.

Parameters

[in]	geometry	- Geometrical definition of the problem.
[in]	solver_container	- Container vector with all the solutions.
[in]	numerics_container	- Description of the numerical method.
[in]	config	- Definition of the particular problem.
[in]	iMesh	- Index of the mesh in multigrid computations.

Reimplemented from CSolver.

Source_Template()

void CIncEulerSolver::Source_Template ( CGeometry *  geometry, CSolver **  solver_container, CNumerics *  numerics, CConfig *  config, unsigned short  iMesh  )

finalvirtual

Source term integration.

Parameters

[in]	geometry	- Geometrical definition of the problem.
[in]	solver_container	- Container vector with all the solutions.
[in]	numerics	- Description of the numerical method.
[in]	config	- Definition of the particular problem.
[in]	iMesh	- Index of the mesh in multigrid computations.

Reimplemented from CSolver.

Upwind_Residual()

void CIncEulerSolver::Upwind_Residual ( CGeometry *  geometry, CSolver **  solver_container, CNumerics **  numerics_container, CConfig *  config, unsigned short  iMesh  )

finalvirtual

Compute the spatial integration using a upwind scheme.

Parameters

[in]	geometry	- Geometrical definition of the problem.
[in]	solver_container	- Container vector with all the solutions.
[in]	numerics_container	- Description of the numerical method.
[in]	config	- Definition of the particular problem.
[in]	iMesh	- Index of the mesh in multigrid computations.

Reimplemented from CSolver.

Member Data Documentation

alpha_p

su2activevector CIncEulerSolver::alpha_p

protected

EdgeMassFluxCorrection

su2activevector CIncEulerSolver::EdgeMassFluxCorrection

protected

FluidModel

vector<CFluidModel*> CIncEulerSolver::FluidModel

protected

fluid model used in the solver.

momentumCorrection

su2activematrix CIncEulerSolver::momentumCorrection

protected

pressure_based

bool CIncEulerSolver::pressure_based

protected

pressureCorrection

su2activevector CIncEulerSolver::pressureCorrection

protected

SPvals

StreamwisePeriodicValues CIncEulerSolver::SPvals

protected

SPvalsUpdated

StreamwisePeriodicValues CIncEulerSolver::SPvalsUpdated

protected

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The documentation for this class was generated from the following files:

• SU2_CFD/include/solvers/CIncEulerSolver.hpp
• SU2_CFD/src/solvers/CIncEulerSolver.cpp