CNSSolver Class Reference

Main class for defining the Navier-Stokes flow solver. More...

#include <CNSSolver.hpp>

Inheritance diagram for CNSSolver:

Public Member Functions
	CNSSolver ()=default
	Constructor of the class.
	CNSSolver (CGeometry *geometry, CConfig *config, unsigned short iMesh)
	~CNSSolver ()=default
	Destructor of the class.
su2double	GetSurface_Buffet_Metric (unsigned short val_marker) const override
	Provide the buffet metric.
su2double	GetTotal_Buffet_Metric () const override
	Get the buffet metric.
void	Preprocessing (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh, unsigned short iRKStep, unsigned short RunTime_EqSystem, bool Output) override
	Restart residual and compute gradients.
void	Evaluate_ObjFunc (const CConfig *config, CSolver **solver) override
	Compute weighted-sum "combo" objective output.
void	BC_HeatFlux_Wall (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) override
	Impose a constant heat-flux condition at the wall.
void	BC_HeatTransfer_Wall (const CGeometry *geometry, const CConfig *config, const unsigned short val_marker) override
	Impose a heat flux by prescribing a heat transfer coefficient and a temperature at infinity.
void	BC_Isothermal_Wall (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) override
	Impose the Navier-Stokes boundary condition (strong).
void	BC_ConjugateHeat_Interface (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short val_marker) override
	Impose the Navier-Stokes boundary condition (strong) with values from a CHT coupling.
void	Buffet_Monitoring (const CGeometry *geometry, const CConfig *config) override
	Compute the buffet sensor.
su2double	GetBuffetSensor (unsigned short val_marker, unsigned long val_vertex) const override
	Get the value of the buffet sensor.
Public Member Functions inherited from CEulerSolver
	CEulerSolver ()=delete
	CEulerSolver (CGeometry *geometry, CConfig *config, unsigned short iMesh, const bool navier_stokes=false)
	Main constructor of this class.
	~CEulerSolver (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) override
	Source term integration.
void	Source_Template (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short iMesh) final
	Source term integration.
void	SetPreconditioner (const CConfig *config, unsigned long iPoint, su2double delta, su2activematrix &preconditioner) const
	Compute the preconditioner for convergence acceleration by Roe-Turkel method.
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_ActDisk_Inlet (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) final
	Impose the engine inflow boundary condition.
void	BC_ActDisk_Outlet (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) final
	Impose the engine exhaust boundary condition.
void	BC_ActDisk (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker, bool val_inlet_surface) final
	Impose an actuator disk inlet boundary condition.
void	BC_ActDisk_VariableLoad (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker, bool val_inlet_surface)
	Impose an actuator disk with variable load boundary condition.
void	BC_Riemann (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) final
	Impose the boundary condition using characteristic recostruction.
void	BC_TurboRiemann (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) final
	Impose the boundary condition using characteristic recostruction.
void	PreprocessBC_Giles (CGeometry *geometry, CConfig *config, CNumerics *conv_numerics, unsigned short marker_flag) final
	It computes Fourier transformation for the needed quantities along the pitch for each span in turbomachinery analysis.
void	BC_Giles (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) final
	Impose the boundary condition using characteristic recostruction.
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_Supersonic_Inlet (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) final
	Impose a supersonic inlet boundary condition.
void	BC_Supersonic_Outlet (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) final
	Impose a supersonic outlet 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	BC_Engine_Inflow (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) final
	Impose the nacelle inflow boundary condition.
void	BC_Engine_Exhaust (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) final
	Impose the ancelle exhaust 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 fourth-order Runge-Kutta scheme.
bool	FixedCL_Convergence (CConfig *config, bool convergence) final
	Check for convergence of the Fixed CL mode to the target CL.
bool	GetStart_AoA_FD (void) const final
	Checking whether fixed CL mode in finite-differencing mode.
bool	GetEnd_AoA_FD (void) const final
	Checking whether fixed CL mode in finite-differencing mode.
unsigned long	GetIter_Update_AoA (void) const final
	Get the iteration of the last AoA update (Fixed CL Mode)
su2double	GetPrevious_AoA (void) const final
	Get the AoA before the most recent update.
su2double	GetAoA_inc (void) const final
	Get the CL Driver's control command.
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	ComputeUnderRelaxationFactor (const CConfig *config) final
	Compute a suitable under-relaxation parameter to limit the change in the solution variables over a nonlinear iteration for stability.
void	IdentifySolutionOutliers (const CConfig *config, unsigned long iter) final
	Identify points where the static temperature is an outlier to treat them as non-physical, e.g. force the reconstruction to be 1st order.
su2double	GetInflow_MassFlow (unsigned short val_marker) const final
	Provide the mass flow rate.
su2double	GetExhaust_MassFlow (unsigned short val_marker) const final
	Provide the mass flow rate.
su2double	GetInflow_Pressure (unsigned short val_marker) const final
	Provide the mass flow rate.
su2double	GetInflow_Mach (unsigned short val_marker) const final
	Provide the mass flow rate.
su2double	GetTotal_AeroCD () const final
	Provide the total (inviscid + viscous) non dimensional aero CD.
su2double	GetTotal_CNearFieldOF () const final
	Provide the total (inviscid + viscous) non dimensional Near-Field pressure coefficient.
void	SetTotal_AeroCD (su2double val_aerocd) final
	Set the value of the Aero drag.
su2double	GetTotal_NetThrust () const final
	Provide the total (inviscid + viscous) non dimensional drag coefficient.
su2double	GetTotal_Power () const final
	Provide the total (inviscid + viscous) non dimensional drag coefficient.
su2double	GetTotal_SolidCD () const final
	Provide the total (inviscid + viscous) non dimensional drag coefficient.
su2double	GetTotal_ReverseFlow () const final
	Provide the total (inviscid + viscous) non dimensional drag coefficient.
su2double	GetTotal_MFR () const final
	Provide the total (inviscid + viscous) non dimensional drag coefficient.
su2double	GetTotal_Prop_Eff () const final
	Provide the total (inviscid + viscous) non dimensional drag coefficient.
su2double	GetTotal_ByPassProp_Eff () const final
	Provide the total (inviscid + viscous) non dimensional drag coefficient.
su2double	GetTotal_Adiab_Eff () const final
	Provide the total (inviscid + viscous) non dimensional drag coefficient.
su2double	GetTotal_Poly_Eff () const final
	Provide the total (inviscid + viscous) non dimensional drag coefficient.
su2double	GetTotal_IDC () const final
	Provide the total (inviscid + viscous) non dimensional drag coefficient.
su2double	GetTotal_IDC_Mach () const final
	Provide the total (inviscid + viscous) non dimensional drag coefficient.
su2double	GetTotal_IDR () const final
	Provide the total (inviscid + viscous) non dimensional drag coefficient.
su2double	GetTotal_DC60 () const final
	Provide the total (inviscid + viscous) non dimensional drag coefficient.
void	SetTotal_NetThrust (su2double val_Total_NetThrust) final
	Store the total (inviscid + viscous) non dimensional drag coefficient.
void	SetTotal_Power (su2double val_Total_Power) final
	Store the total (inviscid + viscous) non dimensional drag coefficient.
void	SetTotal_SolidCD (su2double val_Total_SolidCD) final
	Store the total (inviscid + viscous) non dimensional drag coefficient.
void	SetTotal_ReverseFlow (su2double val_Total_ReverseFlow) final
	Store the total (inviscid + viscous) non dimensional drag coefficient.
void	SetTotal_MFR (su2double val_Total_MFR) final
	Store the total (inviscid + viscous) non dimensional drag coefficient.
void	SetTotal_Prop_Eff (su2double val_Total_Prop_Eff) final
	Store the total (inviscid + viscous) non dimensional drag coefficient.
void	SetTotal_ByPassProp_Eff (su2double val_Total_ByPassProp_Eff) final
	Store the total (inviscid + viscous) non dimensional drag coefficient.
void	SetTotal_Adiab_Eff (su2double val_Total_Adiab_Eff) final
	Store the total (inviscid + viscous) non dimensional drag coefficient.
void	SetTotal_Poly_Eff (su2double val_Total_Poly_Eff) final
	Store the total (inviscid + viscous) non dimensional drag coefficient.
void	SetTotal_IDC (su2double val_Total_IDC) final
	Store the total (inviscid + viscous) non dimensional drag coefficient.
void	SetTotal_IDC_Mach (su2double val_Total_IDC_Mach) final
	Store the total (inviscid + viscous) non dimensional drag coefficient.
void	SetTotal_IDR (su2double val_Total_IDR) final
	Store the total (inviscid + viscous) non dimensional drag coefficient.
void	SetTotal_DC60 (su2double val_Total_DC60) final
	Store the total (inviscid + viscous) non dimensional drag coefficient.
unsigned long	GetDonorGlobalIndex (unsigned short val_marker, unsigned long val_vertex) const final
	Value of the characteristic global index at the boundaries.
void	SetDonorGlobalIndex (unsigned short val_marker, unsigned long val_vertex, unsigned long val_index) final
	Value of the characteristic global index at the boundaries.
void	SetInitialCondition (CGeometry **geometry, CSolver ***solver_container, CConfig *config, unsigned long TimeIter) final
	Set the initial condition for the Euler Equations.
void	SetFreeStream_Solution (const CConfig *config) final
	Set the solution using the Freestream values.
void	InitTurboContainers (CGeometry *geometry, CConfig **config, unsigned short iZone) final
	Initilize turbo containers.
vector< su2double >	GetTurboPrimitive (unsigned short iBlade, unsigned short iSpan, bool INLET) override
	Get Primal variables for turbo performance computation iteration can be executed by multiple threads.
void	SetFreeStream_TurboSolution (CConfig *config) final
	Set the solution using the Freestream values.
void	PreprocessAverage (CSolver **solver, CGeometry *geometry, CConfig *config, unsigned short marker_flag) final
	It computes average quantities along the span for turbomachinery analysis.
void	TurboAverageProcess (CSolver **solver, CGeometry *geometry, CConfig *config, unsigned short marker_flag) final
	It computes average quantities along the span for turbomachinery analysis.
void	ComputeTurboBladePerformance (CGeometry *geometry, CConfig *config, unsigned short iBlade) final
void	MixedOut_Average (CConfig *config, su2double val_init_pressure, const su2double *val_Averaged_Flux, const su2double *val_normal, su2double &pressure_mix, su2double &density_mix)
	it performs a mixed out average of the nodes of a boundary.
void	GatherInOutAverageValues (CConfig *config, CGeometry *geometry) final
	It gathers into the master node average quantities at inflow and outflow needed for turbomachinery analysis.
void	ComputeTurboVelocity (const su2double *cartesianVelocity, const su2double *turboNormal, su2double *turboVelocity, unsigned short marker_flag, TURBOMACHINERY_TYPE kind_turb)
	it take a velocity in the cartesian reference of framework and transform into the turbomachinery frame of reference.
std::shared_ptr< CTurboOutput >	GetTurboBladePerformance () const final
void	ComputeBackVelocity (const su2double *turboVelocity, const su2double *turboNormal, su2double *cartesianVelocity, unsigned short marker_flag, TURBOMACHINERY_TYPE kind_turb)
	it take a velocity in the cartesian reference of framework and transform into the turbomachinery frame of reference.
su2double	GetAverageDensity (unsigned short valMarker, unsigned short valSpan) const final
	Provide the average density at the boundary of interest.
su2double	GetAveragePressure (unsigned short valMarker, unsigned short valSpan) const final
	Provide the average pressure at the boundary of interest.
const su2double *	GetAverageTurboVelocity (unsigned short valMarker, unsigned short valSpan) const final
	Provide the average turbo velocity average at the boundary of interest.
su2double	GetAverageNu (unsigned short valMarker, unsigned short valSpan) const final
	Provide the average density at the boundary of interest.
su2double	GetAverageKine (unsigned short valMarker, unsigned short valSpan) const final
	Provide the average density at the boundary of interest.
su2double	GetAverageOmega (unsigned short valMarker, unsigned short valSpan) const final
	Provide the average density at the boundary of interest.
su2double	GetDensityIn (unsigned short inMarkerTP, unsigned short valSpan) const final
	Provide the inlet density to check convergence of conservative mixing-plane.
su2double	GetPressureIn (unsigned short inMarkerTP, unsigned short valSpan) const final
	Provide the inlet pressure to check convergence of conservative mixing-plane.
const su2double *	GetTurboVelocityIn (unsigned short inMarkerTP, unsigned short valSpan) const final
	Provide the inlet normal velocity to check convergence of conservative mixing-plane.
su2double	GetDensityOut (unsigned short inMarkerTP, unsigned short valSpan) const final
	Provide the outlet density to check convergence of conservative mixing-plane.
su2double	GetPressureOut (unsigned short inMarkerTP, unsigned short valSpan) const final
	Provide the outlet pressure to check convergence of conservative mixing-plane.
const su2double *	GetTurboVelocityOut (unsigned short inMarkerTP, unsigned short valSpan) const final
	Provide the outlet normal velocity to check convergence of conservative mixing-plane.
su2double	GetKineIn (unsigned short inMarkerTP, unsigned short valSpan) const final
	Provide the inlet turbulent kei to check convergence of conservative mixing-plane.
su2double	GetOmegaIn (unsigned short inMarkerTP, unsigned short valSpan) const final
	Provide the inlet turbulent omega to check convergence of conservative mixing-plane.
su2double	GetNuIn (unsigned short inMarkerTP, unsigned short valSpan) const final
	Provide the inlet turbulent nu to check convergence of conservative mixing-plane.
su2double	GetKineOut (unsigned short inMarkerTP, unsigned short valSpan) const final
	Provide the outlet turbulent kei to check convergence of conservative mixing-plane.
su2double	GetOmegaOut (unsigned short inMarkerTP, unsigned short valSpan) const final
	Provide the outlet turbulent omega to check convergence of conservative mixing-plane.
su2double	GetNuOut (unsigned short inMarkerTP, unsigned short valSpan) const final
	Provide the outlet turbulent nu to check convergence of conservative mixing-plane.
void	SetDensityIn (su2double value, unsigned short inMarkerTP, unsigned short valSpan) final
	Set inlet density.
void	SetPressureIn (su2double value, unsigned short inMarkerTP, unsigned short valSpan) final
	Set inlet pressure.
void	SetTurboVelocityIn (const su2double *value, unsigned short inMarkerTP, unsigned short valSpan) final
	Set inlet normal velocity.
void	SetDensityOut (su2double value, unsigned short inMarkerTP, unsigned short valSpan) final
	Set outlet density.
void	SetPressureOut (su2double value, unsigned short inMarkerTP, unsigned short valSpan) final
	Set outlet pressure.
void	SetTurboVelocityOut (const su2double *value, unsigned short inMarkerTP, unsigned short valSpan) final
	Set outlet normal velocity.
void	SetKineIn (su2double value, unsigned short inMarkerTP, unsigned short valSpan) final
	Set inlet turbulent kei.
void	SetOmegaIn (su2double value, unsigned short inMarkerTP, unsigned short valSpan) final
	Set inlet turbulent omega.
void	SetNuIn (su2double value, unsigned short inMarkerTP, unsigned short valSpan) final
	Set inlet turbulent Nu.
void	SetKineOut (su2double value, unsigned short inMarkerTP, unsigned short valSpan) final
	Set outlet turbulent kei.
void	SetOmegaOut (su2double value, unsigned short inMarkerTP, unsigned short valSpan) final
	Set Outlet turbulent omega.
void	SetNuOut (su2double value, unsigned short inMarkerTP, unsigned short valSpan) final
	Set outlet turbulent Nu.
void	PrintVerificationError (const CConfig *config) const final
	Print verification error to screen.
bool	GetHasHybridParallel () const final
	The Euler and NS solvers support MPI+OpenMP.
Public Member Functions inherited from CFVMFlowSolverBase< CEulerVariable, ENUM_REGIME::COMPRESSIBLE >
void	Set_NewSolution () final
	Set the new solution variables to the current solution value for classical RK.
void	LoadRestart (CGeometry **geometry, CSolver ***solver, CConfig *config, int iter, bool update_geo) override
	Load a solution from a restart file.
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	SetResidual_DualTime (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iRKStep, unsigned short iMesh, unsigned short RunTime_EqSystem) override
	Set the total residual adding the term that comes from the Dual Time Strategy.
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.
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	ComputeEdgeMassFluxesRhieChow (CGeometry *geometry, CSolver **solver_container, CConfig *config)
	A virtual member.
virtual void	ApplyPressureVelocityCorrection (CGeometry *geometry, CSolver **solver_container, CConfig *config)
	A virtual member.
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_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_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.
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.
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	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	GetTotal_AvgTemperature () const
	A virtual member.
virtual su2double	GetTotal_CFEA () 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_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 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	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 unsigned long	RegisterSolutionExtra (bool input, const CConfig *config)
	Register In- or Output.
virtual void	SetAdjoint_SolutionExtra (const su2activevector &adj_sol, const CConfig *config)
	Seed the adjoint of the extra solution at the output.
virtual void	ExtractAdjoint_SolutionExtra (su2activevector &adj_sol, const CConfig *config)
	Extract the adjoint of the extra solution at the input.
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 su2double	GetAverageMassFlowRate (unsigned short valMarker) const
	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 StreamwisePeriodicValues	GetStreamwisePeriodicValues () const
	Get values for streamwise periodic flow: delta P, m_dot, inlet T, integrated heat, etc.
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)

Additional Inherited Members
Static Public Member Functions inherited from CEulerSolver
static void	ComputeConsistentExtrapolation (CFluidModel *fluidModel, unsigned short nDim, su2double *primitive, su2double *secondary)
	Recompute the extrapolated quantities, after MUSCL reconstruction, in a more thermodynamically consistent way.
static void	LowMachPrimitiveCorrection (CFluidModel *fluidModel, unsigned short nDim, su2double *primitive_i, su2double *primitive_j)
	Apply low Mach number correction to the primitives at two points, usually connected by an edge.
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.
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 CEulerSolver
using	BaseClass = CFVMFlowSolverBase< CEulerVariable, ENUM_REGIME::COMPRESSIBLE >
Protected Types inherited from CSolver
enum	: size_t { OMP_MIN_SIZE = 32 }
Protected Member Functions inherited from CEulerSolver
su2double	GetTangGridVelIn (unsigned short val_blade, unsigned long val_span)
su2double	GetTangGridVelOut (unsigned short val_blade, unsigned long val_span)
su2double	GetMixingState (unsigned short val_marker, unsigned long val_span, unsigned short val_state) const final
	Get a component of the donor-side averaged state at a mixing plane interface.
void	SetMixingState (unsigned short val_marker, unsigned long val_span, unsigned short val_state, su2double component) final
	Set a component of the donor-side averaged state at a mixing plane interface nodes.
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	SetFarfield_AoA (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh, bool Output)
	Update the AoA and freestream velocity at the farfield.
void	SetUpwind_Ducros_Sensor (CGeometry *geometry, CConfig *config)
	Compute Ducros Sensor for Roe Dissipation.
void	GetPower_Properties (CGeometry *geometry, CConfig *config, unsigned short iMesh, bool Output)
	Compute the Fan face Mach number.
void	Set_MPI_ActDisk (CSolver **solver_container, CGeometry *geometry, CConfig *config)
	Parallelization of Undivided Laplacian.
void	SetActDisk_BCThrust (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh, bool Output)
	Update the AoA and freestream velocity at the farfield.
void	ReadActDisk_InputFile (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh, bool Output)
	Read the actuator disk input file for the VARIABLE_LOAD type.
void	SetActDisk_BEM_VLAD (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh, bool Output)
	Read and update the variable load actuator disk from input file for the BLADE_ELEMENT type.
void	SetMax_Eigenvalue (CGeometry *geometry, const CConfig *config)
	Compute the max eigenvalue.
void	SetUndivided_Laplacian (CGeometry *geometry, const CConfig *config)
	Compute the undivided laplacian for the solution.
void	SetCentered_Dissipation_Sensor (CGeometry *geometry, const CConfig *config)
	Compute the dissipation sensor for centered schemes.
void	SetCoefficient_Gradients (CConfig *config) const
	Set gradients of coefficients for fixed CL mode.
void	InstantiateEdgeNumerics (const CSolver *const *solvers, const CConfig *config) final
	Instantiate a SIMD numerics object.
void	SetNondimensionalization (CConfig *config, unsigned short iMesh)
	Set the solver nondimensionalization.
void	SetReferenceValues (const CConfig &config) final
	Set reference values for pressure, forces, etc.
Protected Member Functions inherited from CFVMFlowSolverBase< CEulerVariable, ENUM_REGIME::COMPRESSIBLE >
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	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.
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.
Static Protected Member Functions inherited from CFVMFlowSolverBase< CEulerVariable, ENUM_REGIME::COMPRESSIBLE >
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.
Protected Attributes inherited from CEulerSolver
su2double	Prandtl_Turb = 0.0
	Turbulent Prandtl number.
su2double	AllBound_CEquivArea_Inv =0.0
	equivalent area coefficient (inviscid contribution) for all the boundaries.
vector< su2double >	CEquivArea_Mnt
	Equivalent area (inviscid contribution) for each boundary.
vector< su2double >	CEquivArea_Inv
	Equivalent area (inviscid contribution) for each boundary.
vector< su2double >	Inflow_MassFlow
	Mass flow rate for each boundary.
vector< su2double >	Exhaust_MassFlow
	Mass flow rate for each boundary.
vector< su2double >	Inflow_Pressure
	Fan face pressure for each boundary.
vector< su2double >	Inflow_Mach
	Fan face mach number for each boundary.
vector< su2double >	Inflow_Area
	Boundary total area.
vector< su2double >	Exhaust_Area
	Boundary total area.
vector< su2double >	Exhaust_Pressure
	Fan face pressure for each boundary.
vector< su2double >	Exhaust_Temperature
	Fan face mach number for each boundary.
su2double	Inflow_MassFlow_Total = 0.0
	Mass flow rate for each boundary.
su2double	Exhaust_MassFlow_Total = 0.0
	Mass flow rate for each boundary.
su2double	Inflow_Pressure_Total = 0.0
	Fan face pressure for each boundary.
su2double	Inflow_Mach_Total = 0.0
	Fan face mach number for each boundary.
su2double	InverseDesign = 0.0
	Inverse design functional for each boundary.
vector< vector< unsigned long > >	DonorGlobalIndex
	Value of the donor global index.
vector< su2activematrix >	DonorPrimVar
	Value of the donor variables at each boundary.
vector< vector< su2double > >	ActDisk_DeltaP
	Value of the Delta P.
vector< vector< su2double > >	ActDisk_DeltaP_r
	Value of the DeltaP_r.
vector< vector< su2double > >	ActDisk_Thrust_r
	Value of the Thrust_r.
vector< vector< su2double > >	ActDisk_Torque_r
	Value of the Torque_r.
vector< vector< su2double > >	ActDisk_DeltaT
	Value of the Delta T.
su2activevector	ActDisk_R
	Value of the actuator disk Radius.
su2activematrix	ActDisk_C
	Value of the actuator disk Center.
su2activematrix	ActDisk_Axis
	Value of the actuator disk Axis.
vector< vector< su2double > >	ActDisk_Fa
	Value of the actuator disk Axial Force per Unit Area.
vector< vector< su2double > >	ActDisk_Fx
	Value of the actuator disk X component of the radial and tangential forces per Unit Area resultant.
vector< vector< su2double > >	ActDisk_Fy
	Value of the actuator disk Y component of the radial and tangential forces per Unit Area resultant.
vector< vector< su2double > >	ActDisk_Fz
	Value of the actuator disk Z component of the radial and tangential forces per Unit Area resultant.
vector< vector< su2double > >	ActDisk_Fa_BEM
	Value of the actuator disk Axial Force per Unit Area.
vector< vector< su2double > >	ActDisk_Fx_BEM
	Value of the actuator disk X component of the radial and tangential forces per Unit Area resultant.
vector< vector< su2double > >	ActDisk_Fy_BEM
	Value of the actuator disk Y component of the radial and tangential forces per Unit Area resultant.
vector< vector< su2double > >	ActDisk_Fz_BEM
	Value of the actuator disk Z component of the radial and tangential forces per Unit Area resultant.
su2double	Total_CL_Prev = 0.0
	Total lift coefficient for all the boundaries (fixed lift mode).
su2double	Total_SolidCD = 0.0
	Total drag coefficient for all the boundaries.
su2double	Total_CD_Prev = 0.0
	Total drag coefficient for all the boundaries (fixed lift mode).
su2double	Total_NetThrust = 0.0
	Total drag coefficient for all the boundaries.
su2double	Total_Power = 0.0
	Total drag coefficient for all the boundaries.
su2double	Total_ReverseFlow = 0.0
	Total drag coefficient for all the boundaries.
su2double	Total_IDC = 0.0
	Total IDC coefficient for all the boundaries.
su2double	Total_IDC_Mach = 0.0
	Total IDC coefficient for all the boundaries.
su2double	Total_IDR = 0.0
	Total IDC coefficient for all the boundaries.
su2double	Total_DC60 = 0.0
	Total IDC coefficient for all the boundaries.
su2double	Total_MFR = 0.0
	Total Mass Flow Ratio for all the boundaries.
su2double	Total_Prop_Eff = 0.0
	Total Mass Flow Ratio for all the boundaries.
su2double	Total_ByPassProp_Eff = 0.0
	Total Mass Flow Ratio for all the boundaries.
su2double	Total_Adiab_Eff = 0.0
	Total Mass Flow Ratio for all the boundaries.
su2double	Total_Poly_Eff = 0.0
	Total Mass Flow Ratio for all the boundaries.
su2double	Total_CMx_Prev = 0.0
	Total drag coefficient for all the boundaries (fixed lift mode).
su2double	Total_CMy_Prev = 0.0
	Total drag coefficient for all the boundaries (fixed lift mode).
su2double	Total_CMz_Prev = 0.0
	Total drag coefficient for all the boundaries (fixed lift mode).
su2double	Total_AeroCD = 0.0
	Total aero drag coefficient for all the boundaries.
su2double	Total_CEquivArea = 0.0
	Total Equivalent Area coefficient for all the boundaries.
su2double	AoA_Prev
	Old value of the angle of attack (monitored).
su2double	AoA_inc
bool	Start_AoA_FD = false
	Boolean for start of finite differencing for FixedCL mode.
bool	End_AoA_FD = false
	Boolean for end of finite differencing for FixedCL mode.
bool	Update_AoA = false
	Boolean to signal Angle of Attack Update.
unsigned long	Iter_Update_AoA = 0
	Iteration at which AoA was updated last.
su2double	dCL_dAlpha
	Value of dCL_dAlpha used to control CL in fixed CL mode.
unsigned long	BCThrust_Counter
vector< CFluidModel * >	FluidModel
	fluid model used in the solver.
su2double	MeanTemperature
su2double	StdDevTemperature
vector< su2activematrix >	AverageFlux
vector< su2activematrix >	SpanTotalFlux
vector< su2activematrix >	AverageVelocity
vector< su2activematrix >	AverageTurboVelocity
vector< su2activematrix >	OldAverageTurboVelocity
su2activematrix	AveragePressure
su2activematrix	OldAveragePressure
su2activematrix	RadialEquilibriumPressure
su2activematrix	AverageDensity
su2activematrix	OldAverageDensity
su2activematrix	AverageNu
su2activematrix	AverageKine
su2activematrix	AverageOmega
su2activevector	AverageMassFlowRate
su2activematrix	AverageRelTangVelocity
su2activematrix	DensityIn
su2activematrix	PressureIn
vector< su2activematrix >	TurboVelocityIn
su2activematrix	DensityOut
su2activematrix	PressureOut
vector< su2activematrix >	TurboVelocityOut
su2activematrix	KineIn
su2activematrix	OmegaIn
su2activematrix	NuIn
su2activematrix	KineOut
su2activematrix	OmegaOut
su2activematrix	NuOut
su2activematrix	RelTangVelocityIn
su2activematrix	RelTangVelocityOut
su2double	ExtAverageDensity
su2double	ExtAveragePressure
su2activevector	ExtAverageTurboVelocity
vector< su2matrix< complex< su2double > > >	CkInflow
vector< su2matrix< complex< su2double > > >	CkOutflow1
vector< su2matrix< complex< su2double > > >	CkOutflow2
vector< su2activematrix >	MixingState
Protected Attributes inherited from CFVMFlowSolverBase< CEulerVariable, ENUM_REGIME::COMPRESSIBLE >
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.
CEulerVariable *	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.
Static Protected Attributes inherited from CEulerSolver
static constexpr unsigned short	nMixingStateVars = 8
	Number of averaged variables transferred across mixing plane interfaces.
Static Protected Attributes inherited from CFVMFlowSolverBase< CEulerVariable, ENUM_REGIME::COMPRESSIBLE >
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 Navier-Stokes flow solver.

Author

F. Palacios

Constructor & Destructor Documentation

CNSSolver() [1/2]

CNSSolver::CNSSolver ( )

default

Constructor of the class.

CNSSolver() [2/2]

CNSSolver::CNSSolver	(	CGeometry *	geometry,
		CConfig *	config,
		unsigned short	iMesh
	)

This is an overloaded member function, provided for convenience. It differs from the above function only in what argument(s) it accepts.

Parameters

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

~CNSSolver()

CNSSolver::~CNSSolver ( )

default

Destructor of the class.

Member Function Documentation

BC_ConjugateHeat_Interface()

void CNSSolver::BC_ConjugateHeat_Interface ( CGeometry *  geometry, CSolver **  solver_container, CNumerics *  numerics, CConfig *  config, unsigned short  val_marker  )

overridevirtual

Impose the Navier-Stokes boundary condition (strong) with values from a CHT coupling.

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_HeatFlux_Wall()

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

overridevirtual

Impose a constant heat-flux condition at the wall.

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_HeatTransfer_Wall()

void CNSSolver::BC_HeatTransfer_Wall ( const CGeometry *  geometry, const CConfig *  config, const unsigned short  val_marker  )

overridevirtual

Impose a heat flux by prescribing a heat transfer coefficient and a temperature at infinity.

Parameters

[in]	geometry	- Geometrical definition of the problem.
[in]	config	- Definition of the particular problem.
[in]	val_marker	- Surface marker where the boundary condition is applied.

Reimplemented from CSolver.

BC_Isothermal_Wall()

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

overridevirtual

Impose the Navier-Stokes boundary condition (strong).

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.

Buffet_Monitoring()

void CNSSolver::Buffet_Monitoring ( const CGeometry *  geometry, const CConfig *  config  )

overridevirtual

Compute the buffet sensor.

Parameters

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

Reimplemented from CFVMFlowSolverBase< CEulerVariable, ENUM_REGIME::COMPRESSIBLE >.

Evaluate_ObjFunc()

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

overridevirtual

Compute weighted-sum "combo" objective output.

Parameters

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

Reimplemented from CEulerSolver.

GetBuffetSensor()

su2double CNSSolver::GetBuffetSensor ( unsigned short  val_marker, unsigned long  val_vertex  ) const

inlineoverridevirtual

Get the value of the buffet sensor.

Parameters

[in]	val_marker	- Surface marker where the coefficient is computed.
[in]	val_vertex	- Vertex of the marker val_marker where the coefficient is evaluated.

Returns

Value of the buffet sensor.

Reimplemented from CSolver.

GetSurface_Buffet_Metric()

su2double CNSSolver::GetSurface_Buffet_Metric ( unsigned short  val_marker ) const

inlineoverridevirtual

Provide the buffet metric.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the buffet metric on the surface val_marker.

Reimplemented from CSolver.

GetTotal_Buffet_Metric()

su2double CNSSolver::GetTotal_Buffet_Metric ( ) const

inlineoverridevirtual

Get the buffet metric.

Returns

Value of the buffet metric.

Reimplemented from CSolver.

Preprocessing()

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

overridevirtual

Restart residual and compute 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 CEulerSolver.

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

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