CEulerSolver Class Reference

Class for compressible inviscid flow problems, serves as base for Navier-Stokes/RANS. More...

#include <CEulerSolver.hpp>

Inheritance diagram for CEulerSolver:

Public Member Functions
	CEulerSolver ()=delete
	CEulerSolver (CGeometry *geometry, CConfig *config, unsigned short iMesh, const bool navier_stokes=false)
	Main constructor of this class.
	~CEulerSolver (void) override
	Destructor of the class.
CFluidModel *	GetFluidModel (void) const final
	Compute the pressure at the infinity.
void	SetTime_Step (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh, unsigned long Iteration) final
	Compute the time step for solving the Euler equations.
void	Centered_Residual (CGeometry *geometry, CSolver **solver_container, CNumerics **numerics_container, CConfig *config, unsigned short iMesh, unsigned short iRKStep) final
	Compute the spatial integration using a centered scheme.
void	Upwind_Residual (CGeometry *geometry, CSolver **solver_container, CNumerics **numerics_container, CConfig *config, unsigned short iMesh) final
	Compute the spatial integration using a upwind scheme.
void	Source_Residual (CGeometry *geometry, CSolver **solver_container, CNumerics **numerics_container, CConfig *config, unsigned short iMesh) override
	Source term integration.
void	Source_Template (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short iMesh) final
	Source term integration.
void	Preprocessing (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh, unsigned short iRKStep, unsigned short RunTime_EqSystem, bool Output) override
	Compute primitive variables and their gradients.
void	SetPreconditioner (const CConfig *config, unsigned long iPoint, su2double delta, su2activematrix &preconditioner) const
	Compute the preconditioner for convergence acceleration by Roe-Turkel method.
void	Evaluate_ObjFunc (const CConfig *config, CSolver **solver) override
	Compute weighted-sum "combo" objective output.
void	BC_Far_Field (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) final
	Impose the far-field boundary condition using characteristics.
void	BC_ActDisk_Inlet (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) final
	Impose the engine inflow boundary condition.
void	BC_ActDisk_Outlet (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) final
	Impose the engine exhaust boundary condition.
void	BC_ActDisk (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker, bool val_inlet_surface) final
	Impose an actuator disk inlet boundary condition.
void	BC_ActDisk_VariableLoad (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker, bool val_inlet_surface)
	Impose an actuator disk with variable load boundary condition.
void	BC_Riemann (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) final
	Impose the boundary condition using characteristic recostruction.
void	BC_TurboRiemann (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) final
	Impose the boundary condition using characteristic recostruction.
void	PreprocessBC_Giles (CGeometry *geometry, CConfig *config, CNumerics *conv_numerics, unsigned short marker_flag) final
	It computes Fourier transformation for the needed quantities along the pitch for each span in turbomachinery analysis.
void	BC_Giles (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) final
	Impose the boundary condition using characteristic recostruction.
void	BC_Inlet (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) final
	Impose a subsonic inlet boundary condition.
void	BC_Supersonic_Inlet (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) final
	Impose a supersonic inlet boundary condition.
void	BC_Supersonic_Outlet (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) final
	Impose a supersonic outlet boundary condition.
void	BC_Outlet (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) final
	Impose the outlet boundary condition.
void	BC_Engine_Inflow (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) final
	Impose the nacelle inflow boundary condition.
void	BC_Engine_Exhaust (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) final
	Impose the ancelle exhaust boundary condition.
void	ExplicitRK_Iteration (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iRKStep) final
	Update the solution using a Runge-Kutta scheme.
void	ClassicalRK4_Iteration (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iRKStep) final
	Update the solution using the classical fourth-order Runge-Kutta scheme.
bool	FixedCL_Convergence (CConfig *config, bool convergence) final
	Check for convergence of the Fixed CL mode to the target CL.
bool	GetStart_AoA_FD (void) const final
	Checking whether fixed CL mode in finite-differencing mode.
bool	GetEnd_AoA_FD (void) const final
	Checking whether fixed CL mode in finite-differencing mode.
unsigned long	GetIter_Update_AoA (void) const final
	Get the iteration of the last AoA update (Fixed CL Mode)
su2double	GetPrevious_AoA (void) const final
	Get the AoA before the most recent update.
su2double	GetAoA_inc (void) const final
	Get the CL Driver's control command.
void	ExplicitEuler_Iteration (CGeometry *geometry, CSolver **solver_container, CConfig *config) final
	Update the solution using the explicit Euler scheme.
void	PrepareImplicitIteration (CGeometry *geometry, CSolver **, CConfig *config) final
	Prepare an implicit iteration.
void	ComputeUnderRelaxationFactor (const CConfig *config) final
	Compute a suitable under-relaxation parameter to limit the change in the solution variables over a nonlinear iteration for stability.
void	IdentifySolutionOutliers (const CConfig *config, unsigned long iter) final
	Identify points where the static temperature is an outlier to treat them as non-physical, e.g. force the reconstruction to be 1st order.
su2double	GetInflow_MassFlow (unsigned short val_marker) const final
	Provide the mass flow rate.
su2double	GetExhaust_MassFlow (unsigned short val_marker) const final
	Provide the mass flow rate.
su2double	GetInflow_Pressure (unsigned short val_marker) const final
	Provide the mass flow rate.
su2double	GetInflow_Mach (unsigned short val_marker) const final
	Provide the mass flow rate.
su2double	GetTotal_AeroCD () const final
	Provide the total (inviscid + viscous) non dimensional aero CD.
su2double	GetTotal_CNearFieldOF () const final
	Provide the total (inviscid + viscous) non dimensional Near-Field pressure coefficient.
void	SetTotal_AeroCD (su2double val_aerocd) final
	Set the value of the Aero drag.
su2double	GetTotal_NetThrust () const final
	Provide the total (inviscid + viscous) non dimensional drag coefficient.
su2double	GetTotal_Power () const final
	Provide the total (inviscid + viscous) non dimensional drag coefficient.
su2double	GetTotal_SolidCD () const final
	Provide the total (inviscid + viscous) non dimensional drag coefficient.
su2double	GetTotal_ReverseFlow () const final
	Provide the total (inviscid + viscous) non dimensional drag coefficient.
su2double	GetTotal_MFR () const final
	Provide the total (inviscid + viscous) non dimensional drag coefficient.
su2double	GetTotal_Prop_Eff () const final
	Provide the total (inviscid + viscous) non dimensional drag coefficient.
su2double	GetTotal_ByPassProp_Eff () const final
	Provide the total (inviscid + viscous) non dimensional drag coefficient.
su2double	GetTotal_Adiab_Eff () const final
	Provide the total (inviscid + viscous) non dimensional drag coefficient.
su2double	GetTotal_Poly_Eff () const final
	Provide the total (inviscid + viscous) non dimensional drag coefficient.
su2double	GetTotal_IDC () const final
	Provide the total (inviscid + viscous) non dimensional drag coefficient.
su2double	GetTotal_IDC_Mach () const final
	Provide the total (inviscid + viscous) non dimensional drag coefficient.
su2double	GetTotal_IDR () const final
	Provide the total (inviscid + viscous) non dimensional drag coefficient.
su2double	GetTotal_DC60 () const final
	Provide the total (inviscid + viscous) non dimensional drag coefficient.
void	SetTotal_NetThrust (su2double val_Total_NetThrust) final
	Store the total (inviscid + viscous) non dimensional drag coefficient.
void	SetTotal_Power (su2double val_Total_Power) final
	Store the total (inviscid + viscous) non dimensional drag coefficient.
void	SetTotal_SolidCD (su2double val_Total_SolidCD) final
	Store the total (inviscid + viscous) non dimensional drag coefficient.
void	SetTotal_ReverseFlow (su2double val_Total_ReverseFlow) final
	Store the total (inviscid + viscous) non dimensional drag coefficient.
void	SetTotal_MFR (su2double val_Total_MFR) final
	Store the total (inviscid + viscous) non dimensional drag coefficient.
void	SetTotal_Prop_Eff (su2double val_Total_Prop_Eff) final
	Store the total (inviscid + viscous) non dimensional drag coefficient.
void	SetTotal_ByPassProp_Eff (su2double val_Total_ByPassProp_Eff) final
	Store the total (inviscid + viscous) non dimensional drag coefficient.
void	SetTotal_Adiab_Eff (su2double val_Total_Adiab_Eff) final
	Store the total (inviscid + viscous) non dimensional drag coefficient.
void	SetTotal_Poly_Eff (su2double val_Total_Poly_Eff) final
	Store the total (inviscid + viscous) non dimensional drag coefficient.
void	SetTotal_IDC (su2double val_Total_IDC) final
	Store the total (inviscid + viscous) non dimensional drag coefficient.
void	SetTotal_IDC_Mach (su2double val_Total_IDC_Mach) final
	Store the total (inviscid + viscous) non dimensional drag coefficient.
void	SetTotal_IDR (su2double val_Total_IDR) final
	Store the total (inviscid + viscous) non dimensional drag coefficient.
void	SetTotal_DC60 (su2double val_Total_DC60) final
	Store the total (inviscid + viscous) non dimensional drag coefficient.
unsigned long	GetDonorGlobalIndex (unsigned short val_marker, unsigned long val_vertex) const final
	Value of the characteristic global index at the boundaries.
void	SetDonorGlobalIndex (unsigned short val_marker, unsigned long val_vertex, unsigned long val_index) final
	Value of the characteristic global index at the boundaries.
void	SetInitialCondition (CGeometry **geometry, CSolver ***solver_container, CConfig *config, unsigned long TimeIter) final
	Set the initial condition for the Euler Equations.
void	SetFreeStream_Solution (const CConfig *config) final
	Set the solution using the Freestream values.
void	InitTurboContainers (CGeometry *geometry, CConfig **config, unsigned short iZone) final
	Initilize turbo containers.
vector< su2double >	GetTurboPrimitive (unsigned short iBlade, unsigned short iSpan, bool INLET) override
	Get Primal variables for turbo performance computation iteration can be executed by multiple threads.
void	SetFreeStream_TurboSolution (CConfig *config) final
	Set the solution using the Freestream values.
void	PreprocessAverage (CSolver **solver, CGeometry *geometry, CConfig *config, unsigned short marker_flag) final
	It computes average quantities along the span for turbomachinery analysis.
void	TurboAverageProcess (CSolver **solver, CGeometry *geometry, CConfig *config, unsigned short marker_flag) final
	It computes average quantities along the span for turbomachinery analysis.
void	ComputeTurboBladePerformance (CGeometry *geometry, CConfig *config, unsigned short iBlade) final
void	MixedOut_Average (CConfig *config, su2double val_init_pressure, const su2double *val_Averaged_Flux, const su2double *val_normal, su2double &pressure_mix, su2double &density_mix)
	it performs a mixed out average of the nodes of a boundary.
void	GatherInOutAverageValues (CConfig *config, CGeometry *geometry) final
	It gathers into the master node average quantities at inflow and outflow needed for turbomachinery analysis.
void	ComputeTurboVelocity (const su2double *cartesianVelocity, const su2double *turboNormal, su2double *turboVelocity, unsigned short marker_flag, TURBOMACHINERY_TYPE kind_turb)
	it take a velocity in the cartesian reference of framework and transform into the turbomachinery frame of reference.
std::shared_ptr< CTurboOutput >	GetTurboBladePerformance () const final
void	ComputeBackVelocity (const su2double *turboVelocity, const su2double *turboNormal, su2double *cartesianVelocity, unsigned short marker_flag, TURBOMACHINERY_TYPE kind_turb)
	it take a velocity in the cartesian reference of framework and transform into the turbomachinery frame of reference.
su2double	GetAverageDensity (unsigned short valMarker, unsigned short valSpan) const final
	Provide the average density at the boundary of interest.
su2double	GetAveragePressure (unsigned short valMarker, unsigned short valSpan) const final
	Provide the average pressure at the boundary of interest.
const su2double *	GetAverageTurboVelocity (unsigned short valMarker, unsigned short valSpan) const final
	Provide the average turbo velocity average at the boundary of interest.
su2double	GetAverageNu (unsigned short valMarker, unsigned short valSpan) const final
	Provide the average density at the boundary of interest.
su2double	GetAverageKine (unsigned short valMarker, unsigned short valSpan) const final
	Provide the average density at the boundary of interest.
su2double	GetAverageOmega (unsigned short valMarker, unsigned short valSpan) const final
	Provide the average density at the boundary of interest.
su2double	GetDensityIn (unsigned short inMarkerTP, unsigned short valSpan) const final
	Provide the inlet density to check convergence of conservative mixing-plane.
su2double	GetPressureIn (unsigned short inMarkerTP, unsigned short valSpan) const final
	Provide the inlet pressure to check convergence of conservative mixing-plane.
const su2double *	GetTurboVelocityIn (unsigned short inMarkerTP, unsigned short valSpan) const final
	Provide the inlet normal velocity to check convergence of conservative mixing-plane.
su2double	GetDensityOut (unsigned short inMarkerTP, unsigned short valSpan) const final
	Provide the outlet density to check convergence of conservative mixing-plane.
su2double	GetPressureOut (unsigned short inMarkerTP, unsigned short valSpan) const final
	Provide the outlet pressure to check convergence of conservative mixing-plane.
const su2double *	GetTurboVelocityOut (unsigned short inMarkerTP, unsigned short valSpan) const final
	Provide the outlet normal velocity to check convergence of conservative mixing-plane.
su2double	GetKineIn (unsigned short inMarkerTP, unsigned short valSpan) const final
	Provide the inlet turbulent kei to check convergence of conservative mixing-plane.
su2double	GetOmegaIn (unsigned short inMarkerTP, unsigned short valSpan) const final
	Provide the inlet turbulent omega to check convergence of conservative mixing-plane.
su2double	GetNuIn (unsigned short inMarkerTP, unsigned short valSpan) const final
	Provide the inlet turbulent nu to check convergence of conservative mixing-plane.
su2double	GetKineOut (unsigned short inMarkerTP, unsigned short valSpan) const final
	Provide the outlet turbulent kei to check convergence of conservative mixing-plane.
su2double	GetOmegaOut (unsigned short inMarkerTP, unsigned short valSpan) const final
	Provide the outlet turbulent omega to check convergence of conservative mixing-plane.
su2double	GetNuOut (unsigned short inMarkerTP, unsigned short valSpan) const final
	Provide the outlet turbulent nu to check convergence of conservative mixing-plane.
void	SetDensityIn (su2double value, unsigned short inMarkerTP, unsigned short valSpan) final
	Set inlet density.
void	SetPressureIn (su2double value, unsigned short inMarkerTP, unsigned short valSpan) final
	Set inlet pressure.
void	SetTurboVelocityIn (const su2double *value, unsigned short inMarkerTP, unsigned short valSpan) final
	Set inlet normal velocity.
void	SetDensityOut (su2double value, unsigned short inMarkerTP, unsigned short valSpan) final
	Set outlet density.
void	SetPressureOut (su2double value, unsigned short inMarkerTP, unsigned short valSpan) final
	Set outlet pressure.
void	SetTurboVelocityOut (const su2double *value, unsigned short inMarkerTP, unsigned short valSpan) final
	Set outlet normal velocity.
void	SetKineIn (su2double value, unsigned short inMarkerTP, unsigned short valSpan) final
	Set inlet turbulent kei.
void	SetOmegaIn (su2double value, unsigned short inMarkerTP, unsigned short valSpan) final
	Set inlet turbulent omega.
void	SetNuIn (su2double value, unsigned short inMarkerTP, unsigned short valSpan) final
	Set inlet turbulent Nu.
void	SetKineOut (su2double value, unsigned short inMarkerTP, unsigned short valSpan) final
	Set outlet turbulent kei.
void	SetOmegaOut (su2double value, unsigned short inMarkerTP, unsigned short valSpan) final
	Set Outlet turbulent omega.
void	SetNuOut (su2double value, unsigned short inMarkerTP, unsigned short valSpan) final
	Set outlet turbulent Nu.
void	PrintVerificationError (const CConfig *config) const final
	Print verification error to screen.
bool	GetHasHybridParallel () const final
	The Euler and NS solvers support MPI+OpenMP.
Public Member Functions inherited from CFVMFlowSolverBase< CEulerVariable, ENUM_REGIME::COMPRESSIBLE >
void	Set_NewSolution () final
	Set the new solution variables to the current solution value for classical RK.
void	LoadRestart (CGeometry **geometry, CSolver ***solver, CConfig *config, int iter, bool update_geo) override
	Load a solution from a restart file.
void	SetInitialCondition (CGeometry **geometry, CSolver ***solver_container, CConfig *config, unsigned long ExtIter) override
	Set the initial condition for the Euler Equations.
void	SetPrimitive_Gradient_GG (CGeometry *geometry, const CConfig *config, bool reconstruction=false) override
	Compute the gradient of the primitive variables using Green-Gauss method, and stores the result in the Gradient_Primitive variable.
void	SetPrimitive_Gradient_LS (CGeometry *geometry, const CConfig *config, bool reconstruction=false) final
	Compute the gradient of the primitive variables using a Least-Squares method, and stores the result in the Gradient_Primitive variable.
void	SetPrimitive_Limiter (CGeometry *geometry, const CConfig *config) final
	Compute the limiter of the primitive variables.
void	ImplicitEuler_Iteration (CGeometry *geometry, CSolver **solver_container, CConfig *config) final
	Implementation of implicit Euler iteration.
void	CompleteImplicitIteration (CGeometry *geometry, CSolver **, CConfig *config) final
	Complete an implicit iteration.
void	SetResidual_DualTime (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iRKStep, unsigned short iMesh, unsigned short RunTime_EqSystem) override
	Set the total residual adding the term that comes from the Dual Time Strategy.
void	SetUniformInlet (const CConfig *config, unsigned short iMarker) final
	Set a uniform inlet profile.
void	SetInletAtVertex (const su2double *val_inlet, unsigned short iMarker, unsigned long iVertex) final
	Store of a set of provided inlet profile values at a vertex.
su2double	GetInletAtVertex (unsigned short iMarker, unsigned long iVertex, const CGeometry *geometry, su2double *val_inlet) const final
	Get the set of values imposed at an inlet.
void	BC_Euler_Wall (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) final
	Impose via the residual the Euler wall boundary condition.
void	MultigridProjectEulerWall (CGeometry *geometry, const CConfig *config, bool use_solution_old) override
	Enforce Euler wall BC on a restricted or prolongated multigrid solution by projecting the momentum to the tangent plane of the wall.
void	BC_Sym_Plane (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) override
	Impose the symmetry boundary condition using the residual.
void	BC_Periodic (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config) final
	Impose a periodic boundary condition by summing contributions from the complete control volume.
void	BC_Fluid_Interface (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config) final
	Impose the interface state across sliding meshes.
void	BC_Custom (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) final
	Impose a custom or verification boundary condition.
su2double	GetDensity_Inf (void) const final
	Compute the density at the infinity.
su2double	GetModVelocity_Inf (void) const final
	Compute 2-norm of the velocity at the infinity.
su2double	GetPressure_Inf (void) const final
	Compute the pressure at the infinity.
su2double	GetTemperature_Inf (void) const
	Get the temperature value at infinity.
su2double	GetVelocity_Inf (unsigned short val_dim) const final
	Get the velocity at the infinity.
su2double *	GetVelocity_Inf (void) final
	Get the velocity at the infinity.
void	SetVelocity_Inf (unsigned short val_dim, su2double val_velocity) final
	Set the velocity at infinity.
su2double	GetDensity_Energy_Inf (void) const final
	Compute the density multiply by energy at the infinity.
void	SetPressure_Inf (su2double p_inf) final
	Set the freestream pressure.
void	SetTemperature_Inf (su2double t_inf) final
	Set the freestream temperature.
void	SetDensity_Inf (su2double rho_inf) final
	Set the freestream temperature.
su2double	GetViscosity_Inf (void) const final
	Compute the viscosity at the infinity.
su2double	GetTke_Inf (void) const final
	Get the turbulent kinetic energy at the infinity.
su2double	GetOmega_Max (void) const final
	Get the max Omega.
su2double	GetStrainMag_Max (void) const final
	Get the max Strain rate magnitude.
su2double	GetCL_Inv (unsigned short val_marker) const final
	Provide the non dimensional lift coefficient (inviscid contribution).
su2double	GetCD_Inv (unsigned short val_marker) const final
	Provide the non dimensional drag coefficient (inviscid contribution).
su2double	GetSurface_CL (unsigned short val_marker) const final
	Provide the non dimensional lift coefficient.
su2double	GetSurface_CD (unsigned short val_marker) const final
	Provide the non dimensional drag coefficient.
su2double	GetSurface_CSF (unsigned short val_marker) const final
	Provide the non dimensional side-force coefficient.
su2double	GetSurface_CEff (unsigned short val_marker) const final
	Provide the non dimensional side-force coefficient.
su2double	GetSurface_CFx (unsigned short val_marker) const final
	Provide the non dimensional x force coefficient.
su2double	GetSurface_CFy (unsigned short val_marker) const final
	Provide the non dimensional y force coefficient.
su2double	GetSurface_CFz (unsigned short val_marker) const final
	Provide the non dimensional z force coefficient.
su2double	GetSurface_CMx (unsigned short val_marker) const final
	Provide the non dimensional x moment coefficient.
su2double	GetSurface_CMy (unsigned short val_marker) const final
	Provide the non dimensional y moment coefficient.
su2double	GetSurface_CMz (unsigned short val_marker) const final
	Provide the non dimensional z moment coefficient.
su2double	GetSurface_CL_Inv (unsigned short val_marker) const final
	Provide the non dimensional lift coefficient.
su2double	GetSurface_CD_Inv (unsigned short val_marker) const final
	Provide the non dimensional drag coefficient.
su2double	GetSurface_CSF_Inv (unsigned short val_marker) const final
	Provide the non dimensional side-force coefficient.
su2double	GetSurface_CEff_Inv (unsigned short val_marker) const final
	Provide the non dimensional side-force coefficient.
su2double	GetSurface_CFx_Inv (unsigned short val_marker) const final
	Provide the non dimensional x force coefficient.
su2double	GetSurface_CFy_Inv (unsigned short val_marker) const final
	Provide the non dimensional y force coefficient.
su2double	GetSurface_CFz_Inv (unsigned short val_marker) const final
	Provide the non dimensional z force coefficient.
su2double	GetSurface_CMx_Inv (unsigned short val_marker) const final
	Provide the non dimensional x moment coefficient.
su2double	GetSurface_CMy_Inv (unsigned short val_marker) const final
	Provide the non dimensional y moment coefficient.
su2double	GetSurface_CMz_Inv (unsigned short val_marker) const final
	Provide the non dimensional z moment coefficient.
su2double	GetSurface_CL_Mnt (unsigned short val_marker) const final
	Provide the non dimensional lift coefficient.
su2double	GetSurface_CD_Mnt (unsigned short val_marker) const final
	Provide the non dimensional drag coefficient.
su2double	GetSurface_CSF_Mnt (unsigned short val_marker) const final
	Provide the non dimensional side-force coefficient.
su2double	GetSurface_CEff_Mnt (unsigned short val_marker) const final
	Provide the non dimensional side-force coefficient.
su2double	GetSurface_CFx_Mnt (unsigned short val_marker) const final
	Provide the non dimensional x force coefficient.
su2double	GetSurface_CFy_Mnt (unsigned short val_marker) const final
	Provide the non dimensional y force coefficient.
su2double	GetSurface_CFz_Mnt (unsigned short val_marker) const final
	Provide the non dimensional z force coefficient.
su2double	GetSurface_CMx_Mnt (unsigned short val_marker) const final
	Provide the non dimensional x moment coefficient.
su2double	GetSurface_CMy_Mnt (unsigned short val_marker) const final
	Provide the non dimensional y moment coefficient.
su2double	GetSurface_CMz_Mnt (unsigned short val_marker) const final
	Provide the non dimensional z moment coefficient.
su2double	GetCSF_Inv (unsigned short val_marker) const final
	Provide the non dimensional sideforce coefficient (inviscid contribution).
su2double	GetCEff_Inv (unsigned short val_marker) const final
	Provide the non dimensional efficiency coefficient (inviscid contribution).
su2double	GetTotal_CSF () const final
	Provide the total (inviscid + viscous) non dimensional sideforce coefficient.
su2double	GetTotal_CEff () const final
	Provide the total (inviscid + viscous) non dimensional efficiency coefficient.
su2double	GetAeroCoeffsReferenceForce () const final
	Get the reference force used to compute CL, CD, etc.
su2double	GetReferenceDynamicPressure () const final
	Get the reference dynamic pressure, for Cp, Cf, etc.
su2double	GetTotal_CL () const final
	Provide the total (inviscid + viscous) non dimensional lift coefficient.
su2double	GetTotal_CD () const final
	Provide the total (inviscid + viscous) non dimensional drag coefficient.
su2double	GetTotal_CMx () const final
	Provide the total (inviscid + viscous) non dimensional x moment coefficient.
su2double	GetTotal_CMy () const final
	Provide the total (inviscid + viscous) non dimensional y moment coefficient.
su2double	GetTotal_CMz () const final
	Provide the total (inviscid + viscous) non dimensional z moment coefficient.
su2double	GetTotal_CoPx () const final
	Provide the total (inviscid + viscous) non dimensional x moment coefficient.
su2double	GetTotal_CoPy () const final
	Provide the total (inviscid + viscous) non dimensional y moment coefficient.
su2double	GetTotal_CoPz () const final
	Provide the total (inviscid + viscous) non dimensional z moment coefficient.
su2double	GetTotal_CFx () const final
	Provide the total (inviscid + viscous) non dimensional x force coefficient.
su2double	GetTotal_CFy () const final
	Provide the total (inviscid + viscous) non dimensional y force coefficient.
su2double	GetTotal_CFz () const final
	Provide the total (inviscid + viscous) non dimensional z force coefficient.
su2double	GetTotal_CT () const final
	Provide the total (inviscid + viscous) non dimensional thrust coefficient.
void	SetTotal_CT (su2double val_Total_CT) final
	Store the total (inviscid + viscous) non dimensional thrust coefficient.
su2double	GetTotal_CQ () const final
	Provide the total (inviscid + viscous) non dimensional torque coefficient.
void	SetTotal_CQ (su2double val_Total_CQ) final
	Store the total (inviscid + viscous) non dimensional torque coefficient.
su2double	GetTotal_CMerit () const final
	Provide the total (inviscid + viscous) non dimensional rotor Figure of Merit.
void	SetTotal_CD (su2double val_Total_CD) final
	Store the total (inviscid + viscous) non dimensional drag coefficient.
void	SetTotal_CL (su2double val_Total_CL) final
	Store the total (inviscid + viscous) non dimensional lift coefficient.
su2double	GetAllBound_CL_Inv () const final
	Get the inviscid contribution to the lift coefficient.
su2double	GetAllBound_CD_Inv () const final
	Get the inviscid contribution to the drag coefficient.
su2double	GetAllBound_CSF_Inv () const final
	Get the inviscid contribution to the sideforce coefficient.
su2double	GetAllBound_CEff_Inv () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CMx_Inv () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CMy_Inv () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CMz_Inv () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CoPx_Inv () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CoPy_Inv () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CoPz_Inv () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CFx_Inv () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CFy_Inv () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CFz_Inv () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CL_Mnt () const final
	Get the inviscid contribution to the lift coefficient.
su2double	GetAllBound_CD_Mnt () const final
	Get the inviscid contribution to the drag coefficient.
su2double	GetAllBound_CSF_Mnt () const final
	Get the inviscid contribution to the sideforce coefficient.
su2double	GetAllBound_CEff_Mnt () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CMx_Mnt () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CMy_Mnt () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CMz_Mnt () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CoPx_Mnt () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CoPy_Mnt () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CoPz_Mnt () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CFx_Mnt () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CFy_Mnt () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CFz_Mnt () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetSurface_CL_Visc (unsigned short val_marker) const final
	Provide the non dimensional lift coefficient.
su2double	GetSurface_CD_Visc (unsigned short val_marker) const final
	Provide the non dimensional drag coefficient.
su2double	GetSurface_CSF_Visc (unsigned short val_marker) const final
	Provide the non dimensional side-force coefficient.
su2double	GetSurface_CEff_Visc (unsigned short val_marker) const final
	Provide the non dimensional side-force coefficient.
su2double	GetSurface_CFx_Visc (unsigned short val_marker) const final
	Provide the non dimensional x force coefficient.
su2double	GetSurface_CFy_Visc (unsigned short val_marker) const final
	Provide the non dimensional y force coefficient.
su2double	GetSurface_CFz_Visc (unsigned short val_marker) const final
	Provide the non dimensional z force coefficient.
su2double	GetSurface_CMx_Visc (unsigned short val_marker) const final
	Provide the non dimensional x moment coefficient.
su2double	GetSurface_CMy_Visc (unsigned short val_marker) const final
	Provide the non dimensional y moment coefficient.
su2double	GetSurface_CMz_Visc (unsigned short val_marker) const final
	Provide the non dimensional z moment coefficient.
su2double	GetAllBound_CL_Visc () const final
	Get the inviscid contribution to the lift coefficient.
su2double	GetAllBound_CD_Visc () const final
	Get the inviscid contribution to the drag coefficient.
su2double	GetAllBound_CSF_Visc () const final
	Get the inviscid contribution to the sideforce coefficient.
su2double	GetAllBound_CEff_Visc () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CMx_Visc () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CMy_Visc () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CMz_Visc () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CoPx_Visc () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CoPy_Visc () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CoPz_Visc () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CFx_Visc () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CFy_Visc () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetAllBound_CFz_Visc () const final
	Get the inviscid contribution to the efficiency coefficient.
su2double	GetCL_Visc (unsigned short val_marker) const final
	Get the non dimensional lift coefficient (viscous contribution).
su2double	GetCSF_Visc (unsigned short val_marker) const final
	Get the non dimensional sideforce coefficient (viscous contribution).
su2double	GetCD_Visc (unsigned short val_marker) const final
	Get the non dimensional drag coefficient (viscous contribution).
su2double	GetSurface_HF_Visc (unsigned short val_marker) const final
	Get the total heat flux.
su2double	GetSurface_MaxHF_Visc (unsigned short val_marker) const final
	Get the maximum (per surface) heat flux.
void	SetTotal_CpDiff (su2double val_pressure) final
	Set the value of the Equivalent Area coefficient.
void	SetTotal_HeatFluxDiff (su2double val_heat) final
	Set the value of the Equivalent Area coefficient.
void	SetTotal_CEquivArea (su2double val_equiv) final
	Set the value of the Equivalent Area coefficient.
void	SetTotal_CNearFieldOF (su2double val_cnearfieldpress) final
	Set the value of the Near-Field pressure oefficient.
su2double	GetTotal_CpDiff () const final
	Provide the total (inviscid + viscous) non dimensional Equivalent Area coefficient.
su2double	GetTotal_HeatFluxDiff () const final
	Provide the total (inviscid + viscous) non dimensional Equivalent Area coefficient.
su2double	GetTotal_CEquivArea () const final
	Provide the total (inviscid + viscous) non dimensional Equivalent Area coefficient.
su2double	GetTotal_HeatFlux () const final
	Provide the total heat load.
su2double	GetTotal_MaxHeatFlux () const final
	Provide the total heat load.
void	SetTotal_HeatFlux (su2double val_Total_Heat) final
	Store the total heat load.
void	SetTotal_MaxHeatFlux (su2double val_Total_MaxHeat) final
	Store the total heat load.
su2double	GetCPressure (unsigned short val_marker, unsigned long val_vertex) const final
	Provide the Pressure coefficient.
su2double	GetCPressureTarget (unsigned short val_marker, unsigned long val_vertex) const final
	Provide the Target Pressure coefficient.
void	SetCPressureTarget (unsigned short val_marker, unsigned long val_vertex, su2double val_pressure) final
	Set the value of the target Pressure coefficient.
su2double *	GetCharacPrimVar (unsigned short val_marker, unsigned long val_vertex) final
	Value of the characteristic variables at the boundaries.
void	SetCharacPrimVar (unsigned short val_marker, unsigned long val_vertex, unsigned short val_var, su2double val_value) final
	Value of the characteristic variables at the boundaries.
su2double	GetInletTtotal (unsigned short val_marker, unsigned long val_vertex) const final
	Value of the total temperature at an inlet boundary.
su2double	GetInletPtotal (unsigned short val_marker, unsigned long val_vertex) const final
	Value of the total pressure at an inlet boundary.
su2double	GetInletFlowDir (unsigned short val_marker, unsigned long val_vertex, unsigned short val_dim) const final
	A component of the unit vector representing the flow direction at an inlet boundary.
void	SetInletTtotal (unsigned short val_marker, unsigned long val_vertex, su2double val_ttotal) final
	Set the value of the total temperature at an inlet boundary.
void	SetInletPtotal (unsigned short val_marker, unsigned long val_vertex, su2double val_ptotal) final
	Set the value of the total pressure at an inlet boundary.
void	SetInletFlowDir (unsigned short val_marker, unsigned long val_vertex, unsigned short val_dim, su2double val_flowdir) final
	Set a component of the unit vector representing the flow direction at an inlet boundary.
void	UpdateCustomBoundaryConditions (CGeometry **geometry_container, CSolver ***solver_container, CConfig *config) final
	Update the multi-grid structure for the customized boundary conditions.
void	UpdateFarfieldVelocity (const CConfig *config) final
	Updates the components of the farfield velocity vector.
void	ComputeVerificationError (CGeometry *geometry, CConfig *config) final
	Compute the global error measures (L2, Linf) for verification cases.
void	Pressure_Forces (const CGeometry *geometry, const CConfig *config) final
	Compute the pressure forces and all the adimensional coefficients.
void	Momentum_Forces (const CGeometry *geometry, const CConfig *config) final
	Compute the pressure forces and all the adimensional coefficients.
void	Friction_Forces (const CGeometry *geometry, const CConfig *config) final
	Compute the viscous forces and all the addimensional coefficients.
virtual void	Buffet_Monitoring (const CGeometry *geometry, const CConfig *config)
	Compute the buffet sensor.
void	SetSlidingStateStructure (unsigned short val_marker, unsigned long val_vertex) final
	Allocates the final pointer of SlidingState depending on how many donor vertex donate to it. That number is stored in SlidingStateNodes[val_marker][val_vertex].
void	SetSlidingState (unsigned short val_marker, unsigned long val_vertex, unsigned short val_state, unsigned long donor_index, su2double component) final
	Set the outer state for fluid interface nodes.
void	SetnSlidingStates (unsigned short val_marker, unsigned long val_vertex, int value) final
	Set the number of outer state for fluid interface nodes.
int	GetnSlidingStates (unsigned short val_marker, unsigned long val_vertex) const final
	Get the number of outer state for fluid interface nodes.
su2double	GetSlidingState (unsigned short val_marker, unsigned long val_vertex, unsigned short val_state, unsigned long donor_index) const final
	Get the outer state for fluid interface nodes.
void	SetConjugateHeatVariable (unsigned short val_marker, unsigned long val_vertex, unsigned short pos_var, su2double relaxation_factor, su2double val_var) final
	Set the conjugate heat variables.
su2double	GetConjugateHeatVariable (unsigned short val_marker, unsigned long val_vertex, unsigned short pos_var) const final
	Set the conjugate heat variables.
su2double	GetCSkinFriction (unsigned short val_marker, unsigned long val_vertex, unsigned short val_dim) const final
	Get the skin friction coefficient.
su2double	GetWallShearStress (unsigned short val_marker, unsigned long val_vertex) const final
	Get the wall shear stress.
su2double	GetHeatFlux (unsigned short val_marker, unsigned long val_vertex) const final
	Get the heat flux.
su2double	GetHeatFluxTarget (unsigned short val_marker, unsigned long val_vertex) const final
	Get the skin friction coefficient.
void	SetHeatFluxTarget (unsigned short val_marker, unsigned long val_vertex, su2double val_heat) final
	Set the value of the target Pressure coefficient.
su2double	GetYPlus (unsigned short val_marker, unsigned long val_vertex) const final
	Get the y plus.
su2double	GetUTau (unsigned short val_marker, unsigned long val_vertex) const final
	Get the u_tau .
su2double	GetEddyViscWall (unsigned short val_marker, unsigned long val_vertex) const final
	Get the eddy viscosity at the wall (wall functions).
const su2activevector *	GetEdgeMassFluxes () const final
	Get the mass fluxes across the edges (computed and stored during the discretization of convective fluxes).
Public Member Functions inherited from CSolver
	CSolver (LINEAR_SOLVER_MODE linear_solver_mode=LINEAR_SOLVER_MODE::STANDARD)
	Constructor of the class.
virtual	~CSolver (void)
	Destructor of the class.
CVariable *	GetNodes ()
	Allow outside access to the nodes of the solver, containing conservatives, primitives, etc.
const CVariable *	GetNodes () const
bool	HasPeriodicRotation (const CConfig &config) const
void	GetCommCountAndType (const CConfig *config, MPI_QUANTITIES commType, unsigned short &COUNT_PER_POINT, COMM_TYPE &MPI_TYPE) const
	Helper function to define the type and number of variables per point for each communication type.
void	InitiateComms (CGeometry *geometry, const CConfig *config, MPI_QUANTITIES commType)
	Routine to load a solver quantity into the data structures for MPI point-to-point communication and to launch non-blocking sends and recvs.
void	CompleteComms (CGeometry *geometry, const CConfig *config, MPI_QUANTITIES commType)
	Routine to complete the set of non-blocking communications launched by InitiateComms() and unpacking of the data in the solver class.
void	GetPeriodicCommCountAndType (const CConfig *config, unsigned short commType, unsigned short &COUNT_PER_POINT, COMM_TYPE &MPI_TYPE, unsigned short &ICOUNT, unsigned short &JCOUNT) const
	Helper function to define the type and number of variables per point for each communication type.
void	InitiatePeriodicComms (CGeometry *geometry, const CConfig *config, unsigned short val_periodic_index, unsigned short commType)
	Routine to load a solver quantity into the data structures for MPI periodic communication and to launch non-blocking sends and recvs.
void	CompletePeriodicComms (CGeometry *geometry, const CConfig *config, unsigned short val_periodic_index, unsigned short commType)
	Routine to complete the set of non-blocking periodic communications launched by InitiatePeriodicComms() and unpacking of the data in the solver class.
void	SetIterLinSolver (unsigned short val_iterlinsolver)
	Set number of linear solver iterations.
void	SetResLinSolver (su2double val_reslinsolver)
	Set the final linear solver residual.
void	SetResidual_RMS (const CGeometry *geometry, const CConfig *config, bool force=false)
	Set the value of the max residual and RMS residual.
void	SetResidual_BGS (const CGeometry *geometry, const CConfig *config)
	Communicate the value of the max residual and RMS residual.
void	ComputeResidual_Multizone (const CGeometry *geometry, const CConfig *config)
	Set the value of the max residual and RMS residual.
virtual void	SetDualTime_Mesh (void)
	Move the mesh in time.
bool	GetAdjoint (void) const
	Get information whether the initialization is an adjoint solver or not.
unsigned short	GetIterLinSolver (void) const
	Get number of linear solver iterations.
su2double	GetResLinSolver (void) const
	Get the final linear solver residual.
su2double	GetMax_Delta_Time (void) const
	Get the value of the maximum delta time.
su2double	GetMin_Delta_Time (void) const
	Get the value of the minimum delta time.
su2double	GetMax_CFL_Local (void) const
	Get the value of the maximum local CFL number.
su2double	GetMin_CFL_Local (void) const
	Get the value of the minimum local CFL number.
su2double	GetAvg_CFL_Local (void) const
	Get the value of the average local CFL number.
void	SetCFL_Local_Stats (su2double val_cfl)
	Set min/max/avg local CFL summary statistics.
unsigned short	GetnVar (void) const
	Get the number of variables of the problem.
unsigned short	GetnPrimVar (void) const
	Get the number of variables of the problem.
unsigned short	GetnPrimVarGrad (void) const
	Get the number of variables of the problem.
unsigned short	GetnSecondaryVar (void) const
	Get the number of variables of the problem.
unsigned short	GetnOutputVariables (void) const
	Get the number of variables of the problem.
su2double	GetRes_RMS (unsigned short val_var) const
	Get the maximal residual, this is useful for the convergence history.
su2double	GetRes_Max (unsigned short val_var) const
	Get the maximal residual, this is useful for the convergence history.
su2double	GetRes_BGS (unsigned short val_var) const
	Get the residual for BGS subiterations.
su2double	GetRes_Max_BGS (unsigned short val_var) const
	Get the maximal residual for BGS subiterations.
virtual su2double	GetRes_FEM (unsigned short val_var) const
	Get the residual for FEM structural analysis.
unsigned long	GetPoint_Max (unsigned short val_var) const
	Get the maximal residual, this is useful for the convergence history.
const su2double *	GetPoint_Max_Coord (unsigned short val_var) const
	Get the location of the maximal residual, this is useful for the convergence history.
unsigned long	GetPoint_Max_BGS (unsigned short val_var) const
	Get the maximal residual, this is useful for the convergence history.
const su2double *	GetPoint_Max_Coord_BGS (unsigned short val_var) const
	Get the location of the maximal residual, this is useful for the convergence history.
void	SetRotatingFrame_GCL (CGeometry *geometry, const CConfig *config)
	Set Value of the residual due to the Geometric Conservation Law (GCL) for steady rotating frame problems.
void	SetAuxVar_Gradient_GG (CGeometry *geometry, const CConfig *config)
	Compute the Green-Gauss gradient of the auxiliary variable.
void	SetAuxVar_Gradient_LS (CGeometry *geometry, const CConfig *config)
	Compute the Least Squares gradient of the auxiliary variable.
void	Add_External_To_Solution ()
	Add External to Solution vector.
void	Add_Solution_To_External ()
	Add the current Solution vector to External.
void	Update_Cross_Term (CConfig *config, su2passivematrix &cross_term)
	Update a given cross-term with relaxation and the running total (External).
void	SetSolution_Gradient_GG (CGeometry *geometry, const CConfig *config, short idxVel, bool reconstruction=false)
	Compute the Green-Gauss gradient of the solution.
void	SetSolution_Gradient_LS (CGeometry *geometry, const CConfig *config, short idxVel, bool reconstruction=false)
	Compute the Least Squares gradient of the solution.
void	SetGridVel_Gradient (CGeometry *geometry, const CConfig *config) const
	Compute the Least Squares gradient of the grid velocity.
void	SetSolution_Limiter (CGeometry *geometry, const CConfig *config)
	Compute slope limiter.
virtual su2double	GetFlameThickness () const
	A virtual member.
su2double	MUSCL_Reconstruction (const su2double *grad, const su2double *vector_ij, su2double delta_ij, su2double kappa, su2double ramp_val) const
	Compute the projection of a variable for MUSCL reconstruction.
virtual void	Set_OldSolution ()
	Set the old solution variables to the current solution value for Runge-Kutta iteration. It is a virtual function, because for the DG-FEM solver a different version is needed.
void	Restart_OldGeometry (CGeometry *geometry, CConfig *config) const
	Load the geometries at the previous time states n and nM1.
virtual void	CheckTimeSynchronization (CConfig *config, const su2double TimeSync, su2double &timeEvolved, bool &syncTimeReached)
	A virtual member.
virtual void	ProcessTaskList_DG (CGeometry *geometry, CSolver **solver_container, CNumerics **numerics, CConfig *config, unsigned short iMesh)
	A virtual member.
virtual void	ADER_SpaceTimeIntegration (CGeometry *geometry, CSolver **solver_container, CNumerics **numerics, CConfig *config, unsigned short iMesh, unsigned short RunTime_EqSystem)
	A virtual member.
virtual void	ComputeSpatialJacobian (CGeometry *geometry, CSolver **solver_container, CNumerics **numerics, CConfig *config, unsigned short iMesh, unsigned short RunTime_EqSystem)
	A virtual member.
virtual void	Postprocessing (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh)
	A virtual member.
virtual void	Postprocessing (CGeometry *geometry, CConfig *config, CNumerics **numerics, bool of_comp_mode=false)
	A virtual member, overloaded.
virtual void	Preprocessing (CGeometry *geometry, CSolver **solver_container, CConfig *config, CNumerics **numerics, unsigned short iMesh, unsigned long Iteration, unsigned short RunTime_EqSystem, bool Output)
	A virtual member overloaded.
virtual void	ComputeEdgeMassFluxesRhieChow (CGeometry *geometry, CSolver **solver_container, CConfig *config)
	A virtual member.
virtual void	ApplyPressureVelocityCorrection (CGeometry *geometry, CSolver **solver_container, CConfig *config)
	A virtual member.
virtual void	Set_Heatflux_Areas (CGeometry *geometry, CConfig *config)
	A virtual member.
virtual void	BC_Clamped (CGeometry *geometry, const CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_Clamped_Post (CGeometry *geometry, const CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_Sym_Plane (CGeometry *geometry, const CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_DispDir (CGeometry *geometry, const CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_Normal_Displacement (CGeometry *geometry, CNumerics *numerics, const CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_Normal_Load (CGeometry *geometry, const CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_Dir_Load (CGeometry *geometry, const CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_Sine_Load (CGeometry *geometry, const CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_Damper (CGeometry *geometry, const CConfig *config, unsigned short val_marker)
	A virtual member.
virtual void	BC_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_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_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.
void	AdaptCFLNumber (CGeometry **geometry, CSolver ***solver_container, CConfig *config)
	Adapt the CFL number based on the local under-relaxation parameters computed for each nonlinear iteration.
void	ResetCFLAdapt ()
	Reset the local CFL adaption variables.
virtual void	ImplicitNewmark_Iteration (const CGeometry *geometry, CNumerics **numerics, const CConfig *config)
	A virtual member.
virtual void	ImplicitNewmark_Update (const CGeometry *geometry, const CConfig *config)
	A virtual member.
virtual void	ImplicitNewmark_Relaxation (const CGeometry *geometry, const CConfig *config)
	A virtual member.
virtual void	GeneralizedAlpha_Iteration (const CGeometry *geometry, CNumerics **numerics, const CConfig *config)
	A virtual member.
virtual void	GeneralizedAlpha_UpdateDisp (const CGeometry *geometry, const CConfig *config)
	A virtual member.
virtual void	GeneralizedAlpha_UpdateSolution (const CGeometry *geometry, const CConfig *config)
	A virtual member.
virtual void	GeneralizedAlpha_UpdateLoads (const CGeometry *geometry, const CConfig *config)
	A virtual member.
virtual void	Heat_Fluxes (CGeometry *geometry, CSolver **solver_container, CConfig *config)
	A virtual member.
virtual void	SetCSensitivity (unsigned short val_marker, unsigned long val_vertex, su2double val_sensitivity)
	A virtual member.
virtual void	SetForceProj_Vector (CGeometry *geometry, CSolver **solver_container, CConfig *config)
	A virtual member.
virtual void	Inviscid_Sensitivity (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config)
	A virtual member.
virtual void	Smooth_Sensitivity (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config)
	A virtual member.
virtual void	Viscous_Sensitivity (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config)
	A virtual member.
su2double	GetTotal_ComboObj () const
	Provide the total "combo" objective (weighted sum of other values).
void	SetTotal_Custom_ObjFunc (su2double value)
	Sets the value of the custom objective function.
virtual su2double	GetSurface_Buffet_Metric (unsigned short val_marker) const
	A virtual member.
virtual su2double	GetTotal_AvgTemperature () const
	A virtual member.
virtual su2double	GetTotal_CFEA () const
	A virtual member.
virtual su2double	GetTotal_OFRefGeom () const
	A virtual member.
virtual su2double	GetTotal_OFRefNode () const
	A virtual member.
virtual su2double	GetTotal_OFVolFrac () const
	A virtual member.
virtual su2double	GetTotal_OFDiscreteness () const
	Retrieve the value of the discreteness objective function.
virtual su2double	GetTotal_OFCompliance () const
	A virtual member.
virtual su2double	GetTotal_OFStressPenalty () const
	A virtual member.
virtual bool	IsElementBased (void) const
	A virtual member.
virtual void	SetTotal_CFEA (su2double val_cfea)
	A virtual member.
virtual void	SetTotal_OFRefGeom (su2double val_ofrefgeom)
	A virtual member.
virtual void	SetTotal_OFRefNode (su2double val_ofrefnode)
	A virtual member.
virtual su2double	GetTotal_Buffet_Metric () const
	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 su2double *	GetVecSolDOFs (void)
	A virtual member.
virtual unsigned long	GetnDOFsGlobal (void) const
	A virtual member.
virtual su2double	GetAverageMassFlowRate (unsigned short valMarker) const
	virtual member
virtual void	DeformMesh (CGeometry **geometry, CNumerics **numerics, CConfig *config)
	A virtual member.
virtual void	DeformMesh (CGeometry *geometry, CNumerics **numerics, CConfig *config)
	A virtual member.
virtual void	SetMesh_Stiffness (CNumerics **numerics, CConfig *config)
	A virtual member.
virtual void	ApplyGradientSmoothingVolume (CGeometry *geometry, CNumerics *numerics, const CConfig *config)
	A virtual member.
virtual void	ApplyGradientSmoothingSurface (CGeometry *geometry, CNumerics *numerics, const CConfig *config)
	A virtual member.
virtual void	ApplyGradientSmoothingDV (CGeometry *geometry, CNumerics *numerics, CSurfaceMovement *surface_movement, CVolumetricMovement *grid_movement, CConfig *config, su2double **Gradient)
	All steps required for smoothing the whole system on DV level in an iterative way.
virtual void	RecordTapeAndCalculateOriginalGradient (CGeometry *geometry, CSurfaceMovement *surface_movement, CVolumetricMovement *grid_movement, CConfig *config, su2double **Gradient)
	A virtual member.
virtual void	ReadSensFromGeometry (const CGeometry *geometry)
	A virtual member.
virtual void	WriteSensToGeometry (CGeometry *geometry) const
	A virtual member.
void	SetImplicitPeriodic (bool val_implicit_periodic)
	Routine that sets the flag controlling implicit treatment for periodic BCs.
void	SetRotatePeriodic (bool val_rotate_periodic)
	Routine that sets the flag controlling solution rotation for periodic BCs.
su2activematrix *	GetPeriodicProjections (const CGeometry &geometry, const CConfig &config)
	Storage for the limiters with rotational periodicity: the min and max, over the edges of the periodic matches of each point, of the reconstruction increments (communicated with PERIODIC_LIM_PRIM_1).
su2double *	GetPeriodicProjection (unsigned long iPoint)
	Reconstruction increment bounds for a periodic receive point, nullptr for other points.
const string &	GetSolverName () const
	Retrieve the solver name for output purposes.
vector< string >	GetSolutionFields () const
	Get the solution fields.
void	ComputeVertexTractions (CGeometry *geometry, const CConfig *config)
	Compute the tractions at the vertices.
su2double	GetVertexTractions (unsigned short iMarker, unsigned long iVertex, unsigned short iDim) const
	Set the adjoints of the vertex tractions.
void	RegisterVertexTractions (CGeometry *geometry, const CConfig *config)
	Register the vertex tractions as output.
void	StoreVertexTractionsAdjoint (unsigned short iMarker, unsigned long iVertex, unsigned short iDim, su2double val_adjoint)
	Store the adjoints of the vertex tractions.
void	SetVertexTractionsAdjoint (CGeometry *geometry, const CConfig *config)
	Set the adjoints of the vertex tractions to the AD structure.
virtual su2double	GetMinimum_Volume () const
	Get minimun volume in the mesh.
virtual su2double	GetMaximum_Volume () const
	Get maximum volume in the mesh.
virtual StreamwisePeriodicValues	GetStreamwisePeriodicValues () const
	Get values for streamwise periodic flow: delta P, m_dot, inlet T, integrated heat, etc.
virtual void	SetMomCoeff (CGeometry *geometry, CSolver **solver_container, CConfig *config, bool periodic, unsigned short iMesh)
	A virtual member.
virtual void	ComputeHbyA (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh)
	A virtual member.
void	SavelibROM (CGeometry *geometry, CConfig *config, bool converged)
	Save snapshot or POD data using libROM.
void	CustomSourceResidual (CGeometry *geometry, CSolver **solver_container, CNumerics **numerics_container, CConfig *config, unsigned short iMesh)

Static Public Member Functions
static void	ComputeConsistentExtrapolation (CFluidModel *fluidModel, unsigned short nDim, su2double *primitive, su2double *secondary)
	Recompute the extrapolated quantities, after MUSCL reconstruction, in a more thermodynamically consistent way.
static void	LowMachPrimitiveCorrection (CFluidModel *fluidModel, unsigned short nDim, su2double *primitive_i, su2double *primitive_j)
	Apply low Mach number correction to the primitives at two points, usually connected by an edge.
Static Public Member Functions inherited from CSolver
static void	MultigridRestriction (const CGeometry &geoFine, const su2activematrix &varsFine, const CGeometry &geoCoarse, su2activematrix &varsCoarse)
	Interpolate variables to a coarser grid level.

Protected Types
using	BaseClass = CFVMFlowSolverBase< CEulerVariable, ENUM_REGIME::COMPRESSIBLE >
Protected Types inherited from CSolver
enum	: size_t { OMP_MIN_SIZE = 32 }

Protected Member Functions
su2double	GetTangGridVelIn (unsigned short val_blade, unsigned long val_span)
su2double	GetTangGridVelOut (unsigned short val_blade, unsigned long val_span)
su2double	GetMixingState (unsigned short val_marker, unsigned long val_span, unsigned short val_state) const final
	Get a component of the donor-side averaged state at a mixing plane interface.
void	SetMixingState (unsigned short val_marker, unsigned long val_span, unsigned short val_state, su2double component) final
	Set a component of the donor-side averaged state at a mixing plane interface nodes.
void	CommonPreprocessing (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh, unsigned short iRKStep, unsigned short RunTime_EqSystem, bool Output)
	Preprocessing actions common to the Euler and NS solvers.
void	SetFarfield_AoA (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh, bool Output)
	Update the AoA and freestream velocity at the farfield.
void	SetUpwind_Ducros_Sensor (CGeometry *geometry, CConfig *config)
	Compute Ducros Sensor for Roe Dissipation.
void	GetPower_Properties (CGeometry *geometry, CConfig *config, unsigned short iMesh, bool Output)
	Compute the Fan face Mach number.
void	Set_MPI_ActDisk (CSolver **solver_container, CGeometry *geometry, CConfig *config)
	Parallelization of Undivided Laplacian.
void	SetActDisk_BCThrust (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh, bool Output)
	Update the AoA and freestream velocity at the farfield.
void	ReadActDisk_InputFile (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh, bool Output)
	Read the actuator disk input file for the VARIABLE_LOAD type.
void	SetActDisk_BEM_VLAD (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh, bool Output)
	Read and update the variable load actuator disk from input file for the BLADE_ELEMENT type.
void	SetMax_Eigenvalue (CGeometry *geometry, const CConfig *config)
	Compute the max eigenvalue.
void	SetUndivided_Laplacian (CGeometry *geometry, const CConfig *config)
	Compute the undivided laplacian for the solution.
void	SetCentered_Dissipation_Sensor (CGeometry *geometry, const CConfig *config)
	Compute the dissipation sensor for centered schemes.
virtual void	SetRoe_Dissipation (CGeometry *geometry, CConfig *config)
	A virtual member.
virtual unsigned long	SetPrimitive_Variables (CSolver **solver_container, const CConfig *config)
	Compute the velocity^2, SoundSpeed, Pressure, Enthalpy, Viscosity.
void	SetCoefficient_Gradients (CConfig *config) const
	Set gradients of coefficients for fixed CL mode.
void	InstantiateEdgeNumerics (const CSolver *const *solvers, const CConfig *config) final
	Instantiate a SIMD numerics object.
void	SetNondimensionalization (CConfig *config, unsigned short iMesh)
	Set the solver nondimensionalization.
void	SetReferenceValues (const CConfig &config) final
	Set reference values for pressure, forces, etc.
Protected Member Functions inherited from CFVMFlowSolverBase< CEulerVariable, ENUM_REGIME::COMPRESSIBLE >
CVariable *	GetBaseClassPointerToNodes () final
	Return nodes to allow CSolver::base_nodes to be set.
	CFVMFlowSolverBase (const CGeometry &geometry, const CConfig &config)
	Protected constructor, this class is not directly instantiable.
void	Allocate (const CConfig &config)
	Allocate member variables.
void	AllocateTerribleLegacyTemporaryVariables ()
	Allocate small member variables that ideally should not be used.
void	CommunicateInitialState (CGeometry *geometry, const CConfig *config)
	Communicate the initial solver state.
void	HybridParallelInitialization (const CConfig &config, CGeometry &geometry)
	Initialize thread parallel variables.
void	PushSolutionBackInTime (unsigned long TimeIter, bool restart, bool rans, CSolver ***solver_container, CGeometry **geometry, CConfig *config)
	Move solution to previous time levels (for restarts).
su2double	EvaluateCommonObjFunc (const CConfig &config) const
	Evaluate common part of objective function to all solvers.
void	EdgeFluxResidual (const CGeometry *geometry, const CSolver *const *solvers, CConfig *config)
	Method to compute convective and viscous residual contribution using vectorized numerics.
void	SumEdgeFluxes (const CGeometry *geometry)
	Sum the edge fluxes for each cell to populate the residual vector, only used on coarse grids.
void	FinalizeResidualComputation (const CGeometry *geometry, bool pausePreacc, unsigned long localCounter, CConfig *config)
	Sums edge fluxes (if required) and computes the global error counter.
void	ComputeAxisymmetricAuxGradients (CGeometry *geometry, const CConfig *config)
	Computes and sets the required auxilliary vars (and gradients) for axisymmetric flow.
virtual CNumerics::ResidualType	Viscous_Residual (unsigned long iEdge, CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config)
	Compute the viscous contribution for a particular edge.
virtual void	Viscous_Residual (CGeometry *geometry, CSolver **solver_container, CNumerics **numerics_container, CConfig *config, unsigned short iMesh, unsigned short iRKStep)
	A virtual member.
CNumerics::ResidualType	Viscous_Residual_impl (unsigned long iEdge, CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config)
void	UpdateJacobian (unsigned long iEdge, unsigned long iPoint, unsigned long jPoint, const CNumerics::ResidualType<> &conv, const CNumerics::ResidualType<> &visc)
	Update the Jacobian for one edge with the fused convective and viscous contributions.
void	LoadRestart_impl (CGeometry **geometry, CSolver ***solver, CConfig *config, int iter, bool update_geo, su2double *RestartSolution=nullptr, unsigned short nVar_Restart=0)
	General implementation to load a flow solution from a restart file.
void	SetTime_Step_impl (const SoundSpeedFunc &soundSpeed, const LambdaViscFunc &lambdaVisc, CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh, unsigned long Iteration)
	Generic implementation to compute the time step based on CFL and conv/visc eigenvalues.
void	SetMax_Eigenvalue_impl (const SoundSpeedFunc &soundSpeed, CGeometry *geometry, const CConfig *config)
	Compute the max eigenvalue, gemeric implementation.
void	SetCentered_Dissipation_Sensor_impl (const SensVarFunc &sensVar, CGeometry *geometry, const CConfig *config)
	Compute the dissipation sensor for centered schemes.
void	Explicit_Iteration_impl (ResidualPrecond &preconditioner, CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iRKStep)
	Generic implementation of explicit iterations with a preconditioner.
void	Explicit_Iteration (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iRKStep)
	Generic implementation of explicit iterations without preconditioner.
void	PrepareImplicitIteration_impl (DiagonalPrecond &preconditioner, CGeometry *geometry, CConfig *config)
	Generic implementation to prepare an implicit iteration with an optional preconditioner applied to the diagonal.
void	ComputeVorticityAndStrainMag (const CConfig &config, const CGeometry *geometry, unsigned short iMesh)
	Evaluate the vorticity and strain rate magnitude.
	~CFVMFlowSolverBase ()
	Destructor.
Protected Member Functions inherited from CSolver
void	SetBaseClassPointerToNodes ()
	Call this method to set "base_nodes" after the "nodes" variable of the derived solver is instantiated.
void	SetUndivided_Laplacian (CGeometry *geometry, const CConfig *config)
	Compute the undivided laplacian for the solution variables.
void	SetVerificationSolution (unsigned short nDim, unsigned short nVar, CConfig *config)
	Allocate the memory for the verification solution, if necessary.
void	ResidualReductions_FromAllThreads (const CGeometry *geometry, const CConfig *config, const su2double *resRMS, const su2double *resMax, const unsigned long *idxMax)
	"Add" local residual variables of all threads to compute global residual variables.
void	SetResToZero ()
	Set the RMS and MAX residual to zero.
void	AddRes_Max (unsigned short val_var, su2double val_residual, unsigned long val_point, const su2double *val_coord)
	Adds the maximal residual, this is useful for the convergence history.
void	AddRes_Max_BGS (unsigned short val_var, su2double val_residual, unsigned long val_point, const su2double *val_coord)
	Adds the maximal residual for BGS subiterations.

Protected Attributes
su2double	Prandtl_Turb = 0.0
	Turbulent Prandtl number.
su2double	AllBound_CEquivArea_Inv =0.0
	equivalent area coefficient (inviscid contribution) for all the boundaries.
vector< su2double >	CEquivArea_Mnt
	Equivalent area (inviscid contribution) for each boundary.
vector< su2double >	CEquivArea_Inv
	Equivalent area (inviscid contribution) for each boundary.
vector< su2double >	Inflow_MassFlow
	Mass flow rate for each boundary.
vector< su2double >	Exhaust_MassFlow
	Mass flow rate for each boundary.
vector< su2double >	Inflow_Pressure
	Fan face pressure for each boundary.
vector< su2double >	Inflow_Mach
	Fan face mach number for each boundary.
vector< su2double >	Inflow_Area
	Boundary total area.
vector< su2double >	Exhaust_Area
	Boundary total area.
vector< su2double >	Exhaust_Pressure
	Fan face pressure for each boundary.
vector< su2double >	Exhaust_Temperature
	Fan face mach number for each boundary.
su2double	Inflow_MassFlow_Total = 0.0
	Mass flow rate for each boundary.
su2double	Exhaust_MassFlow_Total = 0.0
	Mass flow rate for each boundary.
su2double	Inflow_Pressure_Total = 0.0
	Fan face pressure for each boundary.
su2double	Inflow_Mach_Total = 0.0
	Fan face mach number for each boundary.
su2double	InverseDesign = 0.0
	Inverse design functional for each boundary.
vector< vector< unsigned long > >	DonorGlobalIndex
	Value of the donor global index.
vector< su2activematrix >	DonorPrimVar
	Value of the donor variables at each boundary.
vector< vector< su2double > >	ActDisk_DeltaP
	Value of the Delta P.
vector< vector< su2double > >	ActDisk_DeltaP_r
	Value of the DeltaP_r.
vector< vector< su2double > >	ActDisk_Thrust_r
	Value of the Thrust_r.
vector< vector< su2double > >	ActDisk_Torque_r
	Value of the Torque_r.
vector< vector< su2double > >	ActDisk_DeltaT
	Value of the Delta T.
su2activevector	ActDisk_R
	Value of the actuator disk Radius.
su2activematrix	ActDisk_C
	Value of the actuator disk Center.
su2activematrix	ActDisk_Axis
	Value of the actuator disk Axis.
vector< vector< su2double > >	ActDisk_Fa
	Value of the actuator disk Axial Force per Unit Area.
vector< vector< su2double > >	ActDisk_Fx
	Value of the actuator disk X component of the radial and tangential forces per Unit Area resultant.
vector< vector< su2double > >	ActDisk_Fy
	Value of the actuator disk Y component of the radial and tangential forces per Unit Area resultant.
vector< vector< su2double > >	ActDisk_Fz
	Value of the actuator disk Z component of the radial and tangential forces per Unit Area resultant.
vector< vector< su2double > >	ActDisk_Fa_BEM
	Value of the actuator disk Axial Force per Unit Area.
vector< vector< su2double > >	ActDisk_Fx_BEM
	Value of the actuator disk X component of the radial and tangential forces per Unit Area resultant.
vector< vector< su2double > >	ActDisk_Fy_BEM
	Value of the actuator disk Y component of the radial and tangential forces per Unit Area resultant.
vector< vector< su2double > >	ActDisk_Fz_BEM
	Value of the actuator disk Z component of the radial and tangential forces per Unit Area resultant.
su2double	Total_CL_Prev = 0.0
	Total lift coefficient for all the boundaries (fixed lift mode).
su2double	Total_SolidCD = 0.0
	Total drag coefficient for all the boundaries.
su2double	Total_CD_Prev = 0.0
	Total drag coefficient for all the boundaries (fixed lift mode).
su2double	Total_NetThrust = 0.0
	Total drag coefficient for all the boundaries.
su2double	Total_Power = 0.0
	Total drag coefficient for all the boundaries.
su2double	Total_ReverseFlow = 0.0
	Total drag coefficient for all the boundaries.
su2double	Total_IDC = 0.0
	Total IDC coefficient for all the boundaries.
su2double	Total_IDC_Mach = 0.0
	Total IDC coefficient for all the boundaries.
su2double	Total_IDR = 0.0
	Total IDC coefficient for all the boundaries.
su2double	Total_DC60 = 0.0
	Total IDC coefficient for all the boundaries.
su2double	Total_MFR = 0.0
	Total Mass Flow Ratio for all the boundaries.
su2double	Total_Prop_Eff = 0.0
	Total Mass Flow Ratio for all the boundaries.
su2double	Total_ByPassProp_Eff = 0.0
	Total Mass Flow Ratio for all the boundaries.
su2double	Total_Adiab_Eff = 0.0
	Total Mass Flow Ratio for all the boundaries.
su2double	Total_Poly_Eff = 0.0
	Total Mass Flow Ratio for all the boundaries.
su2double	Total_CMx_Prev = 0.0
	Total drag coefficient for all the boundaries (fixed lift mode).
su2double	Total_CMy_Prev = 0.0
	Total drag coefficient for all the boundaries (fixed lift mode).
su2double	Total_CMz_Prev = 0.0
	Total drag coefficient for all the boundaries (fixed lift mode).
su2double	Total_AeroCD = 0.0
	Total aero drag coefficient for all the boundaries.
su2double	Total_CEquivArea = 0.0
	Total Equivalent Area coefficient for all the boundaries.
su2double	AoA_Prev
	Old value of the angle of attack (monitored).
su2double	AoA_inc
bool	Start_AoA_FD = false
	Boolean for start of finite differencing for FixedCL mode.
bool	End_AoA_FD = false
	Boolean for end of finite differencing for FixedCL mode.
bool	Update_AoA = false
	Boolean to signal Angle of Attack Update.
unsigned long	Iter_Update_AoA = 0
	Iteration at which AoA was updated last.
su2double	dCL_dAlpha
	Value of dCL_dAlpha used to control CL in fixed CL mode.
unsigned long	BCThrust_Counter
vector< CFluidModel * >	FluidModel
	fluid model used in the solver.
su2double	MeanTemperature
su2double	StdDevTemperature
vector< su2activematrix >	AverageFlux
vector< su2activematrix >	SpanTotalFlux
vector< su2activematrix >	AverageVelocity
vector< su2activematrix >	AverageTurboVelocity
vector< su2activematrix >	OldAverageTurboVelocity
su2activematrix	AveragePressure
su2activematrix	OldAveragePressure
su2activematrix	RadialEquilibriumPressure
su2activematrix	AverageDensity
su2activematrix	OldAverageDensity
su2activematrix	AverageNu
su2activematrix	AverageKine
su2activematrix	AverageOmega
su2activevector	AverageMassFlowRate
su2activematrix	AverageRelTangVelocity
su2activematrix	DensityIn
su2activematrix	PressureIn
vector< su2activematrix >	TurboVelocityIn
su2activematrix	DensityOut
su2activematrix	PressureOut
vector< su2activematrix >	TurboVelocityOut
su2activematrix	KineIn
su2activematrix	OmegaIn
su2activematrix	NuIn
su2activematrix	KineOut
su2activematrix	OmegaOut
su2activematrix	NuOut
su2activematrix	RelTangVelocityIn
su2activematrix	RelTangVelocityOut
su2double	ExtAverageDensity
su2double	ExtAveragePressure
su2activevector	ExtAverageTurboVelocity
vector< su2matrix< complex< su2double > > >	CkInflow
vector< su2matrix< complex< su2double > > >	CkOutflow1
vector< su2matrix< complex< su2double > > >	CkOutflow2
vector< su2activematrix >	MixingState
Protected Attributes inherited from CFVMFlowSolverBase< CEulerVariable, ENUM_REGIME::COMPRESSIBLE >
const VariableType::template CIndices< unsigned short >	prim_idx
	Object with indices of primitive variables.
unsigned long	omp_chunk_size
	Chunk size used in light point loops.
su2activevector	EdgeMassFluxes
	Mass fluxes across each edge, for discretization of transported scalars.
su2double	Mach_Inf
	Mach number at the infinity.
su2double	Density_Inf
	Density at the infinity.
su2double	Energy_Inf
	Energy at the infinity.
su2double	Temperature_Inf
	Temperature at the infinity.
su2double	Enthalpy_Inf
	Enthalpy at the infinity.
su2double	Pressure_Inf
	Pressure at the infinity.
su2double *	Velocity_Inf
	Flow Velocity vector at the infinity.
su2double	Viscosity_Inf
	Viscosity at the infinity.
su2double	Tke_Inf
	Turbulent kinetic energy at the infinity.
su2double	StrainMag_Max
	Maximum Strain Rate magnitude.
su2double	Omega_Max
	Maximum Omega.
su2double	Global_Delta_Time
	Time-step for TIME_STEPPING time marching strategy.
su2double	Global_Delta_UnstTimeND
	Unsteady time step for the dual time strategy.
unsigned long	ErrorCounter
	Counter for number of un-physical states.
AeroCoeffsArray	InvCoeff
	Inviscid pressure contributions for each boundary.
AeroCoeffsArray	SurfaceInvCoeff
	Inviscid pressure contributions for each monitoring boundary.
AeroCoeffs	AllBoundInvCoeff
	Total pressure contribution for all the boundaries.
AeroCoeffsArray	MntCoeff
	Inviscid momentum contributions for each boundary.
AeroCoeffsArray	SurfaceMntCoeff
	Inviscid momentum contributions for each monitoring boundary.
AeroCoeffs	AllBoundMntCoeff
	Total momentum contribution for all the boundaries.
AeroCoeffsArray	ViscCoeff
	Viscous contributions for each boundary.
AeroCoeffsArray	SurfaceViscCoeff
	Viscous contributions for each monitoring boundary.
AeroCoeffs	AllBoundViscCoeff
	Total pressure contribution for all the boundaries.
AeroCoeffsArray	SurfaceCoeff
	Totals for each monitoring surface.
AeroCoeffs	TotalCoeff
	Totals for all boundaries.
su2double	AeroCoeffForceRef
	Reference force for aerodynamic coefficients.
su2double	DynamicPressureRef
	Reference dynamic pressure.
su2double	Total_CpDiff
	Total Equivalent Area coefficient for all the boundaries.
su2double	Total_HeatFluxDiff
	Total Equivalent Area coefficient for all the boundaries.
su2double	Total_CEquivArea
	Total Equivalent Area coefficient for all the boundaries.
su2double	Total_MassFlowRate
	Total Mass Flow Rate on monitored boundaries.
su2double	Total_CNearFieldOF
	Total Near-Field Pressure coefficient for all the boundaries.
su2double	Total_Heat
	Total heat load for all the boundaries.
su2double	Total_MaxHeat
	Maximum heat flux on all boundaries.
su2double	AllBound_CNearFieldOF_Inv
	Near-Field press coeff (inviscid) for all the boundaries.
vector< su2double >	CNearFieldOF_Inv
	Near field pressure (inviscid) for each boundary.
vector< su2double >	Surface_HF_Visc
	Total (integrated) heat flux for each monitored surface.
vector< su2double >	Surface_MaxHF_Visc
	Maximum heat flux for each monitored surface.
vector< su2double >	HF_Visc
	Heat load (viscous contribution) for each boundary.
vector< su2double >	MaxHF_Visc
	Maximum heat flux (viscous contribution) for each boundary.
su2double	AllBound_HF_Visc
	Heat load (viscous contribution) for all the boundaries.
su2double	AllBound_MaxHF_Visc
	Maximum heat flux (viscous contribution) for all boundaries.
vector< vector< su2double > >	Inlet_Ptotal
	Value of the Total P.
vector< vector< su2double > >	Inlet_Ttotal
	Value of the Total T.
vector< su2activematrix >	Inlet_FlowDir
	Value of the Flow Direction.
vector< vector< su2double > >	HeatFlux
	Heat transfer coefficient for each boundary and vertex.
vector< vector< su2double > >	HeatFluxTarget
	Heat transfer coefficient for each boundary and vertex.
vector< su2activematrix >	CharacPrimVar
	Value of the characteristic variables at each boundary.
vector< su2activematrix >	CSkinFriction
	Skin friction coefficient for each boundary and vertex.
vector< vector< su2double > >	WallShearStress
	Wall Shear Stress for each boundary and vertex.
vector< su2activematrix >	HeatConjugateVar
	CHT variables for each boundary and vertex.
vector< vector< su2double > >	CPressure
	Pressure coefficient for each boundary and vertex.
vector< vector< su2double > >	CPressureTarget
	Target Pressure coefficient for each boundary and vertex.
vector< vector< su2double > >	YPlus
	Yplus for each boundary and vertex.
vector< vector< su2double > >	UTau
	UTau for each boundary and vertex.
vector< vector< su2double > >	EddyViscWall
	Eddy viscosuty at the wall for each boundary and vertex.
bool	space_centered
	True if space centered scheme used.
bool	euler_implicit
	True if euler implicit scheme used.
bool	least_squares
	True if computing gradients by least squares.
su2double	Gamma
	Fluid's Gamma constant (ratio of specific heats).
su2double	Gamma_Minus_One
	Fluids's Gamma - 1.0 .
vector< su2matrix< su2double * > >	SlidingState
vector< vector< int > >	SlidingStateNodes
array< DummyGridColor<>, 1 >	EdgeColoring
CSysVector< su2double >	EdgeFluxes
	Flux across each edge.
CNumericsSIMD *	edgeNumerics
	Object for edge flux computation.
CEulerVariable *	nodes
	The highest level in the variable hierarchy the DERIVED solver can safely use.
Protected Attributes inherited from CSolver
int	rank
	MPI Rank.
int	size
	MPI Size.
bool	adjoint
	Boolean to determine whether solver is initialized as a direct or an adjoint solver.
unsigned short	MGLevel
	Multigrid level of this solver object.
unsigned short	IterLinSolver
	Linear solver iterations.
su2double	ResLinSolver
	Final linear solver residual.
unsigned short	NonLinRes_Counter
	Number of elements of the nonlinear residual indicator series.
vector< su2double >	NonLinRes_Series
	Vector holding the nonlinear residual indicator series.
su2double	Old_Func
	Old value of the nonlinear residual indicator.
su2double	New_Func
	Current value of the nonlinear residual indicator.
unsigned short	nVar
	Number of variables of the problem.
unsigned short	nPrimVar
	Number of primitive variables of the problem.
unsigned short	nPrimVarGrad
	Number of primitive variables of the problem in the gradient computation.
unsigned short	nSecondaryVar
	Number of primitive variables of the problem.
unsigned short	nVarGrad
	Number of variables for deallocating the LS Cvector.
unsigned short	nDim
	Number of dimensions of the problem.
unsigned long	nPoint
	Number of points of the computational grid.
unsigned long	nPointDomain
	Number of points of the computational grid.
su2double	Max_Delta_Time
	Maximum value of the delta time for all the control volumes.
su2double	Min_Delta_Time
	Minimum value of the delta time for all the control volumes.
su2double	Max_CFL_Local
	Maximum value of the CFL across all the control volumes.
su2double	Min_CFL_Local
	Minimum value of the CFL across all the control volumes.
su2double	Avg_CFL_Local
	Average value of the CFL across all the control volumes.
vector< su2double >	Residual_RMS
	Vector with the mean residual for each variable.
vector< su2double >	Residual_Max
	Vector with the maximal residual for each variable.
vector< su2double >	Residual_BGS
	Vector with the mean residual for each variable for BGS subiterations.
vector< su2double >	Residual_Max_BGS
	Vector with the maximal residual for each variable for BGS subiterations.
vector< unsigned long >	Point_Max
	Vector with the maximal residual for each variable.
vector< unsigned long >	Point_Max_BGS
	Vector with the maximal residual for each variable.
su2activematrix	Point_Max_Coord
	Vector with pointers to the coords of the maximal residual for each variable.
su2activematrix	Point_Max_Coord_BGS
	Vector with pointers to the coords of the maximal residual for each variable.
su2double	Total_Custom_ObjFunc = 0.0
	Total custom objective function.
su2double	Total_ComboObj = 0.0
	Total 'combo' objective for all monitored boundaries.
su2double *	Residual
	Auxiliary nVar vector.
su2double *	Residual_i
	Auxiliary nVar vector for storing the residual at point i.
su2double *	Residual_j
	Auxiliary nVar vector for storing the residual at point j.
su2double *	Solution
	Auxiliary nVar vector.
su2double *	Solution_i
	Auxiliary nVar vector for storing the solution at point i.
su2double *	Solution_j
	Auxiliary nVar vector for storing the solution at point j.
su2double *	Vector
	Auxiliary nDim vector.
su2double *	Vector_i
	Auxiliary nDim vector to do the reconstruction of the variables at point i.
su2double *	Vector_j
	Auxiliary nDim vector to do the reconstruction of the variables at point j.
su2double *	Res_Conv
	Auxiliary nVar vector for storing the convective residual.
su2double *	Res_Visc
	Auxiliary nVar vector for storing the viscous residual.
su2double *	Res_Sour
	Auxiliary nVar vector for storing the viscous residual.
su2double *	Res_Conv_i
	Auxiliary vector for storing the convective residual at point i.
su2double *	Res_Visc_i
	Auxiliary vector for storing the viscous residual at point i.
su2double *	Res_Conv_j
	Auxiliary vector for storing the convective residual at point j.
su2double *	Res_Visc_j
	Auxiliary vector for storing the viscous residual at point j.
su2double **	Jacobian_i
	Auxiliary matrices for storing point to point Jacobians at point i.
su2double **	Jacobian_j
	Auxiliary matrices for storing point to point Jacobians at point j.
su2double **	Jacobian_ii
	Auxiliary matrices for storing point to point Jacobians.
su2double **	Jacobian_ij
	Auxiliary matrices for storing point to point Jacobians.
su2double **	Jacobian_ji
	Auxiliary matrices for storing point to point Jacobians.
su2double **	Jacobian_jj
	Auxiliary matrices for storing point to point Jacobians.
su2activevector	iPoint_UndLapl
	Auxiliary variable for the undivided Laplacians.
su2activevector	jPoint_UndLapl
	Auxiliary variable for the undivided Laplacians.
vector< int >	Restart_Vars
	Auxiliary structure for holding the number of variables and points in a restart.
int	Restart_ExtIter
	Auxiliary structure for holding the external iteration offset from a restart.
vector< passivedouble >	Restart_Data
	Auxiliary structure for holding the data values from a restart.
unsigned short	nOutputVariables
	Number of variables to write.
unsigned long	nMarker
	Total number of markers using the grid information.
vector< unsigned long >	nVertex
	Store nVertex at each marker for deallocation.
bool	rotate_periodic
	Flag that controls whether the periodic solution needs to be rotated for the solver.
bool	implicit_periodic
	Flag that controls whether the implicit system should be treated by the periodic BC comms.
su2activematrix	PeriodicProj
	Min/max reconstruction increments at periodic receive points (for limiters).
std::unordered_map< unsigned long, size_t >	PeriodicProjIndex
	Local point to compact projection row.
bool	dynamic_grid
	Flag that determines whether the grid is dynamic (moving or deforming + grid velocities).
vector< su2activematrix >	VertexTraction
vector< su2activematrix >	VertexTractionAdjoint
std::shared_ptr< CTurboOutput >	TurbomachineryPerformance
	turbo performance calculator.
string	SolverName
	Store the name of the solver for output purposes.

Static Protected Attributes
static constexpr unsigned short	nMixingStateVars = 8
	Number of averaged variables transferred across mixing plane interfaces.
Static Protected Attributes inherited from CFVMFlowSolverBase< CEulerVariable, ENUM_REGIME::COMPRESSIBLE >
static constexpr size_t	MAXNDIM
	Max number of space dimensions, used in some static arrays.
static constexpr size_t	MAXNVAR
	Max number of variables, for static arrays.
static constexpr size_t	OMP_MAX_SIZE
	Max chunk size for light point loops.
static constexpr size_t	OMP_MIN_SIZE
	Min chunk size for edge loops (max is color group size).
static constexpr bool	ReducerStrategy

Additional Inherited Members
Public Attributes inherited from CSolver
CSysVector< su2double >	LinSysSol
	vector to store iterative solution of implicit linear system.
CSysVector< su2double >	LinSysRes
	vector to store iterative residual of implicit linear system.
CSysMatrix< su2mixedfloat >	Jacobian
	Complete sparse Jacobian structure for implicit computations.
CSysSolve< su2mixedfloat >	System
	Linear solver/smoother.
CSysVector< su2double >	OutputVariables
	vector to store the extra variables to be written.
string *	OutputHeadingNames
	vector of strings to store the headings for the exra variables
CVerificationSolution *	VerificationSolution
	Verification solution class used within the solver.
vector< string >	fields
Static Protected Member Functions inherited from CFVMFlowSolverBase< CEulerVariable, ENUM_REGIME::COMPRESSIBLE >
static void	ompMasterAssignBarrier (Ts &&... lhsRhsPairs)
	Utility to set the value of a member variables safely, and so that the new values are seen by all threads.
Static Protected Member Functions inherited from CSolver
static void	ResidualReductions_PerThread (unsigned long iPoint, unsigned short iVar, su2double res, su2double *resRMS, su2double *resMax, unsigned long *idxMax)
	"Add" residual at (iPoint,iVar) to residual variables local to the thread.

Detailed Description

Class for compressible inviscid flow problems, serves as base for Navier-Stokes/RANS.

Author

F. Palacios

Member Typedef Documentation

BaseClass

using CEulerSolver::BaseClass = CFVMFlowSolverBase<CEulerVariable, ENUM_REGIME::COMPRESSIBLE>

protected

Constructor & Destructor Documentation

CEulerSolver() [1/2]

CEulerSolver::CEulerSolver ( )

delete

CEulerSolver() [2/2]

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

Main constructor of this class.

Parameters

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

~CEulerSolver()

CEulerSolver::~CEulerSolver ( void  )

override

Destructor of the class.

Member Function Documentation

BC_ActDisk()

void CEulerSolver::BC_ActDisk ( CGeometry *  geometry, CSolver **  solver_container, CNumerics *  conv_numerics, CNumerics *  visc_numerics, CConfig *  config, unsigned short  val_marker, bool  val_inlet_surface  )

finalvirtual

Impose an actuator disk inlet boundary condition.

Parameters

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

Reimplemented from CSolver.

BC_ActDisk_Inlet()

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

finalvirtual

Impose the engine inflow boundary condition.

Parameters

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

Reimplemented from CSolver.

BC_ActDisk_Outlet()

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

finalvirtual

Impose the engine exhaust boundary condition.

Parameters

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

Reimplemented from CSolver.

BC_ActDisk_VariableLoad()

void CEulerSolver::BC_ActDisk_VariableLoad	(	CGeometry *	geometry,
		CSolver **	solver_container,
		CNumerics *	conv_numerics,
		CNumerics *	visc_numerics,
		CConfig *	config,
		unsigned short	val_marker,
		bool	val_inlet_surface
	)

Impose an actuator disk with variable load boundary condition.

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.
[in]	val_inlet_surface	- Boolean for whether val_marker is an inlet

\function BC_ActDisk_VariableLoad Actuator disk model with variable load along disk radius.

Author

: E. Saetta, L. Russo, R. Tognaccini (GitHub references EttoreSaetta, lorenzorusso07, rtogna). Theoretical and Applied Aerodynamics Research Group (TAARG), University of Naples Federico II. First release date : July 1st 2020 modified on:

Force coefficients distribution given in an input file. Actuator disk data initialized in function SetActDisk_BCThrust. Entropy, acoustic Riemann invariant R+ and tangential velocity extrapolated from upstream flow; acoustic Riemann invariant R- is extrapolated from downstream. Hovering condition simulation not available yet: freestream velocity must be different than zero.

BC_Engine_Exhaust()

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

finalvirtual

Impose the ancelle exhaust boundary condition.

Parameters

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

Reimplemented from CSolver.

BC_Engine_Inflow()

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

finalvirtual

Impose the nacelle inflow boundary condition.

Parameters

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

Reimplemented from CSolver.

BC_Far_Field()

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

finalvirtual

Impose the far-field boundary condition using characteristics.

Parameters

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

Reimplemented from CSolver.

BC_Giles()

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

finalvirtual

Impose the boundary condition using characteristic recostruction.

Author

: G.Gori, S.Vitale, M.Pini, A.Guardone, P.Colonna

Parameters

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

Reimplemented from CSolver.

BC_Inlet()

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

finalvirtual

Impose a subsonic inlet boundary condition.

Parameters

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

Reimplemented from CSolver.

BC_Outlet()

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

finalvirtual

Impose the outlet boundary condition.

Parameters

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

Reimplemented from CSolver.

BC_Riemann()

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

finalvirtual

Impose the boundary condition using characteristic recostruction.

Author

: G.Gori, S.Vitale, M.Pini, A.Guardone, P.Colonna

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.

check in which case is true (only freesurface?)

check in which case is true (only freesurface?)

check in which case is true (only freesurface?)

Reimplemented from CSolver.

BC_Supersonic_Inlet()

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

finalvirtual

Impose a supersonic inlet boundary condition.

Parameters

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

Reimplemented from CSolver.

BC_Supersonic_Outlet()

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

finalvirtual

Impose a supersonic outlet boundary condition.

Parameters

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

Reimplemented from CSolver.

BC_TurboRiemann()

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

finalvirtual

Impose the boundary condition using characteristic recostruction.

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.

check in which case is true (only freesurface?)

Reimplemented from CSolver.

Centered_Residual()

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

finalvirtual

Compute the spatial integration using a centered scheme.

Parameters

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

Reimplemented from CSolver.

ClassicalRK4_Iteration()

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

finalvirtual

Update the solution using the classical fourth-order Runge-Kutta scheme.

Parameters

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

Reimplemented from CSolver.

CommonPreprocessing()

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

protected

Preprocessing actions common to the Euler and NS solvers.

Parameters

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

ComputeBackVelocity()

void CEulerSolver::ComputeBackVelocity ( const su2double *  turboVelocity, const su2double *  turboNormal, su2double *  cartesianVelocity, unsigned short  marker_flag, TURBOMACHINERY_TYPE  kind_turb  )

inline

it take a velocity in the cartesian reference of framework and transform into the turbomachinery frame of reference.

Parameters

[in]	cartesianVelocity	- cartesian components of velocity vector.
[in]	turboNormal	- normal vector in the turbomachinery frame of reference.
[in]	turboVelocity	- velocity vector in the turbomachinery frame of reference.

ComputeConsistentExtrapolation()

void CEulerSolver::ComputeConsistentExtrapolation ( CFluidModel *  fluidModel, unsigned short  nDim, su2double *  primitive, su2double *  secondary  )

static

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

Note

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

Parameters

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

ComputeTurboBladePerformance()

void CEulerSolver::ComputeTurboBladePerformance ( CGeometry *  geometry, CConfig *  config, unsigned short  iBlade  )

finalvirtual

Reimplemented from CSolver.

ComputeTurboVelocity()

void CEulerSolver::ComputeTurboVelocity ( const su2double *  cartesianVelocity, const su2double *  turboNormal, su2double *  turboVelocity, unsigned short  marker_flag, TURBOMACHINERY_TYPE  kind_turb  )

inline

it take a velocity in the cartesian reference of framework and transform into the turbomachinery frame of reference.

Parameters

[in]	cartesianVelocity	- cartesian components of velocity vector.
[in]	turboNormal	- normal vector in the turbomachinery frame of reference.
[in]	turboVelocity	- velocity vector in the turbomachinery frame of reference.

ComputeUnderRelaxationFactor()

void CEulerSolver::ComputeUnderRelaxationFactor ( const CConfig *  config )

finalvirtual

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

Parameters

[in]

config

- Definition of the particular problem.

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

Evaluate_ObjFunc()

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

overridevirtual

Compute weighted-sum "combo" objective output.

Author

H. Kline

Parameters

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

Reimplemented from CSolver.

Reimplemented in CNSSolver.

ExplicitEuler_Iteration()

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

finalvirtual

Update the solution using the explicit Euler scheme.

Parameters

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

Reimplemented from CSolver.

ExplicitRK_Iteration()

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

finalvirtual

Update the solution using a Runge-Kutta scheme.

Parameters

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

Reimplemented from CSolver.

FixedCL_Convergence()

bool CEulerSolver::FixedCL_Convergence ( CConfig *  config, bool  convergence  )

finalvirtual

Check for convergence of the Fixed CL mode to the target CL.

Parameters

[in]	config	- Definition of the particular problem.
[in]	convergence	- boolean for whether the solution is converged

Returns

boolean for whether the Fixed CL mode is converged to target CL

Reimplemented from CSolver.

GatherInOutAverageValues()

void CEulerSolver::GatherInOutAverageValues ( CConfig *  config, CGeometry *  geometry  )

finalvirtual

It gathers into the master node average quantities at inflow and outflow needed for turbomachinery analysis.

Parameters

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

Reimplemented from CSolver.

GetAoA_inc()

su2double CEulerSolver::GetAoA_inc ( void  ) const

inlinefinalvirtual

Get the CL Driver's control command.

Returns

value of CL Driver control command (AoA_inc)

Reimplemented from CSolver.

GetAverageDensity()

su2double CEulerSolver::GetAverageDensity ( unsigned short  valMarker, unsigned short  valSpan  ) const

inlinefinalvirtual

Provide the average density at the boundary of interest.

Parameters

[in]

val_marker

- bound marker.

Returns

Value of the Average Density on the surface val_marker.

Reimplemented from CSolver.

GetAverageKine()

su2double CEulerSolver::GetAverageKine ( unsigned short  valMarker, unsigned short  valSpan  ) const

inlinefinalvirtual

Provide the average density at the boundary of interest.

Parameters

[in]

val_marker

- bound marker.

Returns

Value of the Average turbulent Kine on the surface val_marker.

Reimplemented from CSolver.

GetAverageNu()

su2double CEulerSolver::GetAverageNu ( unsigned short  valMarker, unsigned short  valSpan  ) const

inlinefinalvirtual

Provide the average density at the boundary of interest.

Parameters

[in]

val_marker

- bound marker.

Returns

Value of the Average turbulent Nu on the surface val_marker.

Reimplemented from CSolver.

GetAverageOmega()

su2double CEulerSolver::GetAverageOmega ( unsigned short  valMarker, unsigned short  valSpan  ) const

inlinefinalvirtual

Provide the average density at the boundary of interest.

Parameters

[in]

val_marker

- bound marker.

Returns

Value of the Average turbulent Omega on the surface val_marker.

Reimplemented from CSolver.

GetAveragePressure()

su2double CEulerSolver::GetAveragePressure ( unsigned short  valMarker, unsigned short  valSpan  ) const

inlinefinalvirtual

Provide the average pressure at the boundary of interest.

Parameters

[in]

val_marker

- bound marker.

Returns

Value of the Average Pressure on the surface val_marker.

Reimplemented from CSolver.

GetAverageTurboVelocity()

const su2double * CEulerSolver::GetAverageTurboVelocity ( unsigned short  valMarker, unsigned short  valSpan  ) const

inlinefinalvirtual

Provide the average turbo velocity average at the boundary of interest.

Parameters

[in]

val_marker

- bound marker.

Returns

Value of the Average Total Pressure on the surface val_marker.

Reimplemented from CSolver.

GetDensityIn()

su2double CEulerSolver::GetDensityIn ( unsigned short  inMarkerTP, unsigned short  valSpan  ) const

inlinefinalvirtual

Provide the inlet density to check convergence of conservative mixing-plane.

Parameters

[in]

inMarkerTP

- bound marker.

Returns

Value of the inlet density.

Reimplemented from CSolver.

GetDensityOut()

su2double CEulerSolver::GetDensityOut ( unsigned short  inMarkerTP, unsigned short  valSpan  ) const

inlinefinalvirtual

Provide the outlet density to check convergence of conservative mixing-plane.

Parameters

[in]

inMarkerTP

- bound marker.

Returns

Value of the outlet density.

Reimplemented from CSolver.

GetDonorGlobalIndex()

unsigned long CEulerSolver::GetDonorGlobalIndex ( unsigned short  val_marker, unsigned long  val_vertex  ) const

inlinefinalvirtual

Value of the characteristic global index 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.

GetEnd_AoA_FD()

bool CEulerSolver::GetEnd_AoA_FD ( void  ) const

inlinefinalvirtual

Checking whether fixed CL mode in finite-differencing mode.

Returns

boolean for whether the Fixed CL mode is currently in finite-differencing mode

Reimplemented from CSolver.

GetExhaust_MassFlow()

su2double CEulerSolver::GetExhaust_MassFlow ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the mass flow rate.

Parameters

val_marker

Surface where the coeficient is going to be computed.

Returns

Value of the mass flow rate on the surface val_marker.

Reimplemented from CSolver.

GetFluidModel()

CFluidModel * CEulerSolver::GetFluidModel ( void  ) const

inlinefinalvirtual

Compute the pressure at the infinity.

Returns

Value of the pressure at the infinity.

Reimplemented from CSolver.

GetHasHybridParallel()

bool CEulerSolver::GetHasHybridParallel ( ) const

inlinefinalvirtual

The Euler and NS solvers support MPI+OpenMP.

Reimplemented from CSolver.

GetInflow_Mach()

su2double CEulerSolver::GetInflow_Mach ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the mass flow rate.

Parameters

val_marker

Surface where the coeficient is going to be computed.

Returns

Value of the fan face mach on the surface val_marker.

Reimplemented from CSolver.

GetInflow_MassFlow()

su2double CEulerSolver::GetInflow_MassFlow ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the mass flow rate.

Parameters

val_marker

Surface where the coeficient is going to be computed.

Returns

Value of the mass flow rate on the surface val_marker.

Reimplemented from CSolver.

GetInflow_Pressure()

su2double CEulerSolver::GetInflow_Pressure ( unsigned short  val_marker ) const

inlinefinalvirtual

Provide the mass flow rate.

Parameters

val_marker

Surface where the coeficient is going to be computed.

Returns

Value of the fan face pressure on the surface val_marker.

Reimplemented from CSolver.

GetIter_Update_AoA()

unsigned long CEulerSolver::GetIter_Update_AoA ( void  ) const

inlinefinalvirtual

Get the iteration of the last AoA update (Fixed CL Mode)

Returns

value for the last iteration that the AoA was updated

Reimplemented from CSolver.

GetKineIn()

su2double CEulerSolver::GetKineIn ( unsigned short  inMarkerTP, unsigned short  valSpan  ) const

inlinefinalvirtual

Provide the inlet turbulent kei to check convergence of conservative mixing-plane.

Parameters

[in]

inMarkerTP

- bound marker.

Returns

Value of the inlet density.

Reimplemented from CSolver.

GetKineOut()

su2double CEulerSolver::GetKineOut ( unsigned short  inMarkerTP, unsigned short  valSpan  ) const

inlinefinalvirtual

Provide the outlet turbulent kei to check convergence of conservative mixing-plane.

Parameters

[in]

inMarkerTP

- bound marker.

Returns

Value of the inlet density.

Reimplemented from CSolver.

GetMixingState()

su2double CEulerSolver::GetMixingState ( unsigned short  val_marker, unsigned long  val_span, unsigned short  val_state  ) const

inlinefinalprotectedvirtual

Get a component of the donor-side averaged state at a mixing plane interface.

Parameters

[in]	val_marker	- marker index
[in]	val_span	- span index
[in]	val_state	- requested state component

Reimplemented from CSolver.

GetNuIn()

su2double CEulerSolver::GetNuIn ( unsigned short  inMarkerTP, unsigned short  valSpan  ) const

inlinefinalvirtual

Provide the inlet turbulent nu to check convergence of conservative mixing-plane.

Parameters

[in]

inMarkerTP

- bound marker.

Returns

Value of the inlet density.

Reimplemented from CSolver.

GetNuOut()

su2double CEulerSolver::GetNuOut ( unsigned short  inMarkerTP, unsigned short  valSpan  ) const

inlinefinalvirtual

Provide the outlet turbulent nu to check convergence of conservative mixing-plane.

Parameters

[in]

inMarkerTP

- bound marker.

Returns

Value of the inlet density.

Reimplemented from CSolver.

GetOmegaIn()

su2double CEulerSolver::GetOmegaIn ( unsigned short  inMarkerTP, unsigned short  valSpan  ) const

inlinefinalvirtual

Provide the inlet turbulent omega to check convergence of conservative mixing-plane.

Parameters

[in]

inMarkerTP

- bound marker.

Returns

Value of the inlet density.

Reimplemented from CSolver.

GetOmegaOut()

su2double CEulerSolver::GetOmegaOut ( unsigned short  inMarkerTP, unsigned short  valSpan  ) const

inlinefinalvirtual

Provide the outlet turbulent omega to check convergence of conservative mixing-plane.

Parameters

[in]

inMarkerTP

- bound marker.

Returns

Value of the inlet density.

Reimplemented from CSolver.

GetPower_Properties()

void CEulerSolver::GetPower_Properties ( CGeometry *  geometry, CConfig *  config, unsigned short  iMesh, bool  Output  )

protected

Compute the Fan face Mach number.

Parameters

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

GetPressureIn()

su2double CEulerSolver::GetPressureIn ( unsigned short  inMarkerTP, unsigned short  valSpan  ) const

inlinefinalvirtual

Provide the inlet pressure to check convergence of conservative mixing-plane.

Parameters

[in]

inMarkerTP

- bound marker.

Returns

Value of inlet pressure.

Reimplemented from CSolver.

GetPressureOut()

su2double CEulerSolver::GetPressureOut ( unsigned short  inMarkerTP, unsigned short  valSpan  ) const

inlinefinalvirtual

Provide the outlet pressure to check convergence of conservative mixing-plane.

Parameters

[in]

inMarkerTP

- bound marker.

Returns

Value of the outlet pressure.

Reimplemented from CSolver.

GetPrevious_AoA()

su2double CEulerSolver::GetPrevious_AoA ( void  ) const

inlinefinalvirtual

Get the AoA before the most recent update.

Returns

value of the AoA before most recent update

Reimplemented from CSolver.

GetStart_AoA_FD()

bool CEulerSolver::GetStart_AoA_FD ( void  ) const

inlinefinalvirtual

Checking whether fixed CL mode in finite-differencing mode.

Returns

boolean for whether the Fixed CL mode is currently in finite-differencing mode

Reimplemented from CSolver.

GetTangGridVelIn()

su2double CEulerSolver::GetTangGridVelIn ( unsigned short  val_blade, unsigned long  val_span  )

inlineprotected

GetTangGridVelOut()

su2double CEulerSolver::GetTangGridVelOut ( unsigned short  val_blade, unsigned long  val_span  )

inlineprotected

GetTotal_Adiab_Eff()

su2double CEulerSolver::GetTotal_Adiab_Eff ( ) const

inlinefinalvirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_AeroCD()

su2double CEulerSolver::GetTotal_AeroCD ( ) const

inlinefinalvirtual

Provide the total (inviscid + viscous) non dimensional aero CD.

Returns

Value of the Aero CD coefficient (inviscid + viscous contribution).

Reimplemented from CSolver.

GetTotal_ByPassProp_Eff()

su2double CEulerSolver::GetTotal_ByPassProp_Eff ( ) const

inlinefinalvirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_CNearFieldOF()

su2double CEulerSolver::GetTotal_CNearFieldOF ( ) const

inlinefinalvirtual

Provide the total (inviscid + viscous) non dimensional Near-Field pressure coefficient.

Returns

Value of the NearField pressure coefficient (inviscid + viscous contribution).

Reimplemented from CSolver.

GetTotal_DC60()

su2double CEulerSolver::GetTotal_DC60 ( ) const

inlinefinalvirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_IDC()

su2double CEulerSolver::GetTotal_IDC ( ) const

inlinefinalvirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_IDC_Mach()

su2double CEulerSolver::GetTotal_IDC_Mach ( ) const

inlinefinalvirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_IDR()

su2double CEulerSolver::GetTotal_IDR ( ) const

inlinefinalvirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_MFR()

su2double CEulerSolver::GetTotal_MFR ( ) const

inlinefinalvirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_NetThrust()

su2double CEulerSolver::GetTotal_NetThrust ( ) const

inlinefinalvirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_Poly_Eff()

su2double CEulerSolver::GetTotal_Poly_Eff ( ) const

inlinefinalvirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_Power()

su2double CEulerSolver::GetTotal_Power ( ) const

inlinefinalvirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_Prop_Eff()

su2double CEulerSolver::GetTotal_Prop_Eff ( ) const

inlinefinalvirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_ReverseFlow()

su2double CEulerSolver::GetTotal_ReverseFlow ( ) const

inlinefinalvirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_SolidCD()

su2double CEulerSolver::GetTotal_SolidCD ( ) const

inlinefinalvirtual

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

Returns

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

Reimplemented from CSolver.

GetTurboBladePerformance()

std::shared_ptr< CTurboOutput > CEulerSolver::GetTurboBladePerformance ( ) const

inlinefinalvirtual

Reimplemented from CSolver.

GetTurboPrimitive()

vector< su2double > CEulerSolver::GetTurboPrimitive ( unsigned short  iBlade, unsigned short  iSpan, bool  INLET  )

inlineoverridevirtual

Get Primal variables for turbo performance computation iteration can be executed by multiple threads.

Returns

returns Density, pressure and TurboVelocity (IN/OUTLET)

Reimplemented from CSolver.

GetTurboVelocityIn()

const su2double * CEulerSolver::GetTurboVelocityIn ( unsigned short  inMarkerTP, unsigned short  valSpan  ) const

inlinefinalvirtual

Provide the inlet normal velocity to check convergence of conservative mixing-plane.

Parameters

[in]

inMarkerTP

- bound marker.

Returns

Value of the inlet normal velocity.

Reimplemented from CSolver.

GetTurboVelocityOut()

const su2double * CEulerSolver::GetTurboVelocityOut ( unsigned short  inMarkerTP, unsigned short  valSpan  ) const

inlinefinalvirtual

Provide the outlet normal velocity to check convergence of conservative mixing-plane.

Parameters

[in]

inMarkerTP

- bound marker.

Returns

Value of the outlet normal velocity.

Reimplemented from CSolver.

IdentifySolutionOutliers()

void CEulerSolver::IdentifySolutionOutliers ( const CConfig *  config, unsigned long  iter  )

finalvirtual

Identify points where the static temperature is an outlier to treat them as non-physical, e.g. force the reconstruction to be 1st order.

Reimplemented from CSolver.

InitTurboContainers()

void CEulerSolver::InitTurboContainers ( CGeometry *  geometry, CConfig **  config, unsigned short  iZone  )

finalvirtual

Initilize turbo containers.

Parameters

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

Reimplemented from CSolver.

InstantiateEdgeNumerics()

void CEulerSolver::InstantiateEdgeNumerics ( const CSolver *const *  solvers, const CConfig *  config  )

finalprotectedvirtual

Instantiate a SIMD numerics object.

Parameters

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

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

LowMachPrimitiveCorrection()

void CEulerSolver::LowMachPrimitiveCorrection ( CFluidModel *  fluidModel, unsigned short  nDim, su2double *  primitive_i, su2double *  primitive_j  )

static

Apply low Mach number correction to the primitives at two points, usually connected by an edge.

Note

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

Parameters

[in,out]	fluidModel	- The fluid model.
[in]	nDim	- Number of physical dimensions.
[in,out]	primitive_i	- Primitive variables at point i.
[in,out]	primitive_j	- Primitive variables at point j.

MixedOut_Average()

void CEulerSolver::MixedOut_Average	(	CConfig *	config,
		su2double	val_init_pressure,
		const su2double *	val_Averaged_Flux,
		const su2double *	val_normal,
		su2double &	pressure_mix,
		su2double &	density_mix
	)

it performs a mixed out average of the nodes of a boundary.

Parameters

[in]	val_init_pressure	- initial pressure value
[in]	val_Averaged_Flux	- flux averaged values.
[in]	val_normal	- normal vector.
[in]	pressure_mix	- value of the mixed-out avaraged pressure.
[in]	density_miz	- value of the mixed-out avaraged density.

PrepareImplicitIteration()

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

finalvirtual

Prepare an implicit iteration.

Parameters

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

Reimplemented from CSolver.

PreprocessAverage()

void CEulerSolver::PreprocessAverage ( CSolver **  solver, CGeometry *  geometry, CConfig *  config, unsigned short  marker_flag  )

finalvirtual

It computes average quantities along the span for turbomachinery analysis.

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]	marker_flag	- Surface marker flag where the function is applied.

Reimplemented from CSolver.

PreprocessBC_Giles()

void CEulerSolver::PreprocessBC_Giles ( CGeometry *  geometry, CConfig *  config, CNumerics *  conv_numerics, unsigned short  marker_flag  )

finalvirtual

It computes Fourier transformation for the needed quantities along the pitch for each span in turbomachinery analysis.

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]	marker_flag	- Surface marker flag where the function is applied.

Reimplemented from CSolver.

Preprocessing()

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

overridevirtual

Compute primitive variables and their gradients.

Parameters

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

Reimplemented from CSolver.

Reimplemented in CNSSolver.

PrintVerificationError()

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

finalvirtual

Print verification error to screen.

Parameters

[in]

config

- Definition of the particular problem.

Implements CFVMFlowSolverBase< CEulerVariable, ENUM_REGIME::COMPRESSIBLE >.

ReadActDisk_InputFile()

void CEulerSolver::ReadActDisk_InputFile ( CGeometry *  geometry, CSolver **  solver_container, CConfig *  config, unsigned short  iMesh, bool  Output  )

protected

Read the actuator disk input file for the VARIABLE_LOAD type.

Parameters

[in]	geometry	- Geometrical definition of the problem.
[in]	solver_container	- Container vector with all the solutions.
[in]	config	- Definition of the particular problem.
[in]	iMesh	- current mesh level for the multigrid.
[in]	Output	- boolean to determine whether to print output.

Set_MPI_ActDisk()

void CEulerSolver::Set_MPI_ActDisk ( CSolver **  solver_container, CGeometry *  geometry, CConfig *  config  )

protected

Parallelization of Undivided Laplacian.

Parameters

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

SetActDisk_BCThrust()

void CEulerSolver::SetActDisk_BCThrust ( CGeometry *  geometry, CSolver **  solver_container, CConfig *  config, unsigned short  iMesh, bool  Output  )

protected

Update the AoA and freestream velocity at the farfield.

Parameters

[in]	geometry	- Geometrical definition of the problem.
[in]	solver_container	- Container vector with all the solutions.
[in]	config	- Definition of the particular problem.
[in]	iMesh	- current mesh level for the multigrid.
[in]	Output	- boolean to determine whether to print output.

SetActDisk_BEM_VLAD()

void CEulerSolver::SetActDisk_BEM_VLAD ( CGeometry *  geometry, CSolver **  solver_container, CConfig *  config, unsigned short  iMesh, bool  Output  )

protected

Read and update the variable load actuator disk from input file for the BLADE_ELEMENT type.

Author

: Chandukrishna Y., T. N. Venkatesh and Josy P. Pullockara

Parameters

[in]	geometry	- Geometrical definition of the problem.
[in]	solver_container	- Container vector with all the solutions.
[in]	config	- Definition of the particular problem.
[in]	iMesh	- current mesh level for the multigrid.
[in]	Output	- boolean to determine whether to print output.

\function SetActDisk_BEM_VLAD Actuator disk model with Blade Element Method (BEM)

Author

: Chandukrishna Y., T. N. Venkatesh and Josy Pullockara Institution: Computational and Theoretical Fluid Dynamics (CTFD), CSIR - National Aerospace Laboratories, Bangalore Academy of Scientific and Innovative Research, Ghaziabad

Version

8.5.0 "Harrier" First release date : September 26 2023 modified on:

Section properties of the propeller given in an input file. Cl, Cd of propeller sections need to be generated earlier and saved in this file Actuator disk data initialized in function SetActDisk_BCThrust. Propeller load calculated with Blade Element Method Interpolated load at each point on the actuator disk is set in SetActDisk_BEM_VLAD function Rest calculations follows the Variable Load (BC_ActDisk_VariableLoad) approach

SetCentered_Dissipation_Sensor()

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

protected

Compute the dissipation sensor for centered schemes.

Parameters

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

SetCoefficient_Gradients()

void CEulerSolver::SetCoefficient_Gradients ( CConfig *  config ) const

protected

Set gradients of coefficients for fixed CL mode.

Parameters

[in]

config

- Definition of the particular problem.

SetDensityIn()

void CEulerSolver::SetDensityIn ( su2double  value, unsigned short  inMarkerTP, unsigned short  valSpan  )

inlinefinalvirtual

Set inlet density.

Parameters

[in]	value	- turboperformance value to set.
[in]	inMarkerTP	- turboperformance marker.

Reimplemented from CSolver.

SetDensityOut()

void CEulerSolver::SetDensityOut ( su2double  value, unsigned short  inMarkerTP, unsigned short  valSpan  )

inlinefinalvirtual

Set outlet density.

Parameters

[in]	value	- turboperformance value to set.
[in]	inMarkerTP	- turboperformance marker.

Reimplemented from CSolver.

SetDonorGlobalIndex()

void CEulerSolver::SetDonorGlobalIndex ( unsigned short  val_marker, unsigned long  val_vertex, unsigned long  val_index  )

inlinefinalvirtual

Value of the characteristic global index 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.

SetFarfield_AoA()

void CEulerSolver::SetFarfield_AoA ( CGeometry *  geometry, CSolver **  solver_container, CConfig *  config, unsigned short  iMesh, bool  Output  )

protected

Update the AoA and freestream velocity at the farfield.

Parameters

[in]	geometry	- Geometrical definition of the problem.
[in]	solver_container	- Container vector with all the solutions.
[in]	config	- Definition of the particular problem.
[in]	iMesh	- current mesh level for the multigrid.
[in]	Output	- boolean to determine whether to print output.

SetFreeStream_Solution()

void CEulerSolver::SetFreeStream_Solution ( const CConfig *  config )

finalvirtual

Set the solution using the Freestream values.

Parameters

[in]

config

- Definition of the particular problem.

Reimplemented from CSolver.

SetFreeStream_TurboSolution()

void CEulerSolver::SetFreeStream_TurboSolution ( CConfig *  config )

finalvirtual

Set the solution using the Freestream values.

Parameters

[in]

config

- Definition of the particular problem.

Reimplemented from CSolver.

SetInitialCondition()

void CEulerSolver::SetInitialCondition ( CGeometry **  geometry, CSolver ***  solver_container, CConfig *  config, unsigned long  TimeIter  )

finalvirtual

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.

SetKineIn()

void CEulerSolver::SetKineIn ( su2double  value, unsigned short  inMarkerTP, unsigned short  valSpan  )

inlinefinalvirtual

Set inlet turbulent kei.

Parameters

[in]	value	- turboperformance value to set.
[in]	inMarkerTP	- turboperformance marker.

Reimplemented from CSolver.

SetKineOut()

void CEulerSolver::SetKineOut ( su2double  value, unsigned short  inMarkerTP, unsigned short  valSpan  )

inlinefinalvirtual

Set outlet turbulent kei.

Parameters

[in]	value	- turboperformance value to set.
[in]	inMarkerTP	- turboperformance marker.

Reimplemented from CSolver.

SetMax_Eigenvalue()

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

protected

Compute the max eigenvalue.

Parameters

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

SetMixingState()

void CEulerSolver::SetMixingState ( unsigned short  val_marker, unsigned long  val_span, unsigned short  val_state, su2double  component  )

inlinefinalprotectedvirtual

Set a component of the donor-side averaged state at a mixing plane interface nodes.

Parameters

[in]	val_marker	- marker index
[in]	val_span	- span index
[in]	val_state	- state component to set
[in]	component	- value to set

Reimplemented from CSolver.

SetNondimensionalization()

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

protected

Set the solver nondimensionalization.

Parameters

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

SetNuIn()

void CEulerSolver::SetNuIn ( su2double  value, unsigned short  inMarkerTP, unsigned short  valSpan  )

inlinefinalvirtual

Set inlet turbulent Nu.

Parameters

[in]	value	- turboperformance value to set.
[in]	inMarkerTP	- turboperformance marker.

Reimplemented from CSolver.

SetNuOut()

void CEulerSolver::SetNuOut ( su2double  value, unsigned short  inMarkerTP, unsigned short  valSpan  )

inlinefinalvirtual

Set outlet turbulent Nu.

Parameters

[in]	value	- turboperformance value to set.
[in]	inMarkerTP	- turboperformance marker.

Reimplemented from CSolver.

SetOmegaIn()

void CEulerSolver::SetOmegaIn ( su2double  value, unsigned short  inMarkerTP, unsigned short  valSpan  )

inlinefinalvirtual

Set inlet turbulent omega.

Parameters

[in]	value	- turboperformance value to set.
[in]	inMarkerTP	- turboperformance marker.

Reimplemented from CSolver.

SetOmegaOut()

void CEulerSolver::SetOmegaOut ( su2double  value, unsigned short  inMarkerTP, unsigned short  valSpan  )

inlinefinalvirtual

Set Outlet turbulent omega.

Parameters

[in]	value	- turboperformance value to set.
[in]	inMarkerTP	- turboperformance marker.

Reimplemented from CSolver.

SetPreconditioner()

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

Compute the preconditioner for convergence acceleration by Roe-Turkel method.

Parameters

[in]	config	- Definition of the particular problem.
[in]	iPoint	- Index of the grid point.
[in]	delta	- Volume over delta t.
[in,out]	preconditioner	- The preconditioner matrix, must be allocated outside.

SetPressureIn()

void CEulerSolver::SetPressureIn ( su2double  value, unsigned short  inMarkerTP, unsigned short  valSpan  )

inlinefinalvirtual

Set inlet pressure.

Parameters

[in]	value	- turboperformance value to set.
[in]	inMarkerTP	- turboperformance marker.

Reimplemented from CSolver.

SetPressureOut()

void CEulerSolver::SetPressureOut ( su2double  value, unsigned short  inMarkerTP, unsigned short  valSpan  )

inlinefinalvirtual

Set outlet pressure.

Parameters

[in]	value	- turboperformance value to set.
[in]	inMarkerTP	- turboperformance marker.

Reimplemented from CSolver.

SetPrimitive_Variables()

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

protectedvirtual

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

Parameters

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

Returns

- The number of non-physical points.

SetReferenceValues()

void CEulerSolver::SetReferenceValues ( const CConfig &  config )

finalprotectedvirtual

Set reference values for pressure, forces, etc.

Implements CFVMFlowSolverBase< CEulerVariable, ENUM_REGIME::COMPRESSIBLE >.

SetRoe_Dissipation()

virtual void CEulerSolver::SetRoe_Dissipation ( CGeometry *  geometry, CConfig *  config  )

inlineprotectedvirtual

A virtual member.

Parameters

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

SetTime_Step()

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

finalvirtual

Compute the time step for solving the Euler equations.

Parameters

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

TODO: (REAL_GAS) removing gamma as it cannot work with FLUIDPROP

Reimplemented from CSolver.

SetTotal_Adiab_Eff()

void CEulerSolver::SetTotal_Adiab_Eff ( su2double  val_Total_Adiab_Eff )

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_AeroCD()

void CEulerSolver::SetTotal_AeroCD ( su2double  val_aerocd )

inlinefinalvirtual

Set the value of the Aero drag.

Parameters

[in]

val_cequivarea

- Value of the aero drag.

Reimplemented from CSolver.

SetTotal_ByPassProp_Eff()

void CEulerSolver::SetTotal_ByPassProp_Eff ( su2double  val_Total_ByPassProp_Eff )

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_DC60()

void CEulerSolver::SetTotal_DC60 ( su2double  val_Total_DC60 )

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_IDC()

void CEulerSolver::SetTotal_IDC ( su2double  val_Total_IDC )

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_IDC_Mach()

void CEulerSolver::SetTotal_IDC_Mach ( su2double  val_Total_IDC_Mach )

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_IDR()

void CEulerSolver::SetTotal_IDR ( su2double  val_Total_IDR )

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_MFR()

void CEulerSolver::SetTotal_MFR ( su2double  val_Total_MFR )

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_NetThrust()

void CEulerSolver::SetTotal_NetThrust ( su2double  val_Total_NetThrust )

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_Poly_Eff()

void CEulerSolver::SetTotal_Poly_Eff ( su2double  val_Total_Poly_Eff )

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_Power()

void CEulerSolver::SetTotal_Power ( su2double  val_Total_Power )

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_Prop_Eff()

void CEulerSolver::SetTotal_Prop_Eff ( su2double  val_Total_Prop_Eff )

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_ReverseFlow()

void CEulerSolver::SetTotal_ReverseFlow ( su2double  val_Total_ReverseFlow )

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_SolidCD()

void CEulerSolver::SetTotal_SolidCD ( su2double  val_Total_SolidCD )

inlinefinalvirtual

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

Parameters

[in]

val_Total_CD

- Value of the total drag coefficient.

Reimplemented from CSolver.

SetTurboVelocityIn()

void CEulerSolver::SetTurboVelocityIn ( const su2double *  value, unsigned short  inMarkerTP, unsigned short  valSpan  )

inlinefinalvirtual

Set inlet normal velocity.

Parameters

[in]	value	- turboperformance value to set.
[in]	inMarkerTP	- turboperformance marker.

Reimplemented from CSolver.

SetTurboVelocityOut()

void CEulerSolver::SetTurboVelocityOut ( const su2double *  value, unsigned short  inMarkerTP, unsigned short  valSpan  )

inlinefinalvirtual

Set outlet normal velocity.

Parameters

[in]	value	- turboperformance value to set.
[in]	inMarkerTP	- turboperformance marker.

Reimplemented from CSolver.

SetUndivided_Laplacian()

void CEulerSolver::SetUndivided_Laplacian ( CGeometry *  geometry, const CConfig *  config  )

protected

Compute the undivided laplacian for the solution.

Parameters

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

SetUpwind_Ducros_Sensor()

void CEulerSolver::SetUpwind_Ducros_Sensor ( CGeometry *  geometry, CConfig *  config  )

protected

Compute Ducros Sensor for Roe Dissipation.

Parameters

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

Source_Residual()

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

overridevirtual

Source term integration.

Parameters

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

Reimplemented from CSolver.

Source_Template()

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

finalvirtual

Source term integration.

Parameters

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

Reimplemented from CSolver.

TurboAverageProcess()

void CEulerSolver::TurboAverageProcess ( CSolver **  solver, CGeometry *  geometry, CConfig *  config, unsigned short  marker_flag  )

finalvirtual

It computes average quantities along the span for turbomachinery analysis.

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]	marker_flag	- Surface marker flag where the function is applied.

Reimplemented from CSolver.

Upwind_Residual()

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

finalvirtual

Compute the spatial integration using a upwind scheme.

Parameters

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

Reimplemented from CSolver.

Member Data Documentation

ActDisk_Axis

su2activematrix CEulerSolver::ActDisk_Axis

protected

Value of the actuator disk Axis.

ActDisk_C

su2activematrix CEulerSolver::ActDisk_C

protected

Value of the actuator disk Center.

ActDisk_DeltaP

vector<vector<su2double> > CEulerSolver::ActDisk_DeltaP

protected

Value of the Delta P.

ActDisk_DeltaP_r

vector<vector<su2double> > CEulerSolver::ActDisk_DeltaP_r

protected

Value of the DeltaP_r.

ActDisk_DeltaT

vector<vector<su2double> > CEulerSolver::ActDisk_DeltaT

protected

Value of the Delta T.

ActDisk_Fa

vector<vector<su2double> > CEulerSolver::ActDisk_Fa

protected

Value of the actuator disk Axial Force per Unit Area.

ActDisk_Fa_BEM

vector<vector<su2double> > CEulerSolver::ActDisk_Fa_BEM

protected

Value of the actuator disk Axial Force per Unit Area.

ActDisk_Fx

vector<vector<su2double> > CEulerSolver::ActDisk_Fx

protected

Value of the actuator disk X component of the radial and tangential forces per Unit Area resultant.

ActDisk_Fx_BEM

vector<vector<su2double> > CEulerSolver::ActDisk_Fx_BEM

protected

Value of the actuator disk X component of the radial and tangential forces per Unit Area resultant.

ActDisk_Fy

vector<vector<su2double> > CEulerSolver::ActDisk_Fy

protected

Value of the actuator disk Y component of the radial and tangential forces per Unit Area resultant.

ActDisk_Fy_BEM

vector<vector<su2double> > CEulerSolver::ActDisk_Fy_BEM

protected

Value of the actuator disk Y component of the radial and tangential forces per Unit Area resultant.

ActDisk_Fz

vector<vector<su2double> > CEulerSolver::ActDisk_Fz

protected

Value of the actuator disk Z component of the radial and tangential forces per Unit Area resultant.

ActDisk_Fz_BEM

vector<vector<su2double> > CEulerSolver::ActDisk_Fz_BEM

protected

Value of the actuator disk Z component of the radial and tangential forces per Unit Area resultant.

ActDisk_R

su2activevector CEulerSolver::ActDisk_R

protected

Value of the actuator disk Radius.

ActDisk_Thrust_r

vector<vector<su2double> > CEulerSolver::ActDisk_Thrust_r

protected

Value of the Thrust_r.

ActDisk_Torque_r

vector<vector<su2double> > CEulerSolver::ActDisk_Torque_r

protected

Value of the Torque_r.

AllBound_CEquivArea_Inv

su2double CEulerSolver::AllBound_CEquivArea_Inv =0.0

protected

equivalent area coefficient (inviscid contribution) for all the boundaries.

AoA_inc

su2double CEulerSolver::AoA_inc

protected

AoA_Prev

su2double CEulerSolver::AoA_Prev

protected

Old value of the angle of attack (monitored).

AverageDensity

su2activematrix CEulerSolver::AverageDensity

protected

AverageFlux

vector<su2activematrix> CEulerSolver::AverageFlux

protected

AverageKine

su2activematrix CEulerSolver::AverageKine

protected

AverageMassFlowRate

su2activevector CEulerSolver::AverageMassFlowRate

protected

AverageNu

su2activematrix CEulerSolver::AverageNu

protected

AverageOmega

su2activematrix CEulerSolver::AverageOmega

protected

AveragePressure

su2activematrix CEulerSolver::AveragePressure

protected

AverageRelTangVelocity

su2activematrix CEulerSolver::AverageRelTangVelocity

protected

AverageTurboVelocity

vector<su2activematrix> CEulerSolver::AverageTurboVelocity

protected

AverageVelocity

vector<su2activematrix> CEulerSolver::AverageVelocity

protected

BCThrust_Counter

unsigned long CEulerSolver::BCThrust_Counter

protected

CEquivArea_Inv

vector<su2double> CEulerSolver::CEquivArea_Inv

protected

Equivalent area (inviscid contribution) for each boundary.

CEquivArea_Mnt

vector<su2double> CEulerSolver::CEquivArea_Mnt

protected

Equivalent area (inviscid contribution) for each boundary.

CkInflow

vector<su2matrix<complex<su2double> > > CEulerSolver::CkInflow

protected

CkOutflow1

vector<su2matrix<complex<su2double> > > CEulerSolver::CkOutflow1

protected

CkOutflow2

vector<su2matrix<complex<su2double> > > CEulerSolver::CkOutflow2

protected

dCL_dAlpha

su2double CEulerSolver::dCL_dAlpha

protected

Value of dCL_dAlpha used to control CL in fixed CL mode.

DensityIn

su2activematrix CEulerSolver::DensityIn

protected

DensityOut

su2activematrix CEulerSolver::DensityOut

protected

DonorGlobalIndex

vector<vector<unsigned long> > CEulerSolver::DonorGlobalIndex

protected

Value of the donor global index.

DonorPrimVar

vector<su2activematrix> CEulerSolver::DonorPrimVar

protected

Value of the donor variables at each boundary.

End_AoA_FD

bool CEulerSolver::End_AoA_FD = false

protected

Boolean for end of finite differencing for FixedCL mode.

Exhaust_Area

vector<su2double> CEulerSolver::Exhaust_Area

protected

Boundary total area.

Exhaust_MassFlow

vector<su2double> CEulerSolver::Exhaust_MassFlow

protected

Mass flow rate for each boundary.

Exhaust_MassFlow_Total

su2double CEulerSolver::Exhaust_MassFlow_Total = 0.0

protected

Mass flow rate for each boundary.

Exhaust_Pressure

vector<su2double> CEulerSolver::Exhaust_Pressure

protected

Fan face pressure for each boundary.

Exhaust_Temperature

vector<su2double> CEulerSolver::Exhaust_Temperature

protected

Fan face mach number for each boundary.

ExtAverageDensity

su2double CEulerSolver::ExtAverageDensity

protected

ExtAveragePressure

su2double CEulerSolver::ExtAveragePressure

protected

ExtAverageTurboVelocity

su2activevector CEulerSolver::ExtAverageTurboVelocity

protected

FluidModel

vector<CFluidModel*> CEulerSolver::FluidModel

protected

fluid model used in the solver.

Variables for outlier detection.

Inflow_Area

vector<su2double> CEulerSolver::Inflow_Area

protected

Boundary total area.

Inflow_Mach

vector<su2double> CEulerSolver::Inflow_Mach

protected

Fan face mach number for each boundary.

Inflow_Mach_Total

su2double CEulerSolver::Inflow_Mach_Total = 0.0

protected

Fan face mach number for each boundary.

Inflow_MassFlow

vector<su2double> CEulerSolver::Inflow_MassFlow

protected

Mass flow rate for each boundary.

Inflow_MassFlow_Total

su2double CEulerSolver::Inflow_MassFlow_Total = 0.0

protected

Mass flow rate for each boundary.

Inflow_Pressure

vector<su2double> CEulerSolver::Inflow_Pressure

protected

Fan face pressure for each boundary.

Inflow_Pressure_Total

su2double CEulerSolver::Inflow_Pressure_Total = 0.0

protected

Fan face pressure for each boundary.

InverseDesign

su2double CEulerSolver::InverseDesign = 0.0

protected

Inverse design functional for each boundary.

Iter_Update_AoA

unsigned long CEulerSolver::Iter_Update_AoA = 0

protected

Iteration at which AoA was updated last.

KineIn

su2activematrix CEulerSolver::KineIn

protected

KineOut

su2activematrix CEulerSolver::KineOut

protected

MeanTemperature

su2double CEulerSolver::MeanTemperature

protected

MixingState

vector<su2activematrix> CEulerSolver::MixingState

protected

nMixingStateVars

constexpr unsigned short CEulerSolver::nMixingStateVars = 8

staticconstexprprotected

Number of averaged variables transferred across mixing plane interfaces.

NuIn

su2activematrix CEulerSolver::NuIn

protected

NuOut

su2activematrix CEulerSolver::NuOut

protected

OldAverageDensity

su2activematrix CEulerSolver::OldAverageDensity

protected

OldAveragePressure

su2activematrix CEulerSolver::OldAveragePressure

protected

OldAverageTurboVelocity

vector<su2activematrix> CEulerSolver::OldAverageTurboVelocity

protected

OmegaIn

su2activematrix CEulerSolver::OmegaIn

protected

OmegaOut

su2activematrix CEulerSolver::OmegaOut

protected

Prandtl_Turb

su2double CEulerSolver::Prandtl_Turb = 0.0

protected

Turbulent Prandtl number.

PressureIn

su2activematrix CEulerSolver::PressureIn

protected

PressureOut

su2activematrix CEulerSolver::PressureOut

protected

RadialEquilibriumPressure

su2activematrix CEulerSolver::RadialEquilibriumPressure

protected

RelTangVelocityIn

su2activematrix CEulerSolver::RelTangVelocityIn

protected

RelTangVelocityOut

su2activematrix CEulerSolver::RelTangVelocityOut

protected

SpanTotalFlux

vector<su2activematrix> CEulerSolver::SpanTotalFlux

protected

Start_AoA_FD

bool CEulerSolver::Start_AoA_FD = false

protected

Boolean for start of finite differencing for FixedCL mode.

StdDevTemperature

su2double CEulerSolver::StdDevTemperature

protected

Total_Adiab_Eff

su2double CEulerSolver::Total_Adiab_Eff = 0.0

protected

Total Mass Flow Ratio for all the boundaries.

Total_AeroCD

su2double CEulerSolver::Total_AeroCD = 0.0

protected

Total aero drag coefficient for all the boundaries.

Total_ByPassProp_Eff

su2double CEulerSolver::Total_ByPassProp_Eff = 0.0

protected

Total Mass Flow Ratio for all the boundaries.

Total_CD_Prev

su2double CEulerSolver::Total_CD_Prev = 0.0

protected

Total drag coefficient for all the boundaries (fixed lift mode).

Total_CEquivArea

su2double CEulerSolver::Total_CEquivArea = 0.0

protected

Total Equivalent Area coefficient for all the boundaries.

Total_CL_Prev

su2double CEulerSolver::Total_CL_Prev = 0.0

protected

Total lift coefficient for all the boundaries (fixed lift mode).

Total_CMx_Prev

su2double CEulerSolver::Total_CMx_Prev = 0.0

protected

Total drag coefficient for all the boundaries (fixed lift mode).

Total_CMy_Prev

su2double CEulerSolver::Total_CMy_Prev = 0.0

protected

Total drag coefficient for all the boundaries (fixed lift mode).

Total_CMz_Prev

su2double CEulerSolver::Total_CMz_Prev = 0.0

protected

Total drag coefficient for all the boundaries (fixed lift mode).

Total_DC60

su2double CEulerSolver::Total_DC60 = 0.0

protected

Total IDC coefficient for all the boundaries.

Total_IDC

su2double CEulerSolver::Total_IDC = 0.0

protected

Total IDC coefficient for all the boundaries.

Total_IDC_Mach

su2double CEulerSolver::Total_IDC_Mach = 0.0

protected

Total IDC coefficient for all the boundaries.

Total_IDR

su2double CEulerSolver::Total_IDR = 0.0

protected

Total IDC coefficient for all the boundaries.

Total_MFR

su2double CEulerSolver::Total_MFR = 0.0

protected

Total Mass Flow Ratio for all the boundaries.

Total_NetThrust

su2double CEulerSolver::Total_NetThrust = 0.0

protected

Total drag coefficient for all the boundaries.

Total_Poly_Eff

su2double CEulerSolver::Total_Poly_Eff = 0.0

protected

Total Mass Flow Ratio for all the boundaries.

Total_Power

su2double CEulerSolver::Total_Power = 0.0

protected

Total drag coefficient for all the boundaries.

Total_Prop_Eff

su2double CEulerSolver::Total_Prop_Eff = 0.0

protected

Total Mass Flow Ratio for all the boundaries.

Total_ReverseFlow

su2double CEulerSolver::Total_ReverseFlow = 0.0

protected

Total drag coefficient for all the boundaries.

Total_SolidCD

su2double CEulerSolver::Total_SolidCD = 0.0

protected

Total drag coefficient for all the boundaries.

TurboVelocityIn

vector<su2activematrix> CEulerSolver::TurboVelocityIn

protected

TurboVelocityOut

vector<su2activematrix> CEulerSolver::TurboVelocityOut

protected

Update_AoA

bool CEulerSolver::Update_AoA = false

protected

Boolean to signal Angle of Attack Update.

---

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

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