CFVMFlowSolverBase< VariableType, FlowRegime > Class Template Reference

#include <CFVMFlowSolverBase.hpp>

Inheritance diagram for CFVMFlowSolverBase< VariableType, FlowRegime >:

Classes
struct	AeroCoeffs
	Scalar version of the coefficients type. More...
struct	AeroCoeffsArray
	Auxilary types to store common aero coefficients (avoids repeating oneself so much). More...

Public Member Functions
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.
virtual void	PrintVerificationError (const CConfig *config) const =0
	Print verification error to screen, derived solvers must define this.
void	Pressure_Forces (const CGeometry *geometry, const CConfig *config) final
	Compute the pressure forces and all the adimensional coefficients.
void	Momentum_Forces (const CGeometry *geometry, const CConfig *config) final
	Compute the pressure forces and all the adimensional coefficients.
void	Friction_Forces (const CGeometry *geometry, const CConfig *config) final
	Compute the viscous forces and all the addimensional coefficients.
virtual void	Buffet_Monitoring (const CGeometry *geometry, const CConfig *config)
	Compute the buffet sensor.
void	SetSlidingStateStructure (unsigned short val_marker, unsigned long val_vertex) final
	Allocates the final pointer of SlidingState depending on how many donor vertex donate to it. That number is stored in SlidingStateNodes[val_marker][val_vertex].
void	SetSlidingState (unsigned short val_marker, unsigned long val_vertex, unsigned short val_state, unsigned long donor_index, su2double component) final
	Set the outer state for fluid interface nodes.
void	SetnSlidingStates (unsigned short val_marker, unsigned long val_vertex, int value) final
	Set the number of outer state for fluid interface nodes.
int	GetnSlidingStates (unsigned short val_marker, unsigned long val_vertex) const final
	Get the number of outer state for fluid interface nodes.
su2double	GetSlidingState (unsigned short val_marker, unsigned long val_vertex, unsigned short val_state, unsigned long donor_index) const final
	Get the outer state for fluid interface nodes.
void	SetConjugateHeatVariable (unsigned short val_marker, unsigned long val_vertex, unsigned short pos_var, su2double relaxation_factor, su2double val_var) final
	Set the conjugate heat variables.
su2double	GetConjugateHeatVariable (unsigned short val_marker, unsigned long val_vertex, unsigned short pos_var) const final
	Set the conjugate heat variables.
su2double	GetCSkinFriction (unsigned short val_marker, unsigned long val_vertex, unsigned short val_dim) const final
	Get the skin friction coefficient.
su2double	GetWallShearStress (unsigned short val_marker, unsigned long val_vertex) const final
	Get the wall shear stress.
su2double	GetHeatFlux (unsigned short val_marker, unsigned long val_vertex) const final
	Get the heat flux.
su2double	GetHeatFluxTarget (unsigned short val_marker, unsigned long val_vertex) const final
	Get the skin friction coefficient.
void	SetHeatFluxTarget (unsigned short val_marker, unsigned long val_vertex, su2double val_heat) final
	Set the value of the target Pressure coefficient.
su2double	GetYPlus (unsigned short val_marker, unsigned long val_vertex) const final
	Get the y plus.
su2double	GetUTau (unsigned short val_marker, unsigned long val_vertex) const final
	Get the u_tau .
su2double	GetEddyViscWall (unsigned short val_marker, unsigned long val_vertex) const final
	Get the eddy viscosity at the wall (wall functions).
const su2activevector *	GetEdgeMassFluxes () const final
	Get the mass fluxes across the edges (computed and stored during the discretization of convective fluxes).
Public Member Functions inherited from CSolver
	CSolver (LINEAR_SOLVER_MODE linear_solver_mode=LINEAR_SOLVER_MODE::STANDARD)
	Constructor of the class.
virtual	~CSolver (void)
	Destructor of the class.
CVariable *	GetNodes ()
	Allow outside access to the nodes of the solver, containing conservatives, primitives, etc.
const CVariable *	GetNodes () const
bool	HasPeriodicRotation (const CConfig &config) const
void	GetCommCountAndType (const CConfig *config, MPI_QUANTITIES commType, unsigned short &COUNT_PER_POINT, COMM_TYPE &MPI_TYPE) const
	Helper function to define the type and number of variables per point for each communication type.
void	InitiateComms (CGeometry *geometry, const CConfig *config, MPI_QUANTITIES commType)
	Routine to load a solver quantity into the data structures for MPI point-to-point communication and to launch non-blocking sends and recvs.
void	CompleteComms (CGeometry *geometry, const CConfig *config, MPI_QUANTITIES commType)
	Routine to complete the set of non-blocking communications launched by InitiateComms() and unpacking of the data in the solver class.
void	GetPeriodicCommCountAndType (const CConfig *config, unsigned short commType, unsigned short &COUNT_PER_POINT, COMM_TYPE &MPI_TYPE, unsigned short &ICOUNT, unsigned short &JCOUNT) const
	Helper function to define the type and number of variables per point for each communication type.
void	InitiatePeriodicComms (CGeometry *geometry, const CConfig *config, unsigned short val_periodic_index, unsigned short commType)
	Routine to load a solver quantity into the data structures for MPI periodic communication and to launch non-blocking sends and recvs.
void	CompletePeriodicComms (CGeometry *geometry, const CConfig *config, unsigned short val_periodic_index, unsigned short commType)
	Routine to complete the set of non-blocking periodic communications launched by InitiatePeriodicComms() and unpacking of the data in the solver class.
void	SetIterLinSolver (unsigned short val_iterlinsolver)
	Set number of linear solver iterations.
void	SetResLinSolver (su2double val_reslinsolver)
	Set the final linear solver residual.
void	SetResidual_RMS (const CGeometry *geometry, const CConfig *config, bool force=false)
	Set the value of the max residual and RMS residual.
void	SetResidual_BGS (const CGeometry *geometry, const CConfig *config)
	Communicate the value of the max residual and RMS residual.
void	ComputeResidual_Multizone (const CGeometry *geometry, const CConfig *config)
	Set the value of the max residual and RMS residual.
virtual void	SetDualTime_Mesh (void)
	Move the mesh in time.
bool	GetAdjoint (void) const
	Get information whether the initialization is an adjoint solver or not.
virtual CFluidModel *	GetFluidModel (void) const
	Compute the pressure at the infinity.
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	SetTime_Step (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh, unsigned long Iteration)
	A virtual member.
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	Centered_Residual (CGeometry *geometry, CSolver **solver_container, CNumerics **numerics_container, CConfig *config, unsigned short iMesh, unsigned short iRKStep)
	A virtual member.
virtual void	Upwind_Residual (CGeometry *geometry, CSolver **solver_container, CNumerics **numerics_container, CConfig *config, unsigned short iMesh)
	A virtual member.
virtual void	Preprocessing (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh, unsigned short iRKStep, unsigned short RunTime_EqSystem, bool Output)
	A virtual member.
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	Evaluate_ObjFunc (const CConfig *config, CSolver **solver)
	Compute weighted-sum "combo" objective output.
virtual void	BC_Clamped (CGeometry *geometry, const CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_Clamped_Post (CGeometry *geometry, const CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_Sym_Plane (CGeometry *geometry, const CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_DispDir (CGeometry *geometry, const CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_Normal_Displacement (CGeometry *geometry, CNumerics *numerics, const CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_Normal_Load (CGeometry *geometry, const CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_Dir_Load (CGeometry *geometry, const CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_Sine_Load (CGeometry *geometry, const CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_Damper (CGeometry *geometry, const CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_ActDisk_Inlet (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_ActDisk_Outlet (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_ActDisk (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker, bool val_inlet_surface)
	A virtual member.
virtual void	BC_Isothermal_Wall (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_HeatFlux_Wall (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_HeatTransfer_Wall (const CGeometry *geometry, const CConfig *config, const unsigned short val_marker)
	Impose a heat flux by prescribing a heat transfer coefficient and a temperature at infinity.
virtual void	BC_Far_Field (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_Riemann (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_TurboRiemann (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	PreprocessBC_Giles (CGeometry *geometry, CConfig *config, CNumerics *conv_numerics, unsigned short marker_flag)
	It computes Fourier transformation for the needed quantities along the pitch for each span in turbomachinery analysis.
virtual void	BC_Giles (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	A virtual member.
virtual std::shared_ptr< CTurboOutput >	GetTurboBladePerformance () const
virtual void	BC_Inlet (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, 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_Supersonic_Inlet (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_Supersonic_Outlet (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_Outlet (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_Engine_Inflow (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_Engine_Exhaust (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_ConjugateHeat_Interface (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_Smoluchowski_Maxwell (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	Impose_Fixed_Values (const CGeometry *geometry, const CConfig *config)
	Virtual function to apply something like a strong BC to the whole domain.
virtual su2double	GetMixingState (unsigned short val_marker, unsigned long val_span, unsigned short val_state) const
	Get a component of the donor-side averaged state at a mixing plane interface.
virtual void	SetMixingState (unsigned short val_marker, unsigned long val_span, unsigned short val_state, su2double component)
	Set a component of the donor-side averaged state at a mixing plane interface nodes.
virtual void	ExplicitRK_Iteration (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iRKStep)
	A virtual member.
virtual void	ClassicalRK4_Iteration (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iRKStep)
	A virtual member.
virtual void	ExplicitEuler_Iteration (CGeometry *geometry, CSolver **solver_container, CConfig *config)
	A virtual member.
virtual void	PrepareImplicitIteration (CGeometry *geometry, CSolver **solver_container, CConfig *config)
	A virtual member.
void	AdaptCFLNumber (CGeometry **geometry, CSolver ***solver_container, CConfig *config)
	Adapt the CFL number based on the local under-relaxation parameters computed for each nonlinear iteration.
virtual void	IdentifySolutionOutliers (const CConfig *config, unsigned long iter)
	Identify points where the solution is an outlier (physics-specific concept) so that solvers can try to restore them to a stable condition.
void	ResetCFLAdapt ()
	Reset the local CFL adaption variables.
virtual void	ImplicitNewmark_Iteration (const CGeometry *geometry, CNumerics **numerics, const CConfig *config)
	A virtual member.
virtual void	ImplicitNewmark_Update (const CGeometry *geometry, const CConfig *config)
	A virtual member.
virtual void	ImplicitNewmark_Relaxation (const CGeometry *geometry, const CConfig *config)
	A virtual member.
virtual void	GeneralizedAlpha_Iteration (const CGeometry *geometry, CNumerics **numerics, const CConfig *config)
	A virtual member.
virtual void	GeneralizedAlpha_UpdateDisp (const CGeometry *geometry, const CConfig *config)
	A virtual member.
virtual void	GeneralizedAlpha_UpdateSolution (const CGeometry *geometry, const CConfig *config)
	A virtual member.
virtual void	GeneralizedAlpha_UpdateLoads (const CGeometry *geometry, const CConfig *config)
	A virtual member.
virtual void	Heat_Fluxes (CGeometry *geometry, CSolver **solver_container, CConfig *config)
	A virtual member.
virtual void	Source_Residual (CGeometry *geometry, CSolver **solver_container, CNumerics **numerics_container, CConfig *config, unsigned short iMesh)
	A virtual member.
virtual void	Source_Template (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short iMesh)
	A virtual member.
virtual void	SetCSensitivity (unsigned short val_marker, unsigned long val_vertex, su2double val_sensitivity)
	A virtual member.
virtual void	SetForceProj_Vector (CGeometry *geometry, CSolver **solver_container, CConfig *config)
	A virtual member.
virtual void	SetTotal_NetThrust (su2double val_Total_NetThrust)
	A virtual member.
virtual void	SetTotal_Power (su2double val_Total_Power)
	A virtual member.
virtual void	SetTotal_SolidCD (su2double val_Total_SolidCD)
	A virtual member.
virtual void	SetTotal_ReverseFlow (su2double val_Total_ReverseFlow)
	A virtual member.
virtual void	SetTotal_MFR (su2double val_Total_MFR)
	A virtual member.
virtual void	SetTotal_Prop_Eff (su2double val_Total_Prop_Eff)
	A virtual member.
virtual void	SetTotal_ByPassProp_Eff (su2double val_Total_ByPassProp_Eff)
	A virtual member.
virtual void	SetTotal_Adiab_Eff (su2double val_Total_Adiab_Eff)
	A virtual member.
virtual void	SetTotal_Poly_Eff (su2double val_Total_Poly_Eff)
	A virtual member.
virtual void	SetTotal_IDC (su2double val_Total_IDC)
	A virtual member.
virtual void	SetTotal_IDC_Mach (su2double val_Total_IDC_Mach)
	A virtual member.
virtual void	SetTotal_IDR (su2double val_Total_IDR)
	A virtual member.
virtual void	SetTotal_DC60 (su2double val_Total_DC60)
	A virtual member.
virtual void	Inviscid_Sensitivity (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config)
	A virtual member.
virtual void	Smooth_Sensitivity (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config)
	A virtual member.
virtual void	Viscous_Sensitivity (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config)
	A virtual member.
su2double	GetTotal_ComboObj () const
	Provide the total "combo" objective (weighted sum of other values).
void	SetTotal_Custom_ObjFunc (su2double value)
	Sets the value of the custom objective function.
virtual su2double	GetSurface_Buffet_Metric (unsigned short val_marker) const
	A virtual member.
virtual su2double	GetInflow_MassFlow (unsigned short val_marker) const
	A virtual member.
virtual bool	FixedCL_Convergence (CConfig *config, bool convergence)
	A virtual member.
virtual bool	GetStart_AoA_FD (void) const
	A virtual member.
virtual bool	GetEnd_AoA_FD (void) const
	A virtual member.
virtual unsigned long	GetIter_Update_AoA (void) const
	A virtual member.
virtual su2double	GetPrevious_AoA (void) const
	A virtual member.
virtual su2double	GetAoA_inc (void) const
	A virtual member.
virtual su2double	GetExhaust_MassFlow (unsigned short val_marker) const
	A virtual member.
virtual su2double	GetInflow_Pressure (unsigned short val_marker) const
	A virtual member.
virtual su2double	GetInflow_Mach (unsigned short val_marker) const
	A virtual member.
virtual su2double	GetTotal_AvgTemperature () const
	A virtual member.
virtual su2double	GetTotal_AeroCD () const
	A virtual member.
virtual su2double	GetTotal_CFEA () const
	A virtual member.
virtual su2double	GetTotal_CNearFieldOF () const
	A virtual member.
virtual su2double	GetTotal_OFRefGeom () const
	A virtual member.
virtual su2double	GetTotal_OFRefNode () const
	A virtual member.
virtual su2double	GetTotal_OFVolFrac () const
	A virtual member.
virtual su2double	GetTotal_OFDiscreteness () const
	Retrieve the value of the discreteness objective function.
virtual su2double	GetTotal_OFCompliance () const
	A virtual member.
virtual su2double	GetTotal_OFStressPenalty () const
	A virtual member.
virtual bool	IsElementBased (void) const
	A virtual member.
virtual void	SetTotal_AeroCD (su2double val_aerocd)
	A virtual member.
virtual void	SetTotal_CFEA (su2double val_cfea)
	A virtual member.
virtual void	SetTotal_OFRefGeom (su2double val_ofrefgeom)
	A virtual member.
virtual void	SetTotal_OFRefNode (su2double val_ofrefnode)
	A virtual member.
virtual su2double	GetTotal_NetThrust () const
	A virtual member.
virtual su2double	GetTotal_Power () const
	A virtual member.
virtual su2double	GetTotal_SolidCD () const
	A virtual member.
virtual su2double	GetTotal_ReverseFlow () const
	A virtual member.
virtual su2double	GetTotal_MFR () const
	A virtual member.
virtual su2double	GetTotal_Prop_Eff () const
	A virtual member.
virtual su2double	GetTotal_ByPassProp_Eff () const
	A virtual member.
virtual su2double	GetTotal_Adiab_Eff () const
	A virtual member.
virtual su2double	GetTotal_Poly_Eff () const
	A virtual member.
virtual su2double	GetTotal_IDC () const
	A virtual member.
virtual su2double	GetTotal_IDC_Mach () const
	A virtual member.
virtual su2double	GetTotal_IDR () const
	A virtual member.
virtual su2double	GetTotal_DC60 () const
	A virtual member.
virtual su2double	GetTotal_Buffet_Metric () const
	A virtual member.
virtual unsigned long	GetDonorGlobalIndex (unsigned short val_marker, unsigned long val_vertex) const
	A virtual member.
virtual void	SetDonorGlobalIndex (unsigned short val_marker, unsigned long val_vertex, unsigned long val_index)
	A virtual member.
virtual void	SetCustomBoundaryScalar (unsigned short val_marker, unsigned long val_vertex, vector< passivedouble > val_customBoundaryScalar)
	Set the value of the customized normal scalar values/flux at a specified vertex on a specified marker.
virtual void	SetInlet_TurbVar (unsigned short val_marker, unsigned long val_vertex, unsigned short val_dim, su2double val_turb_var)
	A virtual member.
virtual su2double	GetBuffetSensor (unsigned short val_marker, unsigned long val_vertex) const
	A virtual member.
virtual su2double	GetPsiRho_Inf (void) const
	A virtual member.
virtual su2double	GetPsiE_Inf (void) const
	A virtual member.
virtual su2double	GetPhi_Inf (unsigned short val_dim) const
	A virtual member.
virtual su2double	GetTotal_Sens_Geo () const
	A virtual member.
virtual su2double	GetTotal_Sens_Mach () const
	A virtual member.
virtual su2double	GetTotal_Sens_AoA () const
	A virtual member.
virtual su2double	GetTotal_Sens_Press () const
	Set the total farfield pressure sensitivity coefficient.
virtual su2double	GetTotal_Sens_Temp () const
	Set the total farfield temperature sensitivity coefficient.
virtual su2double	GetTotal_Sens_BPress () const
	Get the total back pressure sensitivity coefficient.
virtual su2double	GetTotal_Sens_Density () const
	A virtual member.
virtual su2double	GetTotal_Sens_ModVel () const
	A virtual member.
virtual su2double	GetNuTilde_Inf (void) const
	A virtual member.
virtual su2double	GetOmega_Inf (void) const
	A virtual member.
virtual su2double	GetIntermittency_Inf () const
	Get value of the Intermittency.
virtual su2double	GetReThetaT_Inf () const
	Get value of the momentum thickness Reynolds number.
virtual su2double	GetTotal_Sens_E (unsigned short iVal) const
	A virtual member.
virtual su2double	GetTotal_Sens_Nu (unsigned short iVal) const
	A virtual member.
virtual su2double	GetTotal_Sens_Rho (unsigned short iVal) const
	A virtual member.
virtual su2double	GetTotal_Sens_Rho_DL (unsigned short iVal) const
	A virtual member.
virtual su2double	GetTotal_Sens_EField (unsigned short iEField) const
	A virtual member.
virtual su2double	GetTotal_Sens_DVFEA (unsigned short iDVFEA) const
	A virtual member.
virtual su2double	GetVal_Young (unsigned short iVal) const
	A virtual member.
virtual su2double	GetVal_Poisson (unsigned short iVal) const
	A virtual member.
virtual su2double	GetVal_Rho (unsigned short iVal) const
	A virtual member.
virtual su2double	GetVal_Rho_DL (unsigned short iVal) const
	A virtual member.
virtual unsigned short	GetnEField (void) const
	A virtual member.
virtual unsigned short	GetnDVFEA (void) const
	A virtual member.
virtual su2double	GetVal_EField (unsigned short iVal) const
	A virtual member.
virtual su2double	GetVal_DVFEA (unsigned short iVal) const
	A virtual member.
virtual su2double	GetCSensitivity (unsigned short val_marker, unsigned long val_vertex) const
	A virtual member.
virtual const su2double *	GetConstants () const
	A virtual member.
virtual void	SetForceCoeff (su2double val_forcecoeff_history)
	A virtual member.
virtual void	SetRelaxCoeff (su2double val_relaxcoeff_history)
	A virtual member.
virtual void	SetFSI_Residual (su2double val_FSI_residual)
	A virtual member.
virtual su2double	GetForceCoeff (void) const
	A virtual member.
virtual su2double	GetRelaxCoeff (void) const
	A virtual member.
virtual su2double	GetFSI_Residual (void) const
	A virtual member.
virtual void	PredictStruct_Displacement (CGeometry *geometry, const CConfig *config)
	A virtual member.
virtual void	ComputeAitken_Coefficient (CGeometry *geometry, const CConfig *config, unsigned long iOuterIter)
	A virtual member.
virtual void	SetAitken_Relaxation (CGeometry *geometry, const CConfig *config)
	A virtual member.
void	BasicLoadRestart (CGeometry *geometry, const CConfig *config, const string &filename, unsigned long skipVars)
	Loads the solution from the restart file.
void	Read_SU2_Restart_ASCII (CGeometry *geometry, const CConfig *config, string val_filename)
	Read a native SU2 restart file in ASCII format.
void	Read_SU2_Restart_Binary (CGeometry *geometry, const CConfig *config, string val_filename)
	Read a native SU2 restart file in binary format.
void	Read_SU2_Restart_Metadata (CGeometry *geometry, CConfig *config, bool adjoint_run, const string &val_filename) const
	Read the metadata from a native SU2 restart file (ASCII or binary).
void	LoadInletProfile (CGeometry **geometry, CSolver ***solver, CConfig *config, int val_iter, unsigned short val_kind_solver, unsigned short val_kind_marker) const
	Load a inlet profile data from file into a particular solver.
virtual void	LoadRestart_FSI (CGeometry *geometry, CConfig *config, int val_iter)
	A virtual member.
virtual unsigned short	Get_iElem_iDe (unsigned long iElem) const
	A virtual member.
virtual void	Set_DV_Val (su2double val_EField, unsigned short i_DV)
	A virtual member.
virtual su2double	Get_DV_Val (unsigned short i_DV) const
	A virtual member.
void	GaussElimination (su2double **A, su2double *rhs, unsigned short nVar)
	Gauss method for solving a linear system.
void	Aeroelastic (CSurfaceMovement *surface_movement, CGeometry *geometry, CConfig *config, unsigned long TimeIter)
	Prepares and solves the aeroelastic equations.
void	SetUpTypicalSectionWingModel (vector< vector< su2double > > &PHI, vector< su2double > &w, CConfig *config)
	Sets up the generalized eigenvectors and eigenvalues needed to solve the aeroelastic equations.
void	SolveTypicalSectionWingModel (CGeometry *geometry, su2double Cl, su2double Cm, CConfig *config, unsigned short val_Marker, vector< su2double > &displacements)
	Solve the typical section wing model.
virtual void	RegisterSolution (CGeometry *geometry_container, CConfig *config)
	A virtual member.
virtual void	RegisterOutput (CGeometry *geometry_container, CConfig *config)
	A virtual member.
virtual void	SetAdjoint_Output (CGeometry *geometry, CConfig *config)
	A virtual member.
virtual void	ExtractAdjoint_Solution (CGeometry *geometry, CConfig *config, bool CrossTerm)
	A virtual member.
virtual 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 void	SetFreeStream_Solution (const CConfig *config)
	A virtual member.
virtual su2double *	GetVecSolDOFs (void)
	A virtual member.
virtual unsigned long	GetnDOFsGlobal (void) const
	A virtual member.
virtual void	InitTurboContainers (CGeometry *geometry, CConfig **config, unsigned short iZone)
	A virtual member.
virtual vector< su2double >	GetTurboPrimitive (unsigned short iBlade, unsigned short iSpan, bool Inlet)
	Get Primal variables for turbo performance computation iteration can be executed by multiple threads.
virtual void	PreprocessAverage (CSolver **solver, CGeometry *geometry, CConfig *config, unsigned short marker_flag)
	virtual member.
virtual void	TurboAverageProcess (CSolver **solver, CGeometry *geometry, CConfig *config, unsigned short marker_flag)
	virtual member.
virtual void	GatherInOutAverageValues (CConfig *config, CGeometry *geometry)
	virtual member.
virtual void	ComputeTurboBladePerformance (CGeometry *geometry, CConfig *config, unsigned short iBlade)
virtual su2double	GetAverageDensity (unsigned short valMarker, unsigned short valSpan) const
	A virtual member.
virtual su2double	GetAverageMassFlowRate (unsigned short valMarker) const
	virtual member
virtual su2double	GetAveragePressure (unsigned short valMarker, unsigned short valSpan) const
	A virtual member.
virtual const su2double *	GetAverageTurboVelocity (unsigned short valMarker, unsigned short valSpan) const
	A virtual member.
virtual su2double	GetAverageNu (unsigned short valMarker, unsigned short valSpan) const
	A virtual member.
virtual su2double	GetAverageKine (unsigned short valMarker, unsigned short valSpan) const
	A virtual member.
virtual su2double	GetAverageOmega (unsigned short valMarker, unsigned short valSpan) const
	A virtual member.
virtual su2double	GetDensityIn (unsigned short inMarkerTP, unsigned short valSpan) const
	A virtual member.
virtual su2double	GetPressureIn (unsigned short inMarkerTP, unsigned short valSpan) const
	A virtual member.
virtual const su2double *	GetTurboVelocityIn (unsigned short inMarkerTP, unsigned short valSpan) const
	A virtual member.
virtual su2double	GetDensityOut (unsigned short inMarkerTP, unsigned short valSpan) const
	A virtual member.
virtual su2double	GetPressureOut (unsigned short inMarkerTP, unsigned short valSpan) const
	A virtual member.
virtual const su2double *	GetTurboVelocityOut (unsigned short inMarkerTP, unsigned short valSpan) const
	A virtual member.
virtual su2double	GetKineIn (unsigned short inMarkerTP, unsigned short valSpan) const
	A virtual member.
virtual su2double	GetOmegaIn (unsigned short inMarkerTP, unsigned short valSpan) const
	A virtual member.
virtual su2double	GetNuIn (unsigned short inMarkerTP, unsigned short valSpan) const
	A virtual member.
virtual su2double	GetKineOut (unsigned short inMarkerTP, unsigned short valSpan) const
	A virtual member.
virtual su2double	GetOmegaOut (unsigned short inMarkerTP, unsigned short valSpan) const
	A virtual member.
virtual su2double	GetNuOut (unsigned short inMarkerTP, unsigned short valSpan) const
	A virtual member.
virtual void	SetDensityIn (su2double value, unsigned short inMarkerTP, unsigned short valSpan)
	A virtual member.
virtual void	SetPressureIn (su2double value, unsigned short inMarkerTP, unsigned short valSpan)
	A virtual member.
virtual void	SetTurboVelocityIn (const su2double *value, unsigned short inMarkerTP, unsigned short valSpan)
	A virtual member.
virtual void	SetDensityOut (su2double value, unsigned short inMarkerTP, unsigned short valSpan)
	A virtual member.
virtual void	SetPressureOut (su2double value, unsigned short inMarkerTP, unsigned short valSpan)
	A virtual member.
virtual void	SetTurboVelocityOut (const su2double *value, unsigned short inMarkerTP, unsigned short valSpan)
	A virtual member.
virtual void	SetKineIn (su2double value, unsigned short inMarkerTP, unsigned short valSpan)
	A virtual member.
virtual void	SetOmegaIn (su2double value, unsigned short inMarkerTP, unsigned short valSpan)
	A virtual member.
virtual void	SetNuIn (su2double value, unsigned short inMarkerTP, unsigned short valSpan)
	A virtual member.
virtual void	SetKineOut (su2double value, unsigned short inMarkerTP, unsigned short valSpan)
	A virtual member.
virtual void	SetOmegaOut (su2double value, unsigned short inMarkerTP, unsigned short valSpan)
	A virtual member.
virtual void	SetNuOut (su2double value, unsigned short inMarkerTP, unsigned short valSpan)
	A virtual member.
virtual void	SetFreeStream_TurboSolution (CConfig *config)
	A virtual member.
virtual void	DeformMesh (CGeometry **geometry, CNumerics **numerics, CConfig *config)
	A virtual member.
virtual void	DeformMesh (CGeometry *geometry, CNumerics **numerics, CConfig *config)
	A virtual member.
virtual void	SetMesh_Stiffness (CNumerics **numerics, CConfig *config)
	A virtual member.
virtual void	ApplyGradientSmoothingVolume (CGeometry *geometry, CNumerics *numerics, const CConfig *config)
	A virtual member.
virtual void	ApplyGradientSmoothingSurface (CGeometry *geometry, CNumerics *numerics, const CConfig *config)
	A virtual member.
virtual void	ApplyGradientSmoothingDV (CGeometry *geometry, CNumerics *numerics, CSurfaceMovement *surface_movement, CVolumetricMovement *grid_movement, CConfig *config, su2double **Gradient)
	All steps required for smoothing the whole system on DV level in an iterative way.
virtual void	RecordTapeAndCalculateOriginalGradient (CGeometry *geometry, CSurfaceMovement *surface_movement, CVolumetricMovement *grid_movement, CConfig *config, su2double **Gradient)
	A virtual member.
virtual void	ReadSensFromGeometry (const CGeometry *geometry)
	A virtual member.
virtual void	WriteSensToGeometry (CGeometry *geometry) const
	A virtual member.
void	SetImplicitPeriodic (bool val_implicit_periodic)
	Routine that sets the flag controlling implicit treatment for periodic BCs.
void	SetRotatePeriodic (bool val_rotate_periodic)
	Routine that sets the flag controlling solution rotation for periodic BCs.
su2activematrix *	GetPeriodicProjections (const CGeometry &geometry, const CConfig &config)
	Storage for the limiters with rotational periodicity: the min and max, over the edges of the periodic matches of each point, of the reconstruction increments (communicated with PERIODIC_LIM_PRIM_1).
su2double *	GetPeriodicProjection (unsigned long iPoint)
	Reconstruction increment bounds for a periodic receive point, nullptr for other points.
const string &	GetSolverName () const
	Retrieve the solver name for output purposes.
vector< string >	GetSolutionFields () const
	Get the solution fields.
void	ComputeVertexTractions (CGeometry *geometry, const CConfig *config)
	Compute the tractions at the vertices.
su2double	GetVertexTractions (unsigned short iMarker, unsigned long iVertex, unsigned short iDim) const
	Set the adjoints of the vertex tractions.
void	RegisterVertexTractions (CGeometry *geometry, const CConfig *config)
	Register the vertex tractions as output.
void	StoreVertexTractionsAdjoint (unsigned short iMarker, unsigned long iVertex, unsigned short iDim, su2double val_adjoint)
	Store the adjoints of the vertex tractions.
void	SetVertexTractionsAdjoint (CGeometry *geometry, const CConfig *config)
	Set the adjoints of the vertex tractions to the AD structure.
virtual su2double	GetMinimum_Volume () const
	Get minimun volume in the mesh.
virtual su2double	GetMaximum_Volume () const
	Get maximum volume in the mesh.
virtual bool	GetHasHybridParallel () const
	Whether the methods of the solver called by multi/single-grid iteration can be executed by multiple threads.
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)

Protected Member Functions
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.
virtual void	SetReferenceValues (const CConfig &config)=0
	Set reference values for pressure, forces, etc., e.g. "AeroCoeffForceRef".
void	Allocate (const CConfig &config)
	Allocate member variables.
void	AllocateTerribleLegacyTemporaryVariables ()
	Allocate small member variables that ideally should not be used.
void	CommunicateInitialState (CGeometry *geometry, const CConfig *config)
	Communicate the initial solver state.
void	HybridParallelInitialization (const CConfig &config, CGeometry &geometry)
	Initialize thread parallel variables.
void	PushSolutionBackInTime (unsigned long TimeIter, bool restart, bool rans, CSolver ***solver_container, CGeometry **geometry, CConfig *config)
	Move solution to previous time levels (for restarts).
su2double	EvaluateCommonObjFunc (const CConfig &config) const
	Evaluate common part of objective function to all solvers.
void	EdgeFluxResidual (const CGeometry *geometry, const CSolver *const *solvers, CConfig *config)
	Method to compute convective and viscous residual contribution using vectorized numerics.
void	SumEdgeFluxes (const CGeometry *geometry)
	Sum the edge fluxes for each cell to populate the residual vector, only used on coarse grids.
void	FinalizeResidualComputation (const CGeometry *geometry, bool pausePreacc, unsigned long localCounter, CConfig *config)
	Sums edge fluxes (if required) and computes the global error counter.
void	ComputeAxisymmetricAuxGradients (CGeometry *geometry, const CConfig *config)
	Computes and sets the required auxilliary vars (and gradients) for axisymmetric flow.
virtual void	InstantiateEdgeNumerics (const CSolver *const *solvers, const CConfig *config)
	Instantiate a SIMD numerics object.
virtual CNumerics::ResidualType	Viscous_Residual (unsigned long iEdge, CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config)
	Compute the viscous contribution for a particular edge.
CNumerics::ResidualType	Viscous_Residual_impl (unsigned long iEdge, CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config)
void	UpdateJacobian (unsigned long iEdge, unsigned long iPoint, unsigned long jPoint, const CNumerics::ResidualType<> &conv, const CNumerics::ResidualType<> &visc)
	Update the Jacobian for one edge with the fused convective and viscous contributions.
virtual void	ComputeUnderRelaxationFactor (const CConfig *config)
	Compute a suitable under-relaxation parameter to limit the change in the solution variables over a nonlinear iteration for stability.
void	LoadRestart_impl (CGeometry **geometry, CSolver ***solver, CConfig *config, int iter, bool update_geo, su2double *RestartSolution=nullptr, unsigned short nVar_Restart=0)
	General implementation to load a flow solution from a restart file.
template<class SoundSpeedFunc , class LambdaViscFunc >
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.
template<class SoundSpeedFunc >
void	SetMax_Eigenvalue_impl (const SoundSpeedFunc &soundSpeed, CGeometry *geometry, const CConfig *config)
	Compute the max eigenvalue, gemeric implementation.
template<class SensVarFunc >
void	SetCentered_Dissipation_Sensor_impl (const SensVarFunc &sensVar, CGeometry *geometry, const CConfig *config)
	Compute the dissipation sensor for centered schemes.
template<ENUM_TIME_INT IntegrationType, class ResidualPrecond >
void	Explicit_Iteration_impl (ResidualPrecond &preconditioner, CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iRKStep)
	Generic implementation of explicit iterations with a preconditioner.
template<ENUM_TIME_INT IntegrationType>
void	Explicit_Iteration (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iRKStep)
	Generic implementation of explicit iterations without preconditioner.
template<class DiagonalPrecond >
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.
virtual void	Viscous_Residual (CGeometry *geometry, CSolver **solver_container, CNumerics **numerics_container, CConfig *config, unsigned short iMesh, unsigned short iRKStep)
	A virtual member.
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
template<class... Ts>
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
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 = 0.0
	Mach number at the infinity.
su2double	Density_Inf = 0.0
	Density at the infinity.
su2double	Energy_Inf = 0.0
	Energy at the infinity.
su2double	Temperature_Inf = 0.0
	Temperature at the infinity.
su2double	Enthalpy_Inf = 0.0
	Enthalpy at the infinity.
su2double	Pressure_Inf = 0.0
	Pressure at the infinity.
su2double *	Velocity_Inf = nullptr
	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 = 0.0
	Time-step for TIME_STEPPING time marching strategy.
su2double	Global_Delta_UnstTimeND = 0.0
	Unsteady time step for the dual time strategy.
unsigned long	ErrorCounter = 0
	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 = 1.0
	Reference force for aerodynamic coefficients.
su2double	DynamicPressureRef = 1.0
	Reference dynamic pressure.
su2double	Total_CpDiff = 0.0
	Total Equivalent Area coefficient for all the boundaries.
su2double	Total_HeatFluxDiff = 0.0
	Total Equivalent Area coefficient for all the boundaries.
su2double	Total_CEquivArea = 0.0
	Total Equivalent Area coefficient for all the boundaries.
su2double	Total_MassFlowRate = 0.0
	Total Mass Flow Rate on monitored boundaries.
su2double	Total_CNearFieldOF = 0.0
	Total Near-Field Pressure coefficient for all the boundaries.
su2double	Total_Heat = 0.0
	Total heat load for all the boundaries.
su2double	Total_MaxHeat = 0.0
	Maximum heat flux on all boundaries.
su2double	AllBound_CNearFieldOF_Inv = 0.0
	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 = 0.0
	Heat load (viscous contribution) for all the boundaries.
su2double	AllBound_MaxHF_Visc = 0.0
	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 = nullptr
	Object for edge flux computation.
VariableType *	nodes = nullptr
	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
static constexpr size_t	MAXNDIM = 3
	Max number of space dimensions, used in some static arrays.
static constexpr size_t	MAXNVAR = VariableType::MAXNVAR
	Max number of variables, for static arrays.
static constexpr size_t	OMP_MAX_SIZE = 512
	Max chunk size for light point loops.
static constexpr size_t	OMP_MIN_SIZE = 32
	Min chunk size for edge loops (max is color group size).
static constexpr bool	ReducerStrategy = false

Additional Inherited Members
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 CSolver
enum	: size_t { OMP_MIN_SIZE = 32 }

Constructor & Destructor Documentation

CFVMFlowSolverBase()

template<class VariableType , ENUM_REGIME FlowRegime>

CFVMFlowSolverBase< VariableType, FlowRegime >::CFVMFlowSolverBase ( const CGeometry &  geometry, const CConfig &  config  )

inlineprotected

Protected constructor, this class is not directly instantiable.

~CFVMFlowSolverBase()

template<class V , ENUM_REGIME R>

CFVMFlowSolverBase< V, R >::~CFVMFlowSolverBase ( )

protected

Destructor.

Member Function Documentation

Allocate()

template<class V , ENUM_REGIME R>

void CFVMFlowSolverBase< V, R >::Allocate ( const CConfig &  config )

protected

Allocate member variables.

AllocateTerribleLegacyTemporaryVariables()

template<class V , ENUM_REGIME R>

void CFVMFlowSolverBase< V, R >::AllocateTerribleLegacyTemporaryVariables ( )

protected

Allocate small member variables that ideally should not be used.

BC_Custom()

template<class V , ENUM_REGIME R>

void CFVMFlowSolverBase< V, R >::BC_Custom ( CGeometry *  geometry, CSolver **  solver_container, CNumerics *  conv_numerics, CNumerics *  visc_numerics, CConfig *  config, unsigned short  val_marker  )

finalvirtual

Impose a custom or verification boundary condition.

Parameters

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

Reimplemented from CSolver.

BC_Euler_Wall()

template<class VariableType , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< VariableType, FlowRegime >::BC_Euler_Wall ( CGeometry *  geometry, CSolver **  solver_container, CNumerics *  conv_numerics, CNumerics *  visc_numerics, CConfig *  config, unsigned short  val_marker  )

inlinefinalvirtual

Impose via the residual the Euler wall boundary condition.

Author

T. Kattmann

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_Fluid_Interface()

template<class V , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< V, FlowRegime >::BC_Fluid_Interface ( CGeometry *  geometry, CSolver **  solver_container, CNumerics *  conv_numerics, CNumerics *  visc_numerics, CConfig *  config  )

finalvirtual

Impose the interface state across sliding meshes.

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.

Reimplemented from CSolver.

BC_Periodic()

template<class V , ENUM_REGIME R>

void CFVMFlowSolverBase< V, R >::BC_Periodic ( CGeometry *  geometry, CSolver **  solver_container, CNumerics *  numerics, CConfig *  config  )

finalvirtual

Impose a periodic boundary condition by summing contributions from the complete control volume.

Parameters

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

Reimplemented from CSolver.

BC_Sym_Plane()

template<class V , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< V, FlowRegime >::BC_Sym_Plane ( CGeometry *  geometry, CSolver **  solver_container, CNumerics *  conv_numerics, CNumerics *  visc_numerics, CConfig *  config, unsigned short  val_marker  )

overridevirtual

Impose the symmetry boundary condition using the residual.

Author

T. Kattmann

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.

Reimplemented in CNEMOEulerSolver.

Buffet_Monitoring()

template<class VariableType , ENUM_REGIME FlowRegime>

virtual void CFVMFlowSolverBase< VariableType, FlowRegime >::Buffet_Monitoring ( const CGeometry *  geometry, const CConfig *  config  )

inlinevirtual

Compute the buffet sensor.

Parameters

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

Reimplemented in CNSSolver.

CommunicateInitialState()

template<class V , ENUM_REGIME R>

void CFVMFlowSolverBase< V, R >::CommunicateInitialState ( CGeometry *  geometry, const CConfig *  config  )

protected

Communicate the initial solver state.

CompleteImplicitIteration()

template<class V , ENUM_REGIME R>

void CFVMFlowSolverBase< V, R >::CompleteImplicitIteration ( CGeometry *  geometry, CSolver **  , CConfig *  config  )

finalvirtual

Complete an implicit iteration.

Parameters

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

Reimplemented from CSolver.

ComputeAxisymmetricAuxGradients()

template<class V , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< V, FlowRegime >::ComputeAxisymmetricAuxGradients ( CGeometry *  geometry, const CConfig *  config  )

protected

Computes and sets the required auxilliary vars (and gradients) for axisymmetric flow.

ComputeUnderRelaxationFactor()

template<class VariableType , ENUM_REGIME FlowRegime>

virtual void CFVMFlowSolverBase< VariableType, FlowRegime >::ComputeUnderRelaxationFactor ( const CConfig *  config )

inlineprotectedvirtual

Compute a suitable under-relaxation parameter to limit the change in the solution variables over a nonlinear iteration for stability.

Reimplemented in CEulerSolver, and CNEMOEulerSolver.

ComputeVerificationError()

template<class V , ENUM_REGIME R>

void CFVMFlowSolverBase< V, R >::ComputeVerificationError ( CGeometry *  geometry, CConfig *  config  )

finalvirtual

Compute the global error measures (L2, Linf) for verification cases.

Parameters

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

Reimplemented from CSolver.

ComputeVorticityAndStrainMag()

template<class V , ENUM_REGIME R>

void CFVMFlowSolverBase< V, R >::ComputeVorticityAndStrainMag ( const CConfig &  config, const CGeometry *  geometry, unsigned short  iMesh  )

protected

Evaluate the vorticity and strain rate magnitude.

EdgeFluxResidual()

template<class V , ENUM_REGIME R>

void CFVMFlowSolverBase< V, R >::EdgeFluxResidual ( const CGeometry *  geometry, const CSolver *const *  solvers, CConfig *  config  )

protected

Method to compute convective and viscous residual contribution using vectorized numerics.

EvaluateCommonObjFunc()

template<class V , ENUM_REGIME R>

su2double CFVMFlowSolverBase< V, R >::EvaluateCommonObjFunc ( const CConfig &  config ) const

protected

Evaluate common part of objective function to all solvers.

Explicit_Iteration()

template<class VariableType , ENUM_REGIME FlowRegime>

template<ENUM_TIME_INT IntegrationType>

void CFVMFlowSolverBase< VariableType, FlowRegime >::Explicit_Iteration ( CGeometry *  geometry, CSolver **  solver_container, CConfig *  config, unsigned short  iRKStep  )

inlineprotected

Generic implementation of explicit iterations without preconditioner.

Explicit_Iteration_impl()

template<class VariableType , ENUM_REGIME FlowRegime>

template<ENUM_TIME_INT IntegrationType, class ResidualPrecond >

void CFVMFlowSolverBase< VariableType, FlowRegime >::Explicit_Iteration_impl ( ResidualPrecond &  preconditioner, CGeometry *  geometry, CSolver **  solver_container, CConfig *  config, unsigned short  iRKStep  )

inlineprotected

Generic implementation of explicit iterations with a preconditioner.

Note

The preconditioner is a functor implementing the methods:

• compute(config, iPoint): Should prepare the preconditioner for iPoint.
• apply(iVar, residual[], resTruncError[]): Apply it to compute the iVar update. See Explicit_Iteration for the general form of the preconditioner.

FinalizeResidualComputation()

template<class VariableType , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< VariableType, FlowRegime >::FinalizeResidualComputation ( const CGeometry *  geometry, bool  pausePreacc, unsigned long  localCounter, CConfig *  config  )

inlineprotected

Sums edge fluxes (if required) and computes the global error counter.

Parameters

[in]	pausePreacc	- Whether preaccumulation was paused durin.
[in]	localCounter	- Thread-local error counter.
[in,out]	config	- Used to set the global error counter.

Friction_Forces()

template<class V , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< V, FlowRegime >::Friction_Forces ( const CGeometry *  geometry, const CConfig *  config  )

finalvirtual

Compute the viscous forces and all the addimensional coefficients.

Parameters

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

Reimplemented from CSolver.

GetAeroCoeffsReferenceForce()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAeroCoeffsReferenceForce ( ) const

inlinefinalvirtual

Get the reference force used to compute CL, CD, etc.

Reimplemented from CSolver.

GetAllBound_CD_Inv()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CD_Inv ( ) const

inlinefinalvirtual

Get the inviscid contribution to the drag coefficient.

Returns

Value of the drag coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CD_Mnt()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CD_Mnt ( ) const

inlinefinalvirtual

Get the inviscid contribution to the drag coefficient.

Returns

Value of the drag coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CD_Visc()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CD_Visc ( ) const

inlinefinalvirtual

Get the inviscid contribution to the drag coefficient.

Returns

Value of the drag coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CEff_Inv()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CEff_Inv ( ) const

inlinefinalvirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CEff_Mnt()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CEff_Mnt ( ) const

inlinefinalvirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CEff_Visc()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CEff_Visc ( ) const

inlinefinalvirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CFx_Inv()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CFx_Inv ( ) const

inlinefinalvirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CFx_Mnt()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CFx_Mnt ( ) const

inlinefinalvirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CFx_Visc()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CFx_Visc ( ) const

inlinefinalvirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CFy_Inv()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CFy_Inv ( ) const

inlinefinalvirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CFy_Mnt()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CFy_Mnt ( ) const

inlinefinalvirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CFy_Visc()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CFy_Visc ( ) const

inlinefinalvirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CFz_Inv()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CFz_Inv ( ) const

inlinefinalvirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CFz_Mnt()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CFz_Mnt ( ) const

inlinefinalvirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CFz_Visc()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CFz_Visc ( ) const

inlinefinalvirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CL_Inv()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CL_Inv ( ) const

inlinefinalvirtual

Get the inviscid contribution to the lift coefficient.

Returns

Value of the lift coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CL_Mnt()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CL_Mnt ( ) const

inlinefinalvirtual

Get the inviscid contribution to the lift coefficient.

Returns

Value of the lift coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CL_Visc()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CL_Visc ( ) const

inlinefinalvirtual

Get the inviscid contribution to the lift coefficient.

Returns

Value of the lift coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CMx_Inv()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CMx_Inv ( ) const

inlinefinalvirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CMx_Mnt()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CMx_Mnt ( ) const

inlinefinalvirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CMx_Visc()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CMx_Visc ( ) const

inlinefinalvirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CMy_Inv()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CMy_Inv ( ) const

inlinefinalvirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CMy_Mnt()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CMy_Mnt ( ) const

inlinefinalvirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CMy_Visc()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CMy_Visc ( ) const

inlinefinalvirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CMz_Inv()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CMz_Inv ( ) const

inlinefinalvirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CMz_Mnt()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CMz_Mnt ( ) const

inlinefinalvirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CMz_Visc()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CMz_Visc ( ) const

inlinefinalvirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CoPx_Inv()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CoPx_Inv ( ) const

inlinefinalvirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CoPx_Mnt()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CoPx_Mnt ( ) const

inlinefinalvirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CoPx_Visc()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CoPx_Visc ( ) const

inlinefinalvirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CoPy_Inv()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CoPy_Inv ( ) const

inlinefinalvirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CoPy_Mnt()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CoPy_Mnt ( ) const

inlinefinalvirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CoPy_Visc()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CoPy_Visc ( ) const

inlinefinalvirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CoPz_Inv()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CoPz_Inv ( ) const

inlinefinalvirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CoPz_Mnt()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CoPz_Mnt ( ) const

inlinefinalvirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CoPz_Visc()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CoPz_Visc ( ) const

inlinefinalvirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CSF_Inv()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CSF_Inv ( ) const

inlinefinalvirtual

Get the inviscid contribution to the sideforce coefficient.

Returns

Value of the sideforce coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CSF_Mnt()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CSF_Mnt ( ) const

inlinefinalvirtual

Get the inviscid contribution to the sideforce coefficient.

Returns

Value of the sideforce coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CSF_Visc()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetAllBound_CSF_Visc ( ) const

inlinefinalvirtual

Get the inviscid contribution to the sideforce coefficient.

Returns

Value of the sideforce coefficient (inviscid contribution).

Reimplemented from CSolver.

GetBaseClassPointerToNodes()

template<class VariableType , ENUM_REGIME FlowRegime>

CVariable * CFVMFlowSolverBase< VariableType, FlowRegime >::GetBaseClassPointerToNodes ( )

inlinefinalprotectedvirtual

Return nodes to allow CSolver::base_nodes to be set.

Implements CSolver.

GetCD_Inv()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetCD_Inv ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional drag coefficient (inviscid contribution).

Parameters

val_marker

Surface where the coeficient is going to be computed.

Returns

Value of the drag coefficient (inviscid contribution) on the surface val_marker.

Reimplemented from CSolver.

GetCD_Visc()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetCD_Visc ( unsigned short  val_marker ) const

inlinefinalvirtual

Get the non dimensional drag coefficient (viscous contribution).

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the drag coefficient (viscous contribution) on the surface val_marker.

Reimplemented from CSolver.

GetCEff_Inv()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetCEff_Inv ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional efficiency coefficient (inviscid contribution).

Parameters

val_marker

Surface where the coeficient is going to be computed.

Returns

Value of the efficiency coefficient (inviscid contribution) on the surface val_marker.

Reimplemented from CSolver.

GetCharacPrimVar()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double * CFVMFlowSolverBase< VariableType, FlowRegime >::GetCharacPrimVar ( unsigned short  val_marker, unsigned long  val_vertex  )

inlinefinalvirtual

Value of the characteristic variables at the boundaries.

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 pressure coefficient.

Reimplemented from CSolver.

GetCL_Inv()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetCL_Inv ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional lift coefficient (inviscid contribution).

Parameters

val_marker

Surface where the coefficient is going to be computed.

Returns

Value of the lift coefficient (inviscid contribution) on the surface val_marker.

Reimplemented from CSolver.

GetCL_Visc()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetCL_Visc ( unsigned short  val_marker ) const

inlinefinalvirtual

Get the non dimensional lift coefficient (viscous contribution).

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the lift coefficient (viscous contribution) on the surface val_marker.

Reimplemented from CSolver.

GetConjugateHeatVariable()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetConjugateHeatVariable ( unsigned short  val_marker, unsigned long  val_vertex, unsigned short  pos_var  ) const

inlinefinalvirtual

Set the conjugate heat variables.

Parameters

[in]	val_marker	- marker index
[in]	val_vertex	- vertex index
[in]	pos_var	- variable position (in vector of all conjugate heat variables)

Reimplemented from CSolver.

GetCPressure()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetCPressure ( unsigned short  val_marker, unsigned long  val_vertex  ) const

inlinefinalvirtual

Provide the Pressure coefficient.

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 pressure coefficient.

Reimplemented from CSolver.

GetCPressureTarget()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetCPressureTarget ( unsigned short  val_marker, unsigned long  val_vertex  ) const

inlinefinalvirtual

Provide the Target Pressure coefficient.

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 pressure coefficient.

Reimplemented from CSolver.

GetCSF_Inv()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetCSF_Inv ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional sideforce coefficient (inviscid contribution).

Parameters

val_marker

Surface where the coeficient is going to be computed.

Returns

Value of the sideforce coefficient (inviscid contribution) on the surface val_marker.

Reimplemented from CSolver.

GetCSF_Visc()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetCSF_Visc ( unsigned short  val_marker ) const

inlinefinalvirtual

Get the non dimensional sideforce coefficient (viscous contribution).

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the sideforce coefficient (viscous contribution) on the surface val_marker.

Reimplemented from CSolver.

GetCSkinFriction()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetCSkinFriction ( unsigned short  val_marker, unsigned long  val_vertex, unsigned short  val_dim  ) const

inlinefinalvirtual

Get the skin friction coefficient.

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 skin friction coefficient.

Reimplemented from CSolver.

GetDensity_Energy_Inf()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetDensity_Energy_Inf ( void  ) const

inlinefinalvirtual

Compute the density multiply by energy at the infinity.

Returns

Value of the density multiply by energy at the infinity.

Reimplemented from CSolver.

GetDensity_Inf()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetDensity_Inf ( void  ) const

inlinefinalvirtual

Compute the density at the infinity.

Returns

Value of the density at the infinity.

Reimplemented from CSolver.

GetEddyViscWall()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetEddyViscWall ( unsigned short  val_marker, unsigned long  val_vertex  ) const

inlinefinalvirtual

Get the eddy viscosity at the wall (wall functions).

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 eddy viscosity.

Reimplemented from CSolver.

GetEdgeMassFluxes()

template<class VariableType , ENUM_REGIME FlowRegime>

const su2activevector * CFVMFlowSolverBase< VariableType, FlowRegime >::GetEdgeMassFluxes ( ) const

inlinefinalvirtual

Get the mass fluxes across the edges (computed and stored during the discretization of convective fluxes).

Reimplemented from CSolver.

GetHeatFlux()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetHeatFlux ( unsigned short  val_marker, unsigned long  val_vertex  ) const

inlinefinalvirtual

Get the heat flux.

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 heat transfer coefficient.

Reimplemented from CSolver.

GetHeatFluxTarget()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetHeatFluxTarget ( unsigned short  val_marker, unsigned long  val_vertex  ) const

inlinefinalvirtual

Get the skin friction coefficient.

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 heat transfer coefficient.

Reimplemented from CSolver.

GetInletAtVertex()

template<class V , ENUM_REGIME R>

su2double CFVMFlowSolverBase< V, R >::GetInletAtVertex ( unsigned short  iMarker, unsigned long  iVertex, const CGeometry *  geometry, su2double *  val_inlet  ) const

finalvirtual

Get the set of values imposed at an inlet.

Parameters

[in]	iMarker	- Index of the surface marker.
[in]	iVertex	- Vertex of the marker iMarker where the inlet is being set.
[in]	geometry	- Geometrical definition of the problem.
[in,out]	val_inlet	- vector returning the inlet values for the current vertex.

Returns

Value of the face area at the vertex.

Reimplemented from CSolver.

GetInletFlowDir()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetInletFlowDir ( unsigned short  val_marker, unsigned long  val_vertex, unsigned short  val_dim  ) const

inlinefinalvirtual

A component of the unit vector representing the flow direction at an inlet boundary.

Parameters

[in]	val_marker	- Surface marker where the flow direction is evaluated
[in]	val_vertex	- Vertex of the marker val_marker where the flow direction is evaluated
[in]	val_dim	- The component of the flow direction unit vector to be evaluated

Returns

Component of a unit vector representing the flow direction.

Reimplemented from CSolver.

GetInletPtotal()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetInletPtotal ( unsigned short  val_marker, unsigned long  val_vertex  ) const

inlinefinalvirtual

Value of the total pressure at an inlet boundary.

Parameters

[in]	val_marker	- Surface marker where the total pressure is evaluated.
[in]	val_vertex	- Vertex of the marker val_marker where the total pressure is evaluated.

Returns

Value of the total pressure

Reimplemented from CSolver.

GetInletTtotal()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetInletTtotal ( unsigned short  val_marker, unsigned long  val_vertex  ) const

inlinefinalvirtual

Value of the total temperature at an inlet boundary.

Parameters

[in]	val_marker	- Surface marker where the total temperature is evaluated.
[in]	val_vertex	- Vertex of the marker val_marker where the total temperature is evaluated.

Returns

Value of the total temperature

Reimplemented from CSolver.

GetModVelocity_Inf()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetModVelocity_Inf ( void  ) const

inlinefinalvirtual

Compute 2-norm of the velocity at the infinity.

Returns

Value of the 2-norm of the velocity at the infinity.

Reimplemented from CSolver.

GetnSlidingStates()

template<class VariableType , ENUM_REGIME FlowRegime>

int CFVMFlowSolverBase< VariableType, FlowRegime >::GetnSlidingStates ( unsigned short  val_marker, unsigned long  val_vertex  ) const

inlinefinalvirtual

Get the number of outer state for fluid interface nodes.

Parameters

[in]	val_marker	- marker index
[in]	val_vertex	- vertex index

Reimplemented from CSolver.

GetOmega_Max()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetOmega_Max ( void  ) const

inlinefinalvirtual

Get the max Omega.

Returns

Value of the max Omega.

Reimplemented from CSolver.

GetPressure_Inf()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetPressure_Inf ( void  ) const

inlinefinalvirtual

Compute the pressure at the infinity.

Returns

Value of the pressure at the infinity.

Reimplemented from CSolver.

GetReferenceDynamicPressure()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetReferenceDynamicPressure ( ) const

inlinefinalvirtual

Get the reference dynamic pressure, for Cp, Cf, etc.

Reimplemented from CSolver.

GetSlidingState()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSlidingState ( unsigned short  val_marker, unsigned long  val_vertex, unsigned short  val_state, unsigned long  donor_index  ) const

inlinefinalvirtual

Get the outer state for fluid interface nodes.

Parameters

[in]	val_marker	- marker index
[in]	val_vertex	- vertex index
[in]	val_state	- requested state component
[in]	donor_index-	index of the donor node to get

Reimplemented from CSolver.

GetStrainMag_Max()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetStrainMag_Max ( void  ) const

inlinefinalvirtual

Get the max Strain rate magnitude.

Returns

Value of the max Strain rate magnitude.

Reimplemented from CSolver.

GetSurface_CD()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CD ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional drag coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the drag coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CD_Inv()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CD_Inv ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional drag coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the drag coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CD_Mnt()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CD_Mnt ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional drag coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the drag coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CD_Visc()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CD_Visc ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional drag coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the drag coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CEff()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CEff ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional side-force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the side-force coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CEff_Inv()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CEff_Inv ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional side-force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the side-force coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CEff_Mnt()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CEff_Mnt ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional side-force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the side-force coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CEff_Visc()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CEff_Visc ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional side-force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the side-force coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CFx()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CFx ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional x force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the x force coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CFx_Inv()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CFx_Inv ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional x force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the x force coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CFx_Mnt()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CFx_Mnt ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional x force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the x force coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CFx_Visc()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CFx_Visc ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional x force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the x force coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CFy()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CFy ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional y force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the y force coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CFy_Inv()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CFy_Inv ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional y force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the y force coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CFy_Mnt()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CFy_Mnt ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional y force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the y force coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CFy_Visc()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CFy_Visc ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional y force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the y force coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CFz()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CFz ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional z force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the z force coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CFz_Inv()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CFz_Inv ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional z force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the z force coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CFz_Mnt()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CFz_Mnt ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional z force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the z force coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CFz_Visc()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CFz_Visc ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional z force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the z force coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CL()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CL ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional lift coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the lift coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CL_Inv()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CL_Inv ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional lift coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the lift coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CL_Mnt()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CL_Mnt ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional lift coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the lift coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CL_Visc()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CL_Visc ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional lift coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the lift coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CMx()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CMx ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional x moment coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the x moment coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CMx_Inv()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CMx_Inv ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional x moment coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the x moment coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CMx_Mnt()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CMx_Mnt ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional x moment coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the x moment coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CMx_Visc()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CMx_Visc ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional x moment coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the x moment coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CMy()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CMy ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional y moment coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the y moment coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CMy_Inv()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CMy_Inv ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional y moment coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the y moment coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CMy_Mnt()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CMy_Mnt ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional y moment coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the y moment coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CMy_Visc()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CMy_Visc ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional y moment coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the y moment coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CMz()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CMz ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional z moment coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the z moment coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CMz_Inv()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CMz_Inv ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional z moment coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the z moment coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CMz_Mnt()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CMz_Mnt ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional z moment coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the z moment coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CMz_Visc()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CMz_Visc ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional z moment coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the z moment coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CSF()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CSF ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional side-force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the side-force coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CSF_Inv()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CSF_Inv ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional side-force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the side-force coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CSF_Mnt()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CSF_Mnt ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional side-force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the side-force coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CSF_Visc()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_CSF_Visc ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the non dimensional side-force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the side-force coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_HF_Visc()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_HF_Visc ( unsigned short  val_marker ) const

inlinefinalvirtual

Get the total heat flux.

Parameters

[in]

val_marker

- Surface marker where the heat flux is computed.

Returns

Value of the integrated heat flux (viscous contribution) on the surface val_marker.

Reimplemented from CSolver.

GetSurface_MaxHF_Visc()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetSurface_MaxHF_Visc ( unsigned short  val_marker ) const

inlinefinalvirtual

Get the maximum (per surface) heat flux.

Parameters

[in]

val_marker

- Surface marker where the heat flux is computed.

Returns

Value of the maximum heat flux (viscous contribution) on the surface val_marker.

Reimplemented from CSolver.

GetTemperature_Inf()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetTemperature_Inf ( void  ) const

inline

Get the temperature value at infinity.

Returns

Value of the temperature at infinity.

GetTke_Inf()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetTke_Inf ( void  ) const

inlinefinalvirtual

Get the turbulent kinetic energy at the infinity.

Returns

Value of the turbulent kinetic energy at the infinity.

Reimplemented from CSolver.

GetTotal_CD()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetTotal_CD ( ) const

inlinefinalvirtual

Provide the total (inviscid + viscous) non dimensional drag coefficient.

Returns

Value of the drag coefficient (inviscid + viscous contribution).

Reimplemented from CSolver.

GetTotal_CEff()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetTotal_CEff ( ) const

inlinefinalvirtual

Provide the total (inviscid + viscous) non dimensional efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid + viscous contribution).

Reimplemented from CSolver.

GetTotal_CEquivArea()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetTotal_CEquivArea ( ) const

inlinefinalvirtual

Provide the total (inviscid + viscous) non dimensional Equivalent Area coefficient.

Returns

Value of the Equivalent Area coefficient (inviscid + viscous contribution).

Reimplemented from CSolver.

GetTotal_CFx()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetTotal_CFx ( ) const

inlinefinalvirtual

Provide the total (inviscid + viscous) non dimensional x force coefficient.

Returns

Value of the force x coefficient (inviscid + viscous contribution).

Reimplemented from CSolver.

GetTotal_CFy()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetTotal_CFy ( ) const

inlinefinalvirtual

Provide the total (inviscid + viscous) non dimensional y force coefficient.

Returns

Value of the force y coefficient (inviscid + viscous contribution).

Reimplemented from CSolver.

GetTotal_CFz()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetTotal_CFz ( ) const

inlinefinalvirtual

Provide the total (inviscid + viscous) non dimensional z force coefficient.

Returns

Value of the force z coefficient (inviscid + viscous contribution).

Reimplemented from CSolver.

GetTotal_CL()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetTotal_CL ( ) const

inlinefinalvirtual

Provide the total (inviscid + viscous) non dimensional lift coefficient.

Returns

Value of the lift coefficient (inviscid + viscous contribution).

Reimplemented from CSolver.

GetTotal_CMerit()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetTotal_CMerit ( ) const

inlinefinalvirtual

Provide the total (inviscid + viscous) non dimensional rotor Figure of Merit.

Returns

Value of the rotor efficiency coefficient (inviscid + viscous contribution).

Reimplemented from CSolver.

GetTotal_CMx()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetTotal_CMx ( ) const

inlinefinalvirtual

Provide the total (inviscid + viscous) non dimensional x moment coefficient.

Returns

Value of the moment x coefficient (inviscid + viscous contribution).

Reimplemented from CSolver.

GetTotal_CMy()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetTotal_CMy ( ) const

inlinefinalvirtual

Provide the total (inviscid + viscous) non dimensional y moment coefficient.

Returns

Value of the moment y coefficient (inviscid + viscous contribution).

Reimplemented from CSolver.

GetTotal_CMz()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetTotal_CMz ( ) const

inlinefinalvirtual

Provide the total (inviscid + viscous) non dimensional z moment coefficient.

Returns

Value of the moment z coefficient (inviscid + viscous contribution).

Reimplemented from CSolver.

GetTotal_CoPx()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetTotal_CoPx ( ) const

inlinefinalvirtual

Provide the total (inviscid + viscous) non dimensional x moment coefficient.

Returns

Value of the moment x coefficient (inviscid + viscous contribution).

Reimplemented from CSolver.

GetTotal_CoPy()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetTotal_CoPy ( ) const

inlinefinalvirtual

Provide the total (inviscid + viscous) non dimensional y moment coefficient.

Returns

Value of the moment y coefficient (inviscid + viscous contribution).

Reimplemented from CSolver.

GetTotal_CoPz()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetTotal_CoPz ( ) const

inlinefinalvirtual

Provide the total (inviscid + viscous) non dimensional z moment coefficient.

Returns

Value of the moment z coefficient (inviscid + viscous contribution).

Reimplemented from CSolver.

GetTotal_CpDiff()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetTotal_CpDiff ( ) const

inlinefinalvirtual

Provide the total (inviscid + viscous) non dimensional Equivalent Area coefficient.

Returns

Value of the Equivalent Area coefficient (inviscid + viscous contribution).

Reimplemented from CSolver.

GetTotal_CQ()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetTotal_CQ ( ) const

inlinefinalvirtual

Provide the total (inviscid + viscous) non dimensional torque coefficient.

Returns

Value of the rotor efficiency coefficient (inviscid + viscous contribution).

Reimplemented from CSolver.

GetTotal_CSF()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetTotal_CSF ( ) const

inlinefinalvirtual

Provide the total (inviscid + viscous) non dimensional sideforce coefficient.

Returns

Value of the sideforce coefficient (inviscid + viscous contribution).

Reimplemented from CSolver.

GetTotal_CT()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetTotal_CT ( ) const

inlinefinalvirtual

Provide the total (inviscid + viscous) non dimensional thrust coefficient.

Returns

Value of the rotor efficiency coefficient (inviscid + viscous contribution).

Reimplemented from CSolver.

GetTotal_HeatFlux()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetTotal_HeatFlux ( ) const

inlinefinalvirtual

Provide the total heat load.

Returns

Value of the heat load (viscous contribution).

Reimplemented from CSolver.

GetTotal_HeatFluxDiff()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetTotal_HeatFluxDiff ( ) const

inlinefinalvirtual

Provide the total (inviscid + viscous) non dimensional Equivalent Area coefficient.

Returns

Value of the Equivalent Area coefficient (inviscid + viscous contribution).

Reimplemented from CSolver.

GetTotal_MaxHeatFlux()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetTotal_MaxHeatFlux ( ) const

inlinefinalvirtual

Provide the total heat load.

Returns

Value of the heat load (viscous contribution).

Reimplemented from CSolver.

GetUTau()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetUTau ( unsigned short  val_marker, unsigned long  val_vertex  ) const

inlinefinalvirtual

Get the u_tau .

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 u_tau.

Reimplemented from CSolver.

GetVelocity_Inf() [1/2]

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetVelocity_Inf ( unsigned short  val_dim ) const

inlinefinalvirtual

Get the velocity at the infinity.

Parameters

[in]

val_dim

- Index of the velocity vector.

Returns

Value of the velocity at the infinity.

Reimplemented from CSolver.

GetVelocity_Inf() [2/2]

template<class VariableType , ENUM_REGIME FlowRegime>

su2double * CFVMFlowSolverBase< VariableType, FlowRegime >::GetVelocity_Inf ( void  )

inlinefinalvirtual

Get the velocity at the infinity.

Returns

Value of the velocity at the infinity.

Reimplemented from CSolver.

GetViscosity_Inf()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetViscosity_Inf ( void  ) const

inlinefinalvirtual

Compute the viscosity at the infinity.

Returns

Value of the viscosity at the infinity.

Reimplemented from CSolver.

GetWallShearStress()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetWallShearStress ( unsigned short  val_marker, unsigned long  val_vertex  ) const

inlinefinalvirtual

Get the wall shear stress.

Parameters

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

Returns

Value of the wall shear stress.

Reimplemented from CSolver.

GetYPlus()

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::GetYPlus ( unsigned short  val_marker, unsigned long  val_vertex  ) const

inlinefinalvirtual

Get the y plus.

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 y plus.

Reimplemented from CSolver.

HybridParallelInitialization()

template<class V , ENUM_REGIME R>

void CFVMFlowSolverBase< V, R >::HybridParallelInitialization ( const CConfig &  config, CGeometry &  geometry  )

protected

Initialize thread parallel variables.

ImplicitEuler_Iteration()

template<class V , ENUM_REGIME R>

void CFVMFlowSolverBase< V, R >::ImplicitEuler_Iteration ( CGeometry *  geometry, CSolver **  solver_container, CConfig *  config  )

finalvirtual

Implementation of implicit Euler iteration.

Reimplemented from CSolver.

InstantiateEdgeNumerics()

template<class VariableType , ENUM_REGIME FlowRegime>

virtual void CFVMFlowSolverBase< VariableType, FlowRegime >::InstantiateEdgeNumerics ( const CSolver *const *  solvers, const CConfig *  config  )

inlineprotectedvirtual

Instantiate a SIMD numerics object.

Reimplemented in CEulerSolver.

LoadRestart()

template<class V , ENUM_REGIME R>

void CFVMFlowSolverBase< V, R >::LoadRestart ( CGeometry **  geometry, CSolver ***  solver, CConfig *  config, int  iter, bool  update_geo  )

overridevirtual

Load a solution from a restart file.

Parameters

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

Reimplemented from CSolver.

Reimplemented in CIncEulerSolver.

LoadRestart_impl()

template<class V , ENUM_REGIME R>

void CFVMFlowSolverBase< V, R >::LoadRestart_impl ( CGeometry **  geometry, CSolver ***  solver, CConfig *  config, int  iter, bool  update_geo, su2double *  RestartSolution = nullptr, unsigned short  nVar_Restart = 0  )

protected

General implementation to load a flow solution from a restart file.

Parameters

[in]	geometry	- Geometrical definition of the problem.
[in]	solver	- Container vector with all of the solvers.
[in]	config	- Definition of the particular problem.
[in]	iter	- Current external iteration number.
[in]	update_geo	- Flag for updating coords and grid velocity.
[in]	RestartSolution	- Optional buffer to load restart vars into, this allows default values to be given when nVar > nVar_Restart.
[in]	nVar_Restart	- Number of restart variables, if 0 defaults to nVar.

Momentum_Forces()

template<class V , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< V, FlowRegime >::Momentum_Forces ( const CGeometry *  geometry, const CConfig *  config  )

finalvirtual

Compute the pressure forces and all the adimensional coefficients.

Parameters

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

Reimplemented from CSolver.

MultigridProjectEulerWall()

template<class V , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< V, FlowRegime >::MultigridProjectEulerWall ( CGeometry *  , const CConfig *  , bool    )

overridevirtual

Enforce Euler wall BC on a restricted or prolongated multigrid solution by projecting the momentum to the tangent plane of the wall.

Parameters

[in]	geometry	- Coarse grid geometry.
[in]	config	- Definition of the particular problem.
[in]	use_solution_old	- If true, project Solution_Old (corrections); if false, project Solution.

Reimplemented from CSolver.

ompMasterAssignBarrier()

template<class VariableType , ENUM_REGIME FlowRegime>

template<class... Ts>

static void CFVMFlowSolverBase< VariableType, FlowRegime >::ompMasterAssignBarrier ( Ts &&...  lhsRhsPairs )

inlinestaticprotected

Utility to set the value of a member variables safely, and so that the new values are seen by all threads.

Parameters

[in]

lhsRhsPairs

- Pairs of destination and source e.g. a,0,b,-1.

PrepareImplicitIteration_impl()

template<class VariableType , ENUM_REGIME FlowRegime>

template<class DiagonalPrecond >

void CFVMFlowSolverBase< VariableType, FlowRegime >::PrepareImplicitIteration_impl ( DiagonalPrecond &  preconditioner, CGeometry *  geometry, CConfig *  config  )

inlineprotected

Generic implementation to prepare an implicit iteration with an optional preconditioner applied to the diagonal.

Template Parameters

DiagonalPrecond

- A function object implementing: active: A boolean variable to determine if the preconditioner should be used. (config, iPoint, delta): Compute and return a matrix type compatible with the Jacobian matrix, where "delta" is V/dt.

Pressure_Forces()

template<class V , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< V, FlowRegime >::Pressure_Forces ( const CGeometry *  geometry, const CConfig *  config  )

finalvirtual

Compute the pressure forces and all the adimensional coefficients.

Parameters

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

Reimplemented from CSolver.

PrintVerificationError()

template<class VariableType , ENUM_REGIME FlowRegime>

virtual void CFVMFlowSolverBase< VariableType, FlowRegime >::PrintVerificationError ( const CConfig *  config ) const

pure virtual

Print verification error to screen, derived solvers must define this.

Parameters

[in]

config

- Definition of the particular problem.

Implemented in CEulerSolver, CIncEulerSolver, and CNEMOEulerSolver.

PushSolutionBackInTime()

template<class V , ENUM_REGIME R>

void CFVMFlowSolverBase< V, R >::PushSolutionBackInTime ( unsigned long  TimeIter, bool  restart, bool  rans, CSolver ***  solver_container, CGeometry **  geometry, CConfig *  config  )

protected

Move solution to previous time levels (for restarts).

Set_NewSolution()

template<class VariableType , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< VariableType, FlowRegime >::Set_NewSolution ( )

inlinefinalvirtual

Set the new solution variables to the current solution value for classical RK.

Reimplemented from CSolver.

SetCentered_Dissipation_Sensor_impl()

template<class VariableType , ENUM_REGIME FlowRegime>

template<class SensVarFunc >

void CFVMFlowSolverBase< VariableType, FlowRegime >::SetCentered_Dissipation_Sensor_impl ( const SensVarFunc &  sensVar, CGeometry *  geometry, const CConfig *  config  )

inlineprotected

Compute the dissipation sensor for centered schemes.

Parameters

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

Template Parameters

SensVarFunc

- Function object implementing (nodes, iPoint) to return the sensor variable, e.g. pressure.

SetCharacPrimVar()

template<class VariableType , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< VariableType, FlowRegime >::SetCharacPrimVar ( unsigned short  val_marker, unsigned long  val_vertex, unsigned short  val_var, su2double  val_value  )

inlinefinalvirtual

Value of the characteristic variables at the boundaries.

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 pressure coefficient.

Reimplemented from CSolver.

SetConjugateHeatVariable()

template<class VariableType , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< VariableType, FlowRegime >::SetConjugateHeatVariable ( unsigned short  val_marker, unsigned long  val_vertex, unsigned short  pos_var, su2double  relaxation_factor, su2double  val_var  )

inlinefinalvirtual

Set the conjugate heat variables.

Parameters

[in]	val_marker	- marker index
[in]	val_vertex	- vertex index
[in]	pos_var	- variable position (in vector of all conjugate heat variables)
[in]	relaxation	factor - relaxation factor for the change of the variables
[in]	val_var	- value of the variable

Reimplemented from CSolver.

SetCPressureTarget()

template<class VariableType , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< VariableType, FlowRegime >::SetCPressureTarget ( unsigned short  val_marker, unsigned long  val_vertex, su2double  val_pressure  )

inlinefinalvirtual

Set the value of the target Pressure coefficient.

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 pressure coefficient.

Reimplemented from CSolver.

SetDensity_Inf()

template<class VariableType , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< VariableType, FlowRegime >::SetDensity_Inf ( su2double  rho_inf )

inlinefinalvirtual

Set the freestream temperature.

Parameters

[in]

Value

of freestream temperature.

Reimplemented from CSolver.

SetHeatFluxTarget()

template<class VariableType , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< VariableType, FlowRegime >::SetHeatFluxTarget ( unsigned short  val_marker, unsigned long  val_vertex, su2double  val_heat  )

inlinefinalvirtual

Set the value of the target Pressure coefficient.

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 pressure coefficient.

Reimplemented from CSolver.

SetInitialCondition()

template<class V , ENUM_REGIME R>

void CFVMFlowSolverBase< V, R >::SetInitialCondition ( CGeometry **  geometry, CSolver ***  solver_container, CConfig *  config, unsigned long  ExtIter  )

overridevirtual

Set the initial condition for the Euler Equations.

Parameters

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

Reimplemented from CSolver.

SetInletAtVertex()

template<class V , ENUM_REGIME R>

void CFVMFlowSolverBase< V, R >::SetInletAtVertex ( const su2double *  val_inlet, unsigned short  iMarker, unsigned long  iVertex  )

finalvirtual

Store of a set of provided inlet profile values at a vertex.

Parameters

[in]	val_inlet	- vector containing the inlet values for the current vertex.
[in]	iMarker	- Index of the surface marker.
[in]	iVertex	- Vertex of the marker iMarker where the inlet is being set.

Reimplemented from CSolver.

SetInletFlowDir()

template<class VariableType , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< VariableType, FlowRegime >::SetInletFlowDir ( unsigned short  val_marker, unsigned long  val_vertex, unsigned short  val_dim, su2double  val_flowdir  )

inlinefinalvirtual

Set a component of the unit vector representing the flow direction at an inlet boundary.

Parameters

[in]	val_marker	- Surface marker where the flow direction is set.
[in]	val_vertex	- Vertex of the marker val_marker where the flow direction is set.
[in]	val_dim	- The component of the flow direction unit vector to be set
[in]	val_flowdir	- Component of a unit vector representing the flow direction.

Reimplemented from CSolver.

SetInletPtotal()

template<class VariableType , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< VariableType, FlowRegime >::SetInletPtotal ( unsigned short  val_marker, unsigned long  val_vertex, su2double  val_ptotal  )

inlinefinalvirtual

Set the value of the total pressure at an inlet boundary.

Parameters

[in]	val_marker	- Surface marker where the total pressure is set.
[in]	val_vertex	- Vertex of the marker val_marker where the total pressure is set.
[in]	val_ptotal	- Value of the total pressure

Reimplemented from CSolver.

SetInletTtotal()

template<class VariableType , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< VariableType, FlowRegime >::SetInletTtotal ( unsigned short  val_marker, unsigned long  val_vertex, su2double  val_ttotal  )

inlinefinalvirtual

Set the value of the total temperature at an inlet boundary.

Parameters

[in]	val_marker	- Surface marker where the total temperature is set.
[in]	val_vertex	- Vertex of the marker val_marker where the total temperature is set.
[in]	val_ttotal	- Value of the total temperature

Reimplemented from CSolver.

SetMax_Eigenvalue_impl()

template<class VariableType , ENUM_REGIME FlowRegime>

template<class SoundSpeedFunc >

void CFVMFlowSolverBase< VariableType, FlowRegime >::SetMax_Eigenvalue_impl ( const SoundSpeedFunc &  soundSpeed, CGeometry *  geometry, const CConfig *  config  )

inlineprotected

Compute the max eigenvalue, gemeric implementation.

Parameters

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

Template Parameters

SoundSpeedFunc

- Function object to compute speed of sound.

Note

Functor needs to implement (nodes,iPoint,jPoint) for edges, and (nodes,iPoint) for vertices.

SetnSlidingStates()

template<class VariableType , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< VariableType, FlowRegime >::SetnSlidingStates ( unsigned short  val_marker, unsigned long  val_vertex, int  value  )

inlinefinalvirtual

Set the number of outer state for fluid interface nodes.

Parameters

[in]	val_marker	- marker index
[in]	val_vertex	- vertex index
[in]	value	- number of outer states

Reimplemented from CSolver.

SetPressure_Inf()

template<class VariableType , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< VariableType, FlowRegime >::SetPressure_Inf ( su2double  p_inf )

inlinefinalvirtual

Set the freestream pressure.

Parameters

[in]

Value

of freestream pressure.

Reimplemented from CSolver.

SetPrimitive_Gradient_GG()

template<class V , ENUM_REGIME R>

void CFVMFlowSolverBase< V, R >::SetPrimitive_Gradient_GG ( CGeometry *  geometry, const CConfig *  config, bool  reconstruction = false  )

overridevirtual

Compute the gradient of the primitive variables using Green-Gauss method, and stores the result in the Gradient_Primitive variable.

Parameters

[in]	geometry	- Geometrical definition of the problem.
[in]	config	- Definition of the particular problem.
[in]	reconstruction	- indicator that the gradient being computed is for upwind reconstruction.

Reimplemented from CSolver.

Reimplemented in CNEMONSSolver.

SetPrimitive_Gradient_LS()

template<class V , ENUM_REGIME R>

void CFVMFlowSolverBase< V, R >::SetPrimitive_Gradient_LS ( CGeometry *  geometry, const CConfig *  config, bool  reconstruction = false  )

finalvirtual

Compute the gradient of the primitive variables using a Least-Squares method, and stores the result in the Gradient_Primitive variable.

Parameters

[in]	geometry	- Geometrical definition of the problem.
[in]	config	- Definition of the particular problem.
[in]	reconstruction	- indicator that the gradient being computed is for upwind reconstruction.

Reimplemented from CSolver.

SetPrimitive_Limiter()

template<class V , ENUM_REGIME R>

void CFVMFlowSolverBase< V, R >::SetPrimitive_Limiter ( CGeometry *  geometry, const CConfig *  config  )

finalvirtual

Compute the limiter of the primitive variables.

Parameters

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

Reimplemented from CSolver.

SetReferenceValues()

template<class VariableType , ENUM_REGIME FlowRegime>

virtual void CFVMFlowSolverBase< VariableType, FlowRegime >::SetReferenceValues ( const CConfig &  config )

protectedpure virtual

Set reference values for pressure, forces, etc., e.g. "AeroCoeffForceRef".

Note

Implement this method in the derived class and call it in its constructor. Duplicating this type of information has caused bugs (I know because I fixed them).

Implemented in CEulerSolver, CIncEulerSolver, and CNEMOEulerSolver.

SetResidual_DualTime()

template<class V , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< V, FlowRegime >::SetResidual_DualTime ( CGeometry *  geometry, CSolver **  solver_container, CConfig *  config, unsigned short  iRKStep, unsigned short  iMesh, unsigned short  RunTime_EqSystem  )

overridevirtual

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

Parameters

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

Reimplemented from CSolver.

Reimplemented in CIncEulerSolver.

SetSlidingState()

template<class VariableType , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< VariableType, FlowRegime >::SetSlidingState ( unsigned short  val_marker, unsigned long  val_vertex, unsigned short  val_state, unsigned long  donor_index, su2double  component  )

inlinefinalvirtual

Set the outer state for fluid interface nodes.

Parameters

[in]	val_marker	- marker index
[in]	val_vertex	- vertex index
[in]	val_state	- requested state component
[in]	donor_index	- index of the donor node to set
[in]	component	- set value

Reimplemented from CSolver.

SetSlidingStateStructure()

template<class VariableType , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< VariableType, FlowRegime >::SetSlidingStateStructure ( unsigned short  val_marker, unsigned long  val_vertex  )

inlinefinalvirtual

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].

Parameters

[in]	val_marker	- marker index
[in]	val_vertex	- vertex index

Reimplemented from CSolver.

SetTemperature_Inf()

template<class VariableType , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< VariableType, FlowRegime >::SetTemperature_Inf ( su2double  t_inf )

inlinefinalvirtual

Set the freestream temperature.

Parameters

[in]

Value

of freestream temperature.

Reimplemented from CSolver.

SetTime_Step_impl()

template<class VariableType , ENUM_REGIME FlowRegime>

template<class SoundSpeedFunc , class LambdaViscFunc >

void CFVMFlowSolverBase< VariableType, FlowRegime >::SetTime_Step_impl ( const SoundSpeedFunc &  soundSpeed, const LambdaViscFunc &  lambdaVisc, CGeometry *  geometry, CSolver **  solver_container, CConfig *  config, unsigned short  iMesh, unsigned long  Iteration  )

inlineprotected

Generic implementation to compute the time step based on CFL and conv/visc eigenvalues.

Parameters

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

Template Parameters

SoundSpeedFunc	- Function object to compute speed of sound.
LambdaViscFunc	- Function object to compute the viscous lambda.

Note

Both functors need to implement (nodes,iPoint,jPoint) for edges, and (nodes,iPoint) for vertices.

SetTotal_CD()

template<class VariableType , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< VariableType, FlowRegime >::SetTotal_CD ( su2double  val_Total_CD )

inlinefinalvirtual

Store the total (inviscid + viscous) non dimensional drag coefficient.

Parameters

[in]

val_Total_CD

- Value of the total drag coefficient.

Reimplemented from CSolver.

SetTotal_CEquivArea()

template<class VariableType , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< VariableType, FlowRegime >::SetTotal_CEquivArea ( su2double  val_equiv )

inlinefinalvirtual

Set the value of the Equivalent Area coefficient.

Parameters

[in]

val_equiv

- Value of the Equivalent Area coefficient.

Reimplemented from CSolver.

SetTotal_CL()

template<class VariableType , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< VariableType, FlowRegime >::SetTotal_CL ( su2double  val_Total_CL )

inlinefinalvirtual

Store the total (inviscid + viscous) non dimensional lift coefficient.

Parameters

[in]

val_Total_CL

- Value of the total lift coefficient.

Reimplemented from CSolver.

SetTotal_CNearFieldOF()

template<class VariableType , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< VariableType, FlowRegime >::SetTotal_CNearFieldOF ( su2double  val_cnearfieldpress )

inlinefinalvirtual

Set the value of the Near-Field pressure oefficient.

Parameters

[in]

val_cnearfieldpress

- Value of the Near-Field pressure coefficient.

Reimplemented from CSolver.

SetTotal_CpDiff()

template<class VariableType , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< VariableType, FlowRegime >::SetTotal_CpDiff ( su2double  val_pressure )

inlinefinalvirtual

Set the value of the Equivalent Area coefficient.

Parameters

[in]

val_cequivarea

- Value of the Equivalent Area coefficient.

Reimplemented from CSolver.

SetTotal_CQ()

template<class VariableType , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< VariableType, FlowRegime >::SetTotal_CQ ( su2double  val_Total_CQ )

inlinefinalvirtual

Store the total (inviscid + viscous) non dimensional torque coefficient.

Parameters

[in]

val_Total_CQ

- Value of the total torque coefficient.

Reimplemented from CSolver.

SetTotal_CT()

template<class VariableType , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< VariableType, FlowRegime >::SetTotal_CT ( su2double  val_Total_CT )

inlinefinalvirtual

Store the total (inviscid + viscous) non dimensional thrust coefficient.

Parameters

[in]

val_Total_CT

- Value of the total thrust coefficient.

Reimplemented from CSolver.

SetTotal_HeatFlux()

template<class VariableType , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< VariableType, FlowRegime >::SetTotal_HeatFlux ( su2double  val_Total_Heat )

inlinefinalvirtual

Store the total heat load.

Parameters

[in]

val_Total_Heat

- Value of the heat load.

Reimplemented from CSolver.

SetTotal_HeatFluxDiff()

template<class VariableType , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< VariableType, FlowRegime >::SetTotal_HeatFluxDiff ( su2double  val_heat )

inlinefinalvirtual

Set the value of the Equivalent Area coefficient.

Parameters

[in]

val_cequivarea

- Value of the Equivalent Area coefficient.

Reimplemented from CSolver.

SetTotal_MaxHeatFlux()

template<class VariableType , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< VariableType, FlowRegime >::SetTotal_MaxHeatFlux ( su2double  val_Total_MaxHeat )

inlinefinalvirtual

Store the total heat load.

Parameters

[in]

val_Total_Heat

- Value of the heat load.

Reimplemented from CSolver.

SetUniformInlet()

template<class V , ENUM_REGIME R>

void CFVMFlowSolverBase< V, R >::SetUniformInlet ( const CConfig *  config, unsigned short  iMarker  )

finalvirtual

Set a uniform inlet profile.

The values at the inlet are set to match the values specified for inlets in the configuration file.

Parameters

[in]	config	- Definition of the particular problem.
[in]	iMarker	- Surface marker where the coefficient is computed.

Reimplemented from CSolver.

SetVelocity_Inf()

template<class VariableType , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< VariableType, FlowRegime >::SetVelocity_Inf ( unsigned short  val_dim, su2double  val_velocity  )

inlinefinalvirtual

Set the velocity at infinity.

Parameters

[in]	val_dim	- Index of the velocity vector.
[in]	val_velocity	- Value of the velocity.

Reimplemented from CSolver.

SumEdgeFluxes()

template<class V , ENUM_REGIME R>

void CFVMFlowSolverBase< V, R >::SumEdgeFluxes ( const CGeometry *  geometry )

protected

Sum the edge fluxes for each cell to populate the residual vector, only used on coarse grids.

UpdateCustomBoundaryConditions()

template<class V , ENUM_REGIME R>

void CFVMFlowSolverBase< V, R >::UpdateCustomBoundaryConditions ( CGeometry **  geometry_container, CSolver ***  solver_container, CConfig *  config  )

finalvirtual

Update the multi-grid structure for the customized boundary conditions.

Parameters

geometry_container	- Geometrical definition.
solver_container	- Solver definition.
config	- Definition of the particular problem.

Reimplemented from CSolver.

UpdateFarfieldVelocity()

template<class VariableType , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< VariableType, FlowRegime >::UpdateFarfieldVelocity ( const CConfig *  config )

inlinefinalvirtual

Updates the components of the farfield velocity vector.

Reimplemented from CSolver.

UpdateJacobian()

template<class VariableType , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< VariableType, FlowRegime >::UpdateJacobian ( unsigned long  iEdge, unsigned long  iPoint, unsigned long  jPoint, const CNumerics::ResidualType<> &  conv, const CNumerics::ResidualType<> &  visc  )

inlineprotected

Update the Jacobian for one edge with the fused convective and viscous contributions.

Note

Both contributions must be applied at once because in quantized mode the off-diagonal blocks of the matrix can only be overwritten, not accumulated.

Parameters

[in]	iEdge	- Edge index for the off-diagonal blocks.
[in]	iPoint,jPoint	- Points connected by the edge (diagonal blocks).
[in]	conv	- Convective residual/Jacobians (added to i, subtracted from j).
[in]	visc	- Viscous residual/Jacobians (subtracted from i, added to j), may hold null Jacobians.

Viscous_Residual() [1/2]

template<class VariableType , ENUM_REGIME FlowRegime>

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

inlineprotectedvirtual

A virtual member.

Parameters

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

Reimplemented from CSolver.

Viscous_Residual() [2/2]

template<class VariableType , ENUM_REGIME FlowRegime>

virtual CNumerics::ResidualType CFVMFlowSolverBase< VariableType, FlowRegime >::Viscous_Residual ( unsigned long  iEdge, CGeometry *  geometry, CSolver **  solver_container, CNumerics *  numerics, CConfig *  config  )

inlineprotectedvirtual

Compute the viscous contribution for a particular edge.

Note

The convective residual methods include a call to this for each edge, this allows convective and viscous loops to be "fused". Only the residual is applied here, the Jacobians are returned so that the caller can update the system matrix in a single operation together with the convective part (a requirement of quantized matrix storage).

Parameters

[in]	iEdge	- Edge for which the flux and Jacobians are to be computed.
[in]	geometry	- Geometrical definition of the problem.
[in]	solver_container	- Container vector with all the solutions.
[in]	numerics	- Description of the numerical method.
[in]	config	- Definition of the particular problem.

Returns

The viscous Jacobians (null for inviscid solvers).

Viscous_Residual_impl()

template<class V , ENUM_REGIME R>

CNumerics::ResidualType CFVMFlowSolverBase< V, R >::Viscous_Residual_impl ( unsigned long  iEdge, CGeometry *  geometry, CSolver **  solver_container, CNumerics *  numerics, CConfig *  config  )

protected

Member Data Documentation

AeroCoeffForceRef

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::AeroCoeffForceRef = 1.0

protected

Reference force for aerodynamic coefficients.

AllBound_CNearFieldOF_Inv

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::AllBound_CNearFieldOF_Inv = 0.0

protected

Near-Field press coeff (inviscid) for all the boundaries.

AllBound_HF_Visc

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::AllBound_HF_Visc = 0.0

protected

Heat load (viscous contribution) for all the boundaries.

AllBound_MaxHF_Visc

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::AllBound_MaxHF_Visc = 0.0

protected

Maximum heat flux (viscous contribution) for all boundaries.

AllBoundInvCoeff

template<class VariableType , ENUM_REGIME FlowRegime>

AeroCoeffs CFVMFlowSolverBase< VariableType, FlowRegime >::AllBoundInvCoeff

protected

Total pressure contribution for all the boundaries.

AllBoundMntCoeff

template<class VariableType , ENUM_REGIME FlowRegime>

AeroCoeffs CFVMFlowSolverBase< VariableType, FlowRegime >::AllBoundMntCoeff

protected

Total momentum contribution for all the boundaries.

AllBoundViscCoeff

template<class VariableType , ENUM_REGIME FlowRegime>

AeroCoeffs CFVMFlowSolverBase< VariableType, FlowRegime >::AllBoundViscCoeff

protected

Total pressure contribution for all the boundaries.

CharacPrimVar

template<class VariableType , ENUM_REGIME FlowRegime>

vector<su2activematrix> CFVMFlowSolverBase< VariableType, FlowRegime >::CharacPrimVar

protected

Value of the characteristic variables at each boundary.

CNearFieldOF_Inv

template<class VariableType , ENUM_REGIME FlowRegime>

vector<su2double> CFVMFlowSolverBase< VariableType, FlowRegime >::CNearFieldOF_Inv

protected

Near field pressure (inviscid) for each boundary.

CPressure

template<class VariableType , ENUM_REGIME FlowRegime>

vector<vector<su2double> > CFVMFlowSolverBase< VariableType, FlowRegime >::CPressure

protected

Pressure coefficient for each boundary and vertex.

CPressureTarget

template<class VariableType , ENUM_REGIME FlowRegime>

vector<vector<su2double> > CFVMFlowSolverBase< VariableType, FlowRegime >::CPressureTarget

protected

Target Pressure coefficient for each boundary and vertex.

CSkinFriction

template<class VariableType , ENUM_REGIME FlowRegime>

vector<su2activematrix> CFVMFlowSolverBase< VariableType, FlowRegime >::CSkinFriction

protected

Skin friction coefficient for each boundary and vertex.

Density_Inf

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::Density_Inf = 0.0

protected

Density at the infinity.

DynamicPressureRef

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::DynamicPressureRef = 1.0

protected

Reference dynamic pressure.

EddyViscWall

template<class VariableType , ENUM_REGIME FlowRegime>

vector<vector<su2double> > CFVMFlowSolverBase< VariableType, FlowRegime >::EddyViscWall

protected

Eddy viscosuty at the wall for each boundary and vertex.

EdgeColoring

template<class VariableType , ENUM_REGIME FlowRegime>

array<DummyGridColor<>, 1> CFVMFlowSolverBase< VariableType, FlowRegime >::EdgeColoring

protected

EdgeFluxes

template<class VariableType , ENUM_REGIME FlowRegime>

CSysVector<su2double> CFVMFlowSolverBase< VariableType, FlowRegime >::EdgeFluxes

protected

Flux across each edge.

EdgeMassFluxes

template<class VariableType , ENUM_REGIME FlowRegime>

su2activevector CFVMFlowSolverBase< VariableType, FlowRegime >::EdgeMassFluxes

protected

Mass fluxes across each edge, for discretization of transported scalars.

edgeNumerics

template<class VariableType , ENUM_REGIME FlowRegime>

CNumericsSIMD* CFVMFlowSolverBase< VariableType, FlowRegime >::edgeNumerics = nullptr

protected

Object for edge flux computation.

Energy_Inf

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::Energy_Inf = 0.0

protected

Energy at the infinity.

Enthalpy_Inf

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::Enthalpy_Inf = 0.0

protected

Enthalpy at the infinity.

ErrorCounter

template<class VariableType , ENUM_REGIME FlowRegime>

unsigned long CFVMFlowSolverBase< VariableType, FlowRegime >::ErrorCounter = 0

protected

Counter for number of un-physical states.

euler_implicit

template<class VariableType , ENUM_REGIME FlowRegime>

bool CFVMFlowSolverBase< VariableType, FlowRegime >::euler_implicit

protected

True if euler implicit scheme used.

Gamma

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::Gamma

protected

Fluid's Gamma constant (ratio of specific heats).

Gamma_Minus_One

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::Gamma_Minus_One

protected

Fluids's Gamma - 1.0 .

Global_Delta_Time

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::Global_Delta_Time = 0.0

protected

Time-step for TIME_STEPPING time marching strategy.

Global_Delta_UnstTimeND

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::Global_Delta_UnstTimeND = 0.0

protected

Unsteady time step for the dual time strategy.

HeatConjugateVar

template<class VariableType , ENUM_REGIME FlowRegime>

vector<su2activematrix> CFVMFlowSolverBase< VariableType, FlowRegime >::HeatConjugateVar

protected

CHT variables for each boundary and vertex.

HeatFlux

template<class VariableType , ENUM_REGIME FlowRegime>

vector<vector<su2double> > CFVMFlowSolverBase< VariableType, FlowRegime >::HeatFlux

protected

Heat transfer coefficient for each boundary and vertex.

HeatFluxTarget

template<class VariableType , ENUM_REGIME FlowRegime>

vector<vector<su2double> > CFVMFlowSolverBase< VariableType, FlowRegime >::HeatFluxTarget

protected

Heat transfer coefficient for each boundary and vertex.

HF_Visc

template<class VariableType , ENUM_REGIME FlowRegime>

vector<su2double> CFVMFlowSolverBase< VariableType, FlowRegime >::HF_Visc

protected

Heat load (viscous contribution) for each boundary.

Inlet_FlowDir

template<class VariableType , ENUM_REGIME FlowRegime>

vector<su2activematrix> CFVMFlowSolverBase< VariableType, FlowRegime >::Inlet_FlowDir

protected

Value of the Flow Direction.

Inlet_Ptotal

template<class VariableType , ENUM_REGIME FlowRegime>

vector<vector<su2double> > CFVMFlowSolverBase< VariableType, FlowRegime >::Inlet_Ptotal

protected

Value of the Total P.

Inlet_Ttotal

template<class VariableType , ENUM_REGIME FlowRegime>

vector<vector<su2double> > CFVMFlowSolverBase< VariableType, FlowRegime >::Inlet_Ttotal

protected

Value of the Total T.

InvCoeff

template<class VariableType , ENUM_REGIME FlowRegime>

AeroCoeffsArray CFVMFlowSolverBase< VariableType, FlowRegime >::InvCoeff

protected

Inviscid pressure contributions for each boundary.

least_squares

template<class VariableType , ENUM_REGIME FlowRegime>

bool CFVMFlowSolverBase< VariableType, FlowRegime >::least_squares

protected

True if computing gradients by least squares.

Mach_Inf

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::Mach_Inf = 0.0

protected

Mach number at the infinity.

MaxHF_Visc

template<class VariableType , ENUM_REGIME FlowRegime>

vector<su2double> CFVMFlowSolverBase< VariableType, FlowRegime >::MaxHF_Visc

protected

Maximum heat flux (viscous contribution) for each boundary.

MAXNDIM

template<class VariableType , ENUM_REGIME FlowRegime>

constexpr size_t CFVMFlowSolverBase< VariableType, FlowRegime >::MAXNDIM = 3

staticconstexprprotected

Max number of space dimensions, used in some static arrays.

MAXNVAR

template<class VariableType , ENUM_REGIME FlowRegime>

constexpr size_t CFVMFlowSolverBase< VariableType, FlowRegime >::MAXNVAR = VariableType::MAXNVAR

staticconstexprprotected

Max number of variables, for static arrays.

MntCoeff

template<class VariableType , ENUM_REGIME FlowRegime>

AeroCoeffsArray CFVMFlowSolverBase< VariableType, FlowRegime >::MntCoeff

protected

Inviscid momentum contributions for each boundary.

nodes

template<class VariableType , ENUM_REGIME FlowRegime>

VariableType* CFVMFlowSolverBase< VariableType, FlowRegime >::nodes = nullptr

protected

The highest level in the variable hierarchy the DERIVED solver can safely use.

Omega_Max

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::Omega_Max

protected

Maximum Omega.

omp_chunk_size

template<class VariableType , ENUM_REGIME FlowRegime>

unsigned long CFVMFlowSolverBase< VariableType, FlowRegime >::omp_chunk_size

protected

Chunk size used in light point loops.

OMP_MAX_SIZE

template<class VariableType , ENUM_REGIME FlowRegime>

constexpr size_t CFVMFlowSolverBase< VariableType, FlowRegime >::OMP_MAX_SIZE = 512

staticconstexprprotected

Max chunk size for light point loops.

OMP_MIN_SIZE

template<class VariableType , ENUM_REGIME FlowRegime>

constexpr size_t CFVMFlowSolverBase< VariableType, FlowRegime >::OMP_MIN_SIZE = 32

staticconstexprprotected

Min chunk size for edge loops (max is color group size).

Pressure_Inf

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::Pressure_Inf = 0.0

protected

Pressure at the infinity.

prim_idx

template<class VariableType , ENUM_REGIME FlowRegime>

const VariableType::template CIndices<unsigned short> CFVMFlowSolverBase< VariableType, FlowRegime >::prim_idx

protected

Object with indices of primitive variables.

<

ReducerStrategy

template<class VariableType , ENUM_REGIME FlowRegime>

constexpr bool CFVMFlowSolverBase< VariableType, FlowRegime >::ReducerStrategy = false

staticconstexprprotected

SlidingState

template<class VariableType , ENUM_REGIME FlowRegime>

vector<su2matrix<su2double*> > CFVMFlowSolverBase< VariableType, FlowRegime >::SlidingState

protected

SlidingStateNodes

template<class VariableType , ENUM_REGIME FlowRegime>

vector<vector<int> > CFVMFlowSolverBase< VariableType, FlowRegime >::SlidingStateNodes

protected

space_centered

template<class VariableType , ENUM_REGIME FlowRegime>

bool CFVMFlowSolverBase< VariableType, FlowRegime >::space_centered

protected

True if space centered scheme used.

StrainMag_Max

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::StrainMag_Max

protected

Maximum Strain Rate magnitude.

Surface_HF_Visc

template<class VariableType , ENUM_REGIME FlowRegime>

vector<su2double> CFVMFlowSolverBase< VariableType, FlowRegime >::Surface_HF_Visc

protected

Total (integrated) heat flux for each monitored surface.

Surface_MaxHF_Visc

template<class VariableType , ENUM_REGIME FlowRegime>

vector<su2double> CFVMFlowSolverBase< VariableType, FlowRegime >::Surface_MaxHF_Visc

protected

Maximum heat flux for each monitored surface.

SurfaceCoeff

template<class VariableType , ENUM_REGIME FlowRegime>

AeroCoeffsArray CFVMFlowSolverBase< VariableType, FlowRegime >::SurfaceCoeff

protected

Totals for each monitoring surface.

SurfaceInvCoeff

template<class VariableType , ENUM_REGIME FlowRegime>

AeroCoeffsArray CFVMFlowSolverBase< VariableType, FlowRegime >::SurfaceInvCoeff

protected

Inviscid pressure contributions for each monitoring boundary.

SurfaceMntCoeff

template<class VariableType , ENUM_REGIME FlowRegime>

AeroCoeffsArray CFVMFlowSolverBase< VariableType, FlowRegime >::SurfaceMntCoeff

protected

Inviscid momentum contributions for each monitoring boundary.

SurfaceViscCoeff

template<class VariableType , ENUM_REGIME FlowRegime>

AeroCoeffsArray CFVMFlowSolverBase< VariableType, FlowRegime >::SurfaceViscCoeff

protected

Viscous contributions for each monitoring boundary.

Temperature_Inf

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::Temperature_Inf = 0.0

protected

Temperature at the infinity.

Tke_Inf

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::Tke_Inf

protected

Turbulent kinetic energy at the infinity.

Total_CEquivArea

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::Total_CEquivArea = 0.0

protected

Total Equivalent Area coefficient for all the boundaries.

Total_CNearFieldOF

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::Total_CNearFieldOF = 0.0

protected

Total Near-Field Pressure coefficient for all the boundaries.

Total_CpDiff

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::Total_CpDiff = 0.0

protected

Total Equivalent Area coefficient for all the boundaries.

Total_Heat

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::Total_Heat = 0.0

protected

Total heat load for all the boundaries.

Total_HeatFluxDiff

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::Total_HeatFluxDiff = 0.0

protected

Total Equivalent Area coefficient for all the boundaries.

Total_MassFlowRate

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::Total_MassFlowRate = 0.0

protected

Total Mass Flow Rate on monitored boundaries.

Total_MaxHeat

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::Total_MaxHeat = 0.0

protected

Maximum heat flux on all boundaries.

TotalCoeff

template<class VariableType , ENUM_REGIME FlowRegime>

AeroCoeffs CFVMFlowSolverBase< VariableType, FlowRegime >::TotalCoeff

protected

Totals for all boundaries.

UTau

template<class VariableType , ENUM_REGIME FlowRegime>

vector<vector<su2double> > CFVMFlowSolverBase< VariableType, FlowRegime >::UTau

protected

UTau for each boundary and vertex.

Velocity_Inf

template<class VariableType , ENUM_REGIME FlowRegime>

su2double* CFVMFlowSolverBase< VariableType, FlowRegime >::Velocity_Inf = nullptr

protected

Flow Velocity vector at the infinity.

ViscCoeff

template<class VariableType , ENUM_REGIME FlowRegime>

AeroCoeffsArray CFVMFlowSolverBase< VariableType, FlowRegime >::ViscCoeff

protected

Viscous contributions for each boundary.

Viscosity_Inf

template<class VariableType , ENUM_REGIME FlowRegime>

su2double CFVMFlowSolverBase< VariableType, FlowRegime >::Viscosity_Inf

protected

Viscosity at the infinity.

WallShearStress

template<class VariableType , ENUM_REGIME FlowRegime>

vector<vector<su2double> > CFVMFlowSolverBase< VariableType, FlowRegime >::WallShearStress

protected

Wall Shear Stress for each boundary and vertex.

YPlus

template<class VariableType , ENUM_REGIME FlowRegime>

vector<vector<su2double> > CFVMFlowSolverBase< VariableType, FlowRegime >::YPlus

protected

Yplus for each boundary and vertex.

---

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

• SU2_CFD/include/solvers/CFVMFlowSolverBase.hpp
• SU2_CFD/include/solvers/CFVMFlowSolverBase.inl