CEulerSolver Class Reference

Main class for defining the Euler's flow solver. More...

#include <solver_structure.hpp>

Inheritance diagram for CEulerSolver:

Public Member Functions
	CEulerSolver (void)
	Constructor of the class.
	CEulerSolver (CGeometry *geometry, CConfig *config, unsigned short iMesh)
virtual	~CEulerSolver (void)
	Destructor of the class.
void	Set_MPI_Solution (CGeometry *geometry, CConfig *config)
	Impose the send-receive boundary condition. More...
void	Set_MPI_Solution_Gradient (CGeometry *geometry, CConfig *config)
	Impose the send-receive boundary condition. More...
void	Set_MPI_Solution_Old (CGeometry *geometry, CConfig *config)
	Impose the send-receive boundary condition. More...
void	Set_MPI_Solution_Limiter (CGeometry *geometry, CConfig *config)
	Impose the send-receive boundary condition. More...
void	Set_MPI_Primitive_Limiter (CGeometry *geometry, CConfig *config)
	Impose the send-receive boundary condition. More...
void	SetNondimensionalization (CGeometry *geometry, CConfig *config, unsigned short iMesh)
	Impose the send-receive boundary condition. More...
CFluidModel *	GetFluidModel (void)
	Compute the pressure at the infinity. More...
su2double	GetDensity_Inf (void)
	Compute the density at the infinity. More...
su2double	GetModVelocity_Inf (void)
	Compute 2-norm of the velocity at the infinity. More...
su2double	GetDensity_Energy_Inf (void)
	Compute the density multiply by energy at the infinity. More...
su2double	GetPressure_Inf (void)
	Compute the pressure at the infinity. More...
su2double	GetDensity_Velocity_Inf (unsigned short val_dim)
	Compute the density multiply by velocity at the infinity. More...
su2double	GetVelocity_Inf (unsigned short val_dim)
	Get the velocity at the infinity. More...
su2double *	GetVelocity_Inf (void)
	Get the velocity at the infinity. More...
void	SetTime_Step (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh, unsigned long Iteration)
	Compute the time step for solving the Euler equations. More...
void	Centered_Residual (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short iMesh, unsigned short iRKStep)
	Compute the spatial integration using a centered scheme. More...
void	Upwind_Residual (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short iMesh)
	Compute the spatial integration using a upwind scheme. More...
void	ComputeConsExtrapolation (CConfig *config)
	Compute the extrapolated quantities, for MUSCL upwind 2nd reconstruction, in a more thermodynamic consistent way. More...
void	Source_Residual (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CNumerics *second_numerics, CConfig *config, unsigned short iMesh)
	Source term integration. More...
void	Source_Template (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short iMesh)
	Source term integration. More...
void	Preprocessing (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh, unsigned short iRKStep, unsigned short RunTime_EqSystem, bool Output)
	Compute primitive variables and their gradients. More...
void	Postprocessing (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh)
	A virtual member. More...
unsigned long	SetPrimitive_Variables (CSolver **solver_container, CConfig *config, bool Output)
	Compute the velocity^2, SoundSpeed, Pressure, Enthalpy, Viscosity. More...
void	SetDissipation_Switch (CGeometry *geometry, CConfig *config)
	Compute a pressure sensor switch. More...
void	Set_MPI_Dissipation_Switch (CGeometry *geometry, CConfig *config)
	Parallelization of SetDissipation_Switch. More...
void	SetPrimitive_Gradient_GG (CGeometry *geometry, CConfig *config)
	Compute the gradient of the primitive variables using Green-Gauss method, and stores the result in the Gradient_Primitive variable. More...
void	SetPrimitive_Gradient_LS (CGeometry *geometry, CConfig *config)
	Compute the gradient of the primitive variables using a Least-Squares method, and stores the result in the Gradient_Primitive variable. More...
void	Set_MPI_Primitive_Gradient (CGeometry *geometry, CConfig *config)
	Compute the gradient of the primitive variables using Green-Gauss method, and stores the result in the Gradient_Primitive variable. More...
void	SetPrimitive_Limiter (CGeometry *geometry, CConfig *config)
	Compute the limiter of the primitive variables. More...
void	SetPreconditioner (CConfig *config, unsigned long iPoint)
	Compute the gradient of the primitive variables using a Least-Squares method, and stores the result in the Gradient_Primitive variable. More...
void	SetUndivided_Laplacian (CGeometry *geometry, CConfig *config)
	Compute the undivided laplacian for the solution, except the energy equation. More...
void	Set_MPI_Undivided_Laplacian (CGeometry *geometry, CConfig *config)
	Parallelization of Undivided Laplacian. More...
void	SetMax_Eigenvalue (CGeometry *geometry, CConfig *config)
	Compute the max eigenvalue. More...
void	Set_MPI_MaxEigenvalue (CGeometry *geometry, CConfig *config)
	Parallelization of the Max eigenvalue. More...
void	Set_MPI_ActDisk (CSolver **solver_container, CGeometry *geometry, CConfig *config)
	Parallelization of Undivided Laplacian. More...
void	Set_MPI_Nearfield (CGeometry *geometry, CConfig *config)
	Parallelization of Undivided Laplacian. More...
void	Set_MPI_Interface (CGeometry *geometry, CConfig *config)
	Parallelization of Undivided Laplacian. More...
void	Compute_ComboObj (CConfig *config)
	Compute weighted-sum "combo" objective output. More...
void	BC_Euler_Wall (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short val_marker)
	Impose via the residual the Euler wall boundary condition. More...
void	BC_Far_Field (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	Impose the far-field boundary condition using characteristics. More...
void	BC_Sym_Plane (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	Impose the symmetry boundary condition using the residual. More...
void	BC_Fluid_Interface (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config)
	Impose the interface state across sliding meshes. More...
void	BC_ActDisk_Inlet (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	Impose the engine inflow boundary condition. More...
void	BC_ActDisk_Outlet (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	Impose the engine exhaust boundary condition. More...
void	BC_ActDisk (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker, bool inlet_surface)
	Impose the engine inflow boundary condition. More...
void	BC_Interface_Boundary (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short val_marker)
	Impose the interface boundary condition using the residual. More...
void	BC_NearField_Boundary (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short val_marker)
	Impose the near-field boundary condition using the residual. More...
void	BC_Dirichlet (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short val_marker)
	Impose the dirichlet boundary condition using the residual. More...
void	BC_Riemann (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	Impose the boundary condition using characteristic recostruction. More...
void	BC_NonReflecting (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	Impose the boundary condition using characteristic recostruction. More...
void	BC_Inlet (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	Impose a subsonic inlet boundary condition. More...
void	BC_Supersonic_Inlet (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	Impose a supersonic inlet boundary condition. More...
void	BC_Supersonic_Outlet (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	Impose a supersonic outlet boundary condition. More...
void	BC_Custom (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short val_marker)
	Impose the dirichlet boundary condition. More...
void	BC_Outlet (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	Impose the outlet boundary condition. More...
void	BC_Engine_Inflow (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	Impose the nacelle inflow boundary condition. More...
void	BC_Engine_Exhaust (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker)
	Impose the ancelle exhaust boundary condition. More...
void	Mixing_Process (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short val_Marker)
	It avarage the fluxes value along a boundary. More...
void	MixedOut_Average (su2double val_init_pressure, su2double *val_Averaged_Flux, su2double *val_normal, su2double *pressure_mix, su2double *density_mix)
	it performs a mixed out average of the nodes of a boundary. More...
void	MixedOut_Root_Function (su2double *pressure, su2double *val_Averaged_Flux, su2double *val_normal, su2double *valfunc, su2double *density)
	it finds the root of an implicit equation that relates pressure and density. More...
void	Boundary_Fourier (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short val_Marker, vector< std::complex< su2double > > &c4k, signed long &nboundaryvertex)
	it performs a fourier transformation of a characteristic value. More...
void	Boundary_Fourier (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short val_Marker, vector< std::complex< su2double > > &c2k, vector< std::complex< su2double > > &c3k, signed long &nboundaryvertex)
	it performs a fourier transformation of a characteristic value. More...
void	SetExtAveragedValue (CSolver *solver_container, unsigned short intMarker, unsigned short extMarker)
	A virtual member. More...
su2double	GetAveragedDensity (unsigned short valMarker)
	Provide the average density at the boundary of interest. More...
su2double	GetAveragedTotPressure (unsigned short valMarker)
	Provide the average pressure at the boundary of interest. More...
su2double	GetTotalPressureLoss (unsigned short inMarkerTP)
	Provide Total Pressure Losses (turbomachinery performance). More...
su2double	GetKineticEnergyLoss (unsigned short inMarkerTP)
	Provide Kinetic Energy Losses (turbomachinery performance). More...
su2double	GetTotalTotalEfficiency (unsigned short inMarkerTP)
	Provide Total-Total Efficiency (turbomachinery performance). More...
su2double	GetTotalStaticEfficiency (unsigned short inMarkerTP)
	Provide Total-Static Efficiency (turbomachinery performance). More...
su2double	GetEulerianWork (unsigned short inMarkerTP)
	Provide the Eulerian Work (turbomachinery performance). More...
su2double	GetTotalEnthalpyIn (unsigned short inMarkerTP)
	Provide the Inlet Total Enthalpy (turbomachinery performance). More...
su2double	GetFlowAngleIn (unsigned short inMarkerTP)
	Provide the Inlet Flow Angle (turbomachinery performance). More...
su2double	GetFlowAngleOut (unsigned short inMarkerTP)
	Provide the Outlet Flow Angle (turbomachinery performance). More...
su2double	GetMassFlowIn (unsigned short inMarkerTP)
	Provide the Inlet Mass Flow (turbomachinery performance). More...
su2double	GetMassFlowOut (unsigned short inMarkerTP)
	Provide the Outlet Mass Flow (turbomachinery performance). More...
su2double	GetMachIn (unsigned short inMarkerTP)
	Provide the Inlet Mach number (turbomachinery performance). More...
su2double	GetMachOut (unsigned short inMarkerTP)
	Provide the Outlet Mach number (turbomachinery performance). More...
su2double	GetNormalMachIn (unsigned short inMarkerTP)
	Provide the normal component of the Inlet Mach number (turbomachinery performance). More...
su2double	GetNormalMachOut (unsigned short inMarkerTP)
	Provide the normal component of the Outlet Mach number (turbomachinery performance). More...
su2double	GetEnthalpyOut (unsigned short inMarkerTP)
	Provide the Outlet Enthalpy (turbomachinery performance). More...
su2double	GetVelocityOutIs (unsigned short inMarkerTP)
	Provide the Isentropic Outlet Velocity (turbomachinery performance). More...
su2double	GetPressureOut (unsigned short inMarkerTP)
	Provide the Outlet Pressure (turbomachinery performance). More...
su2double	GetPressureRatio (unsigned short inMarkerTP)
	Provide Pressure Ratio (tubomachinery performance). More...
su2double	GetAveragedTotTemperature (unsigned short valMarker)
	Provide Averaged Total Temperature at the boundary of interest. More...
su2double	GetAveragedPressure (unsigned short valMarker)
	Provide the Average pressure at the boundary of interest. More...
su2double	GetMassFlow (unsigned short valMarker)
	Provide the MassFlow at the boundary of interest. More...
su2double	GetFlowAngle (unsigned short valMarker)
	Provide the Flow Angle at the boundary of interest. More...
su2double	GetAveragedMach (unsigned short valMarker)
	Provide the Mach number at the boundary of interest. More...
su2double	GetAveragedNormalMach (unsigned short valMarker)
	Provide the Normal Mach number at the boundary of interest. More...
su2double	GetAveragedEnthalpy (unsigned short valMarker)
	Provide the average enthalpy at the boundary of interest. More...
su2double	GetAveragedEntropy (unsigned short valMarker)
	Provide the average pressure at the boundary of interest. More...
su2double *	GetAveragedVelocity (unsigned short valMarker)
	Provide the average pressure at the boundary of interest. More...
su2double *	GetAveragedGridVelocity (unsigned short valMarker)
	Provide the average grid velocity at the boundary of interest. More...
su2double	GetAveragedNormalVelocity (unsigned short valMarker)
	Provide the Average Normal Velocity at the boundary of interest. More...
su2double	GetAveragedTangVelocity (unsigned short valMarker)
	Provide the Tangent Velocity at the boundary of interest. More...
void	ExplicitRK_Iteration (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iRKStep)
	Update the solution using a Runge-Kutta scheme. More...
void	GetSurface_Properties (CGeometry *geometry, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short iMesh, bool Output)
	Compute the Fan face Mach number. More...
void	GetPower_Properties (CGeometry *geometry, CConfig *config, unsigned short iMesh, bool Output)
	Compute the Fan face Mach number. More...
void	GetSurface_Distortion (CGeometry *geometry, CConfig *config, unsigned short iMesh, bool Output)
	Compute the Fan face Mach number. More...
void	SetActDisk_BCThrust (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh, bool Output)
	Update the AoA and freestream velocity at the farfield. More...
void	SetFarfield_AoA (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh, bool Output)
	Update the AoA and freestream velocity at the farfield. More...
void	ExplicitEuler_Iteration (CGeometry *geometry, CSolver **solver_container, CConfig *config)
	Update the solution using the explicit Euler scheme. More...
void	ImplicitEuler_Iteration (CGeometry *geometry, CSolver **solver_container, CConfig *config)
	Update the solution using an implicit Euler scheme. More...
void	Pressure_Forces (CGeometry *geometry, CConfig *config)
	Compute the pressure forces and all the adimensional coefficients. More...
void	Momentum_Forces (CGeometry *geometry, CConfig *config)
	Compute the pressure forces and all the adimensional coefficients. More...
void	TurboPerformance (CSolver *solver, CConfig *config, unsigned short inMarker, unsigned short outMarker, unsigned short Kind_TurboPerf, unsigned short inMarkerTP)
	Compute turbomachinery performance. More...
void	StoreTurboPerformance (CSolver *solver, unsigned short inMarkerTP)
	Compute turbomachinery performance. More...
su2double	GetSlidingState (unsigned short val_marker, unsigned long val_vertex, unsigned short val_state)
	Get the outer state for fluid interface nodes. More...
su2double	GetCL_Inv (unsigned short val_marker)
	Provide the non dimensional lift coefficient (inviscid contribution). More...
su2double	GetCMz_Inv (unsigned short val_marker)
	Provide the non dimensional z moment coefficient (inviscid contribution). More...
su2double	GetSurface_CL (unsigned short val_marker)
	Provide the non dimensional lift coefficient. More...
su2double	GetSurface_CD (unsigned short val_marker)
	Provide the non dimensional drag coefficient. More...
su2double	GetSurface_CSF (unsigned short val_marker)
	Provide the non dimensional side-force coefficient. More...
su2double	GetSurface_CEff (unsigned short val_marker)
	Provide the non dimensional side-force coefficient. More...
su2double	GetSurface_CFx (unsigned short val_marker)
	Provide the non dimensional x force coefficient. More...
su2double	GetSurface_CFy (unsigned short val_marker)
	Provide the non dimensional y force coefficient. More...
su2double	GetSurface_CFz (unsigned short val_marker)
	Provide the non dimensional z force coefficient. More...
su2double	GetSurface_CMx (unsigned short val_marker)
	Provide the non dimensional x moment coefficient. More...
su2double	GetSurface_CMy (unsigned short val_marker)
	Provide the non dimensional y moment coefficient. More...
su2double	GetSurface_CMz (unsigned short val_marker)
	Provide the non dimensional z moment coefficient. More...
su2double	GetSurface_CL_Inv (unsigned short val_marker)
	Provide the non dimensional lift coefficient. More...
su2double	GetSurface_CD_Inv (unsigned short val_marker)
	Provide the non dimensional drag coefficient. More...
su2double	GetSurface_CSF_Inv (unsigned short val_marker)
	Provide the non dimensional side-force coefficient. More...
su2double	GetSurface_CEff_Inv (unsigned short val_marker)
	Provide the non dimensional side-force coefficient. More...
su2double	GetSurface_CFx_Inv (unsigned short val_marker)
	Provide the non dimensional x force coefficient. More...
su2double	GetSurface_CFy_Inv (unsigned short val_marker)
	Provide the non dimensional y force coefficient. More...
su2double	GetSurface_CFz_Inv (unsigned short val_marker)
	Provide the non dimensional z force coefficient. More...
su2double	GetSurface_CMx_Inv (unsigned short val_marker)
	Provide the non dimensional x moment coefficient. More...
su2double	GetSurface_CMy_Inv (unsigned short val_marker)
	Provide the non dimensional y moment coefficient. More...
su2double	GetSurface_CMz_Inv (unsigned short val_marker)
	Provide the non dimensional z moment coefficient. More...
su2double	GetSurface_CL_Mnt (unsigned short val_marker)
	Provide the non dimensional lift coefficient. More...
su2double	GetSurface_CD_Mnt (unsigned short val_marker)
	Provide the non dimensional drag coefficient. More...
su2double	GetSurface_CSF_Mnt (unsigned short val_marker)
	Provide the non dimensional side-force coefficient. More...
su2double	GetSurface_CEff_Mnt (unsigned short val_marker)
	Provide the non dimensional side-force coefficient. More...
su2double	GetSurface_CFx_Mnt (unsigned short val_marker)
	Provide the non dimensional x force coefficient. More...
su2double	GetSurface_CFy_Mnt (unsigned short val_marker)
	Provide the non dimensional y force coefficient. More...
su2double	GetSurface_CFz_Mnt (unsigned short val_marker)
	Provide the non dimensional z force coefficient. More...
su2double	GetSurface_CMx_Mnt (unsigned short val_marker)
	Provide the non dimensional x moment coefficient. More...
su2double	GetSurface_CMy_Mnt (unsigned short val_marker)
	Provide the non dimensional y moment coefficient. More...
su2double	GetSurface_CMz_Mnt (unsigned short val_marker)
	Provide the non dimensional z moment coefficient. More...
su2double	GetCD_Inv (unsigned short val_marker)
	Provide the non dimensional drag coefficient (inviscid contribution). More...
su2double	GetInflow_MassFlow (unsigned short val_marker)
	Provide the mass flow rate. More...
su2double	GetExhaust_MassFlow (unsigned short val_marker)
	Provide the mass flow rate. More...
su2double	GetInflow_Pressure (unsigned short val_marker)
	Provide the mass flow rate. More...
su2double	GetInflow_Mach (unsigned short val_marker)
	Provide the mass flow rate. More...
su2double	GetCSF_Inv (unsigned short val_marker)
	Provide the non dimensional sideforce coefficient (inviscid contribution). More...
su2double	GetCEff_Inv (unsigned short val_marker)
	Provide the non dimensional efficiency coefficient (inviscid contribution). More...
su2double	GetTotal_CSF (void)
	Provide the total (inviscid + viscous) non dimensional sideforce coefficient. More...
su2double	GetTotal_CEff (void)
	Provide the total (inviscid + viscous) non dimensional efficiency coefficient. More...
su2double	GetTotal_CEquivArea (void)
	Provide the total (inviscid + viscous) non dimensional Equivalent Area coefficient. More...
su2double	GetTotal_AeroCD (void)
	Provide the total (inviscid + viscous) non dimensional aero CD. More...
su2double	GetTotal_RadialDistortion (void)
	Provide the total (inviscid + viscous) non dimensional fan face distortion. More...
su2double	GetTotal_CircumferentialDistortion (void)
	Provide the total (inviscid + viscous) non dimensional fan face distortion. More...
su2double	GetTotal_CpDiff (void)
	Provide the total (inviscid + viscous) non dimensional Equivalent Area coefficient. More...
su2double	GetTotal_HeatFluxDiff (void)
	Provide the total (inviscid + viscous) non dimensional Equivalent Area coefficient. More...
su2double	GetTotal_CNearFieldOF (void)
	Provide the total (inviscid + viscous) non dimensional Near-Field pressure coefficient. More...
void	AddTotal_ComboObj (su2double val_obj)
	Add to the value of the total 'combo' objective. More...
void	SetTotal_CEquivArea (su2double val_cequivarea)
	Set the value of the Equivalent Area coefficient. More...
void	SetTotal_AeroCD (su2double val_aerocd)
	Set the value of the Aero drag. More...
void	SetTotal_RadialDistortion (su2double val_distortion)
	Set the value of the fan face distortion. More...
void	SetTotal_CircumferentialDistortion (su2double val_distortion)
	Set the value of the fan face distortion. More...
void	SetTotal_CpDiff (su2double val_pressure)
	Set the value of the Equivalent Area coefficient. More...
void	SetTotal_HeatFluxDiff (su2double val_heat)
	Set the value of the Equivalent Area coefficient. More...
void	SetTotal_CNearFieldOF (su2double val_cnearfieldpress)
	Set the value of the Near-Field pressure oefficient. More...
void	SetTotal_ComboObj (su2double ComboObj)
	Set the total "combo" objective (weighted sum of other values). More...
su2double	GetTotal_ComboObj (void)
	Provide the total "combo" objective (weighted sum of other values). More...
su2double	GetTotal_CL (void)
	Provide the total (inviscid + viscous) non dimensional lift coefficient. More...
su2double	GetTotal_CD (void)
	Provide the total (inviscid + viscous) non dimensional drag coefficient. More...
su2double	GetTotal_NetCThrust (void)
	Provide the total (inviscid + viscous) non dimensional drag coefficient. More...
su2double	GetTotal_Power (void)
	Provide the total (inviscid + viscous) non dimensional drag coefficient. More...
su2double	GetTotal_CD_SolidSurf (void)
	Provide the total (inviscid + viscous) non dimensional drag coefficient. More...
su2double	GetTotal_ReverseFlow (void)
	Provide the total (inviscid + viscous) non dimensional drag coefficient. More...
su2double	GetTotal_MFR (void)
	Provide the total (inviscid + viscous) non dimensional drag coefficient. More...
su2double	GetTotal_Prop_Eff (void)
	Provide the total (inviscid + viscous) non dimensional drag coefficient. More...
su2double	GetTotal_ByPassProp_Eff (void)
	Provide the total (inviscid + viscous) non dimensional drag coefficient. More...
su2double	GetTotal_Adiab_Eff (void)
	Provide the total (inviscid + viscous) non dimensional drag coefficient. More...
su2double	GetTotal_Poly_Eff (void)
	Provide the total (inviscid + viscous) non dimensional drag coefficient. More...
su2double	GetTotal_IDC (void)
	Provide the total (inviscid + viscous) non dimensional drag coefficient. More...
su2double	GetTotal_IDC_Mach (void)
	Provide the total (inviscid + viscous) non dimensional drag coefficient. More...
su2double	GetTotal_IDR (void)
	Provide the total (inviscid + viscous) non dimensional drag coefficient. More...
su2double	GetTotal_DC60 (void)
	Provide the total (inviscid + viscous) non dimensional drag coefficient. More...
su2double	GetTotal_Custom (void)
	Provide the total (inviscid + viscous) non dimensional drag coefficient. More...
su2double	GetTotal_CMx (void)
	Provide the total (inviscid + viscous) non dimensional x moment coefficient. More...
su2double	GetTotal_CMy (void)
	Provide the total (inviscid + viscous) non dimensional y moment coefficient. More...
su2double	GetTotal_CMz (void)
	Provide the total (inviscid + viscous) non dimensional z moment coefficient. More...
su2double	GetTotal_CFx (void)
	Provide the total (inviscid + viscous) non dimensional x force coefficient. More...
su2double	GetTotal_CFy (void)
	Provide the total (inviscid + viscous) non dimensional y force coefficient. More...
su2double	GetTotal_CFz (void)
	Provide the total (inviscid + viscous) non dimensional z force coefficient. More...
su2double	GetTotal_CT (void)
	Provide the total (inviscid + viscous) non dimensional thrust coefficient. More...
void	SetTotal_CT (su2double val_Total_CT)
	Store the total (inviscid + viscous) non dimensional thrust coefficient. More...
su2double	GetTotal_CQ (void)
	Provide the total (inviscid + viscous) non dimensional torque coefficient. More...
su2double	GetTotal_HeatFlux (void)
	Provide the total heat load. More...
su2double	GetTotal_MaxHeatFlux (void)
	Provide the total heat load. More...
void	SetTotal_CQ (su2double val_Total_CQ)
	Store the total (inviscid + viscous) non dimensional torque coefficient. More...
void	SetTotal_HeatFlux (su2double val_Total_Heat)
	Store the total heat load. More...
void	SetTotal_MaxHeatFlux (su2double val_Total_MaxHeat)
	Store the total heat load. More...
su2double	GetTotal_CMerit (void)
	Provide the total (inviscid + viscous) non dimensional rotor Figure of Merit. More...
void	SetTotal_CD (su2double val_Total_CD)
	Store the total (inviscid + viscous) non dimensional drag coefficient. More...
void	SetTotal_CL (su2double val_Total_CL)
	Store the total (inviscid + viscous) non dimensional lift coefficient. More...
void	SetTotal_NetCThrust (su2double val_Total_NetCThrust)
	Store the total (inviscid + viscous) non dimensional drag coefficient. More...
void	SetTotal_Power (su2double val_Total_Power)
	Store the total (inviscid + viscous) non dimensional drag coefficient. More...
void	SetTotal_CD_SolidSurf (su2double val_Total_CD_SolidSurf)
	Store the total (inviscid + viscous) non dimensional drag coefficient. More...
void	SetTotal_ReverseFlow (su2double val_ReverseFlow)
	Store the total (inviscid + viscous) non dimensional drag coefficient. More...
void	SetTotal_MFR (su2double val_Total_MFR)
	Store the total (inviscid + viscous) non dimensional drag coefficient. More...
void	SetTotal_Prop_Eff (su2double val_Total_Prop_Eff)
	Store the total (inviscid + viscous) non dimensional drag coefficient. More...
void	SetTotal_ByPassProp_Eff (su2double val_Total_ByPassProp_Eff)
	Store the total (inviscid + viscous) non dimensional drag coefficient. More...
void	SetTotal_Adiab_Eff (su2double val_Total_Adiab_Eff)
	Store the total (inviscid + viscous) non dimensional drag coefficient. More...
void	SetTotal_Poly_Eff (su2double val_Total_Poly_Eff)
	Store the total (inviscid + viscous) non dimensional drag coefficient. More...
void	SetTotal_IDC (su2double val_Total_IDC)
	Store the total (inviscid + viscous) non dimensional drag coefficient. More...
void	SetTotal_IDC_Mach (su2double val_Total_IDC_Mach)
	Store the total (inviscid + viscous) non dimensional drag coefficient. More...
void	SetTotal_IDR (su2double val_Total_IDR)
	Store the total (inviscid + viscous) non dimensional drag coefficient. More...
void	SetTotal_DC60 (su2double val_Total_DC60)
	Store the total (inviscid + viscous) non dimensional drag coefficient. More...
void	SetTotal_Custom (su2double val_Total_Custom, su2double val_coeff)
	Store the total (inviscid + viscous) non dimensional drag coefficient. More...
void	AddTotal_Custom (su2double val_Total_Custom, su2double val_coeff)
	Store the total (inviscid + viscous) non dimensional drag coefficient. More...
su2double	GetAllBound_CL_Inv (void)
	Get the inviscid contribution to the lift coefficient. More...
su2double	GetAllBound_CD_Inv (void)
	Get the inviscid contribution to the drag coefficient. More...
su2double	GetAllBound_CSF_Inv (void)
	Get the inviscid contribution to the sideforce coefficient. More...
su2double	GetAllBound_CEff_Inv (void)
	Get the inviscid contribution to the efficiency coefficient. More...
su2double	GetAllBound_CMx_Inv (void)
	Get the inviscid contribution to the efficiency coefficient. More...
su2double	GetAllBound_CMy_Inv (void)
	Get the inviscid contribution to the efficiency coefficient. More...
su2double	GetAllBound_CMz_Inv (void)
	Get the inviscid contribution to the efficiency coefficient. More...
su2double	GetAllBound_CFx_Inv (void)
	Get the inviscid contribution to the efficiency coefficient. More...
su2double	GetAllBound_CFy_Inv (void)
	Get the inviscid contribution to the efficiency coefficient. More...
su2double	GetAllBound_CFz_Inv (void)
	Get the inviscid contribution to the efficiency coefficient. More...
su2double	GetAllBound_CL_Mnt (void)
	Get the inviscid contribution to the lift coefficient. More...
su2double	GetAllBound_CD_Mnt (void)
	Get the inviscid contribution to the drag coefficient. More...
su2double	GetAllBound_CSF_Mnt (void)
	Get the inviscid contribution to the sideforce coefficient. More...
su2double	GetAllBound_CEff_Mnt (void)
	Get the inviscid contribution to the efficiency coefficient. More...
su2double	GetAllBound_CMx_Mnt (void)
	Get the inviscid contribution to the efficiency coefficient. More...
su2double	GetAllBound_CMy_Mnt (void)
	Get the inviscid contribution to the efficiency coefficient. More...
su2double	GetAllBound_CMz_Mnt (void)
	Get the inviscid contribution to the efficiency coefficient. More...
su2double	GetAllBound_CFx_Mnt (void)
	Get the inviscid contribution to the efficiency coefficient. More...
su2double	GetAllBound_CFy_Mnt (void)
	Get the inviscid contribution to the efficiency coefficient. More...
su2double	GetAllBound_CFz_Mnt (void)
	Get the inviscid contribution to the efficiency coefficient. More...
su2double	GetCPressure (unsigned short val_marker, unsigned long val_vertex)
	Provide the Pressure coefficient. More...
su2double	GetCPressureTarget (unsigned short val_marker, unsigned long val_vertex)
	Provide the Target Pressure coefficient. More...
void	SetCPressureTarget (unsigned short val_marker, unsigned long val_vertex, su2double val_pressure)
	Set the value of the target Pressure coefficient. More...
su2double *	GetCharacPrimVar (unsigned short val_marker, unsigned long val_vertex)
	Value of the characteristic variables at the boundaries. More...
void	SetCharacPrimVar (unsigned short val_marker, unsigned long val_vertex, unsigned short val_var, su2double val_value)
	Value of the characteristic variables at the boundaries. More...
su2double *	GetDonorPrimVar (unsigned short val_marker, unsigned long val_vertex)
	Value of the characteristic variables at the boundaries. More...
void	SetDonorPrimVar (unsigned short val_marker, unsigned long val_vertex, unsigned short val_var, su2double val_value)
	Value of the characteristic variables at the boundaries. More...
su2double	GetDonorPrimVar (unsigned short val_marker, unsigned long val_vertex, unsigned short val_var)
	Value of the characteristic variables at the boundaries. More...
unsigned long	GetDonorGlobalIndex (unsigned short val_marker, unsigned long val_vertex)
	Value of the characteristic global index at the boundaries. More...
void	SetDonorGlobalIndex (unsigned short val_marker, unsigned long val_vertex, unsigned long val_index)
	Value of the characteristic global index at the boundaries. More...
su2double	GetActDisk_DeltaP (unsigned short val_marker, unsigned long val_vertex)
	Value of the characteristic global index at the boundaries. More...
void	SetActDisk_DeltaP (unsigned short val_marker, unsigned long val_vertex, su2double val_deltap)
	Value of the characteristic global index at the boundaries. More...
su2double	GetActDisk_DeltaT (unsigned short val_marker, unsigned long val_vertex)
	Value of the characteristic global index at the boundaries. More...
void	SetActDisk_DeltaT (unsigned short val_marker, unsigned long val_vertex, su2double val_deltat)
	Value of the characteristic global index at the boundaries. More...
su2double	GetInlet_Ttotal (unsigned short val_marker, unsigned long val_vertex)
	Value of the characteristic global index at the boundaries. More...
su2double	GetInlet_Ptotal (unsigned short val_marker, unsigned long val_vertex)
	Value of the characteristic global index at the boundaries. More...
su2double	GetInlet_FlowDir (unsigned short val_marker, unsigned long val_vertex, unsigned short val_dim)
	Value of the characteristic global index at the boundaries. More...
void	SetInlet_Ttotal (unsigned short val_marker, unsigned long val_vertex, su2double val_ttotal)
	Value of the characteristic global index at the boundaries. More...
void	SetInlet_Ptotal (unsigned short val_marker, unsigned long val_vertex, su2double val_ptotal)
	Value of the characteristic global index at the boundaries. More...
void	SetInlet_FlowDir (unsigned short val_marker, unsigned long val_vertex, unsigned short val_dim, su2double val_flowdir)
	Value of the characteristic global index at the boundaries. More...
su2double	GetOneD_TotalPress (void)
	Provide the averaged total pressure at a marker.
void	SetOneD_TotalPress (su2double AveragePressure)
	Set the value of averaged total pressure. More...
su2double	GetOneD_Mach (void)
	Provide the averaged Mach number at a marker.
void	SetOneD_Mach (su2double AverageMach)
	Set the averaged Mach number at a marker.
su2double	GetOneD_Temp (void)
	Provide the averaged Temperature number at a marker.
void	SetOneD_Temp (su2double AverageTemperature)
	Set the averaged Temperature at a marker.
su2double	GetOneD_MassFlowRate (void)
	Provide the averaged mass flow rate at a marker.
void	SetOneD_MassFlowRate (su2double MassFlowRate)
	Set the averaged mass flow rate at a marker.
su2double	GetOneD_FluxAvgPress (void)
	Get the flux averaged pressure at a marker.(same as area averaged pressure)
void	SetOneD_FluxAvgPress (su2double PressureRef)
	Set the flux averaged pressure at a marker. (same as area averaged pressure)
su2double	GetOneD_FluxAvgDensity (void)
	Get the flux averaged density at a marker. ( = (gamma/(gamma-1)) / ( Pref*(href-1/2 uref^2) )
void	SetOneD_FluxAvgDensity (su2double DensityRef)
	Set the flux averaged density at a marker.( = (gamma/(gamma-1)) / ( Pref*(href-1/2 uref^2) )
su2double	GetOneD_FluxAvgVelocity (void)
	Get the flux averaged velocity at a marker. = \( \sqrt ( \int((rho*u)*u^2dA)/\int(rho*u*dA) )\).
void	SetOneD_FluxAvgVelocity (su2double VelocityRef)
	Set the flux averaged velocity at a marker. = \( sqrt ( \int((rho*u)*u^2dA)/\int(rho*u*dA) ) \).
su2double	GetOneD_FluxAvgEntalpy (void)
	Get the flux averaged enthalpy at a marker. = \( \int(rho*u*h dA) / \int(rho *u *dA ) \).
void	SetOneD_FluxAvgEntalpy (su2double EnthalpyRef)
	Set the flux averaged enthalpy at a marker. = \( \int(rho*u*h dA) / \int(rho *u *dA ) \).
void	SetResidual_DualTime (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iRKStep, unsigned short iMesh, unsigned short RunTime_EqSystem)
	Set the total residual adding the term that comes from the Dual Time Strategy. More...
void	SetFlow_Displacement (CGeometry **flow_geometry, CVolumetricMovement *flow_grid_movement, CConfig *flow_config, CConfig *fea_config, CGeometry **fea_geometry, CSolver ***fea_solution)
	A virtual member. More...
void	SetFlow_Displacement_Int (CGeometry **flow_geometry, CVolumetricMovement *flow_grid_movement, CConfig *flow_config, CConfig *fea_config, CGeometry **fea_geometry, CSolver ***fea_solution)
	A virtual member. More...
void	LoadRestart (CGeometry **geometry, CSolver ***solver, CConfig *config, int val_iter)
	Load a solution from a restart file. More...
void	SetSlidingState (unsigned short val_marker, unsigned long val_vertex, unsigned short val_state, su2double component)
	Set the outer state for fluid interface nodes. More...
void	SetInitialCondition (CGeometry **geometry, CSolver ***solver_container, CConfig *config, unsigned long ExtIter)
	Set the initial condition for the Euler Equations. More...
void	SetPressure_Inf (su2double p_inf)
	Set the freestream pressure. More...
void	SetTemperature_Inf (su2double t_inf)
	Set the freestream temperature. More...
void	SetFreeStream_Solution (CConfig *config)
	Set the solution using the Freestream values. More...
Public Member Functions inherited from CSolver
	CSolver (void)
	Constructor of the class.
virtual	~CSolver (void)
	Destructor of the class.
void	SetIterLinSolver (unsigned short val_iterlinsolver)
	Set number of linear solver iterations. More...
virtual void	Set_MPI_Primitive (CGeometry *geometry, CConfig *config)
	Set number of linear solver iterations. More...
void	SetResidual_RMS (CGeometry *geometry, CConfig *config)
	Set number of linear solver iterations. More...
virtual void	Set_MPI_Solution_DispOnly (CGeometry *geometry, CConfig *config)
	Impose the send-receive boundary condition for velocities and accelerations in structural solutions. More...
virtual void	Set_MPI_Solution_Pred (CGeometry *geometry, CConfig *config)
	Impose the send-receive boundary condition for predicted FSI structural solutions. More...
virtual void	Set_MPI_Solution_Pred_Old (CGeometry *geometry, CConfig *config)
	Impose the send-receive boundary condition for old predicted FSI structural solutions. More...
unsigned short	GetIterLinSolver (void)
	Get number of linear solver iterations. More...
su2double	GetMax_Delta_Time (void)
	Get the value of the maximum delta time. More...
su2double	GetMin_Delta_Time (void)
	Get the value of the minimum delta time. More...
virtual su2double	GetMax_Delta_Time (unsigned short val_Species)
	Get the value of the maximum delta time. More...
virtual su2double	GetMin_Delta_Time (unsigned short val_Species)
	Get the value of the minimum delta time. More...
unsigned short	GetnVar (void)
	Get the number of variables of the problem.
unsigned short	GetnPrimVar (void)
	Get the number of variables of the problem.
unsigned short	GetnPrimVarGrad (void)
	Get the number of variables of the problem.
unsigned short	GetnSecondaryVar (void)
	Get the number of variables of the problem.
unsigned short	GetnSecondaryVarGrad (void)
	Get the number of variables of the problem.
unsigned short	GetnOutputVariables (void)
	Get the number of variables of the problem.
void	SetRes_RMS (unsigned short val_var, su2double val_residual)
	Set the maximal residual, this is useful for the convergence history. More...
void	AddRes_RMS (unsigned short val_var, su2double val_residual)
	Adds the maximal residual, this is useful for the convergence history. More...
su2double	GetRes_RMS (unsigned short val_var)
	Get the maximal residual, this is useful for the convergence history. More...
void	SetRes_Max (unsigned short val_var, su2double val_residual, unsigned long val_point)
	Set the maximal residual, this is useful for the convergence history. More...
void	AddRes_Max (unsigned short val_var, su2double val_residual, unsigned long val_point, su2double *val_coord)
	Adds the maximal residual, this is useful for the convergence history. More...
su2double	GetRes_Max (unsigned short val_var)
	Get the maximal residual, this is useful for the convergence history. More...
virtual su2double	GetRes_FEM (unsigned short val_var)
	Get the residual for FEM structural analysis. More...
unsigned long	GetPoint_Max (unsigned short val_var)
	Get the maximal residual, this is useful for the convergence history. More...
su2double *	GetPoint_Max_Coord (unsigned short val_var)
	Get the location of the maximal residual, this is useful for the convergence history. More...
void	SetGrid_Movement_Residual (CGeometry *geometry, CConfig *config)
	Set Value of the residual if there is a grid movement. More...
void	SetAuxVar_Gradient_GG (CGeometry *geometry, CConfig *config)
	Compute the Green-Gauss gradient of the auxiliary variable. More...
void	SetAuxVar_Gradient_LS (CGeometry *geometry, CConfig *config)
	Compute the Least Squares gradient of the auxiliary variable. More...
void	SetAuxVar_Surface_Gradient (CGeometry *geometry, CConfig *config)
	Compute the Least Squares gradient of an auxiliar variable on the profile surface. More...
void	SetSolution_Gradient_GG (CGeometry *geometry, CConfig *config)
	Compute the Green-Gauss gradient of the solution. More...
void	SetSolution_Gradient_LS (CGeometry *geometry, CConfig *config)
	Compute the Least Squares gradient of the solution. More...
void	SetGridVel_Gradient (CGeometry *geometry, CConfig *config)
	Compute the Least Squares gradient of the grid velocity. More...
void	SetSolution_Limiter (CGeometry *geometry, CConfig *config)
	Compute slope limiter. More...
void	SetPressureLaplacian (CGeometry *geometry, CConfig *config, su2double *PressureLaplacian)
	A virtual member. More...
void	Set_OldSolution (CGeometry *geometry)
	Set the old solution variables to the current solution value for Runge-Kutta iteration. More...
void	Restart_OldGeometry (CGeometry *geometry, CConfig *config)
	Load the geometries at the previous time states n and nM1. More...
virtual void	Postprocessing (CGeometry *geometry, CSolver **solver_container, CConfig *config, CNumerics **numerics, unsigned short iMesh)
	A virtual member, overloaded. More...
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. More...
virtual void	BC_Clamped (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short val_marker)
	A virtual member. More...
virtual void	BC_Clamped_Post (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short val_marker)
	A virtual member. More...
virtual void	BC_Normal_Displacement (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short val_marker)
	A virtual member. More...
virtual void	BC_Normal_Load (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short val_marker)
	A virtual member. More...
virtual void	BC_Dir_Load (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short val_marker)
	A virtual member. More...
virtual void	BC_Sine_Load (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short val_marker)
	A virtual member. More...
virtual void	BC_Pressure (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short val_marker)
	A virtual member. More...
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. More...
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. More...
virtual void	BC_Neumann (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short val_marker)
	A virtual member. More...
virtual void	BC_Dielec (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short val_marker)
	A virtual member. More...
virtual void	BC_Electrode (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short val_marker)
	A virtual member. More...
virtual void	ImplicitNewmark_Iteration (CGeometry *geometry, CSolver **solver_container, CConfig *config)
	A virtual member. More...
virtual void	ImplicitNewmark_Update (CGeometry *geometry, CSolver **solver_container, CConfig *config)
	A virtual member. More...
virtual void	ImplicitNewmark_Relaxation (CGeometry *geometry, CSolver **solver_container, CConfig *config)
	A virtual member. More...
virtual void	GeneralizedAlpha_Iteration (CGeometry *geometry, CSolver **solver_container, CConfig *config)
	A virtual member. More...
virtual void	GeneralizedAlpha_UpdateDisp (CGeometry *geometry, CSolver **solver_container, CConfig *config)
	A virtual member. More...
virtual void	GeneralizedAlpha_UpdateSolution (CGeometry *geometry, CSolver **solver_container, CConfig *config)
	A virtual member. More...
virtual void	GeneralizedAlpha_UpdateLoads (CGeometry *geometry, CSolver **solver_container, CConfig *config)
	A virtual member. More...
virtual void	Compute_Residual (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh)
	A virtual member. More...
virtual void	Inviscid_DeltaForces (CGeometry *geometry, CSolver **solver_container, CConfig *config)
	A virtual member. More...
virtual void	Friction_Forces (CGeometry *geometry, CConfig *config)
	A virtual member. More...
virtual void	Viscous_DeltaForces (CGeometry *geometry, CConfig *config)
	A virtual member. More...
virtual void	Wave_Strength (CGeometry *geometry, CConfig *config)
	A virtual member. More...
virtual void	SetPrimitive_Limiter_MPI (CGeometry *geometry, CConfig *config)
	A virtual member. More...
virtual void	Viscous_Residual (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short iMesh, unsigned short iRKStep)
	A virtual member. More...
virtual void	AddStiffMatrix (su2double **StiffMatrix_Elem, unsigned long Point_0, unsigned long Point_1, unsigned long Point_2, unsigned long Point_3)
	A virtual member. More...
virtual void	SetCSensitivity (unsigned short val_marker, unsigned long val_vertex, su2double val_sensitivity)
	A virtual member. More...
virtual void	SetForceProj_Vector (CGeometry *geometry, CSolver **solver_container, CConfig *config)
	A virtual member. More...
virtual void	SetIntBoundary_Jump (CGeometry *geometry, CSolver **solver_container, CConfig *config)
	A virtual member. More...
virtual void	SetDistance (CGeometry *geometry, CConfig *config)
	A virtual member. More...
virtual void	Inviscid_Sensitivity (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config)
	A virtual member. More...
virtual void	Smooth_Sensitivity (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config)
	A virtual member. More...
virtual void	Viscous_Sensitivity (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config)
	A virtual member. More...
virtual su2double	GetCL_Visc (unsigned short val_marker)
	A virtual member. More...
virtual su2double	GetCMz_Visc (unsigned short val_marker)
	Get the non dimensional z moment coefficient (viscous contribution). More...
virtual su2double	GetSurface_CL_Visc (unsigned short val_marker)
	A virtual member. More...
virtual su2double	GetSurface_CD_Visc (unsigned short val_marker)
	A virtual member. More...
virtual su2double	GetSurface_CSF_Visc (unsigned short val_marker)
	A virtual member. More...
virtual su2double	GetSurface_CEff_Visc (unsigned short val_marker)
	A virtual member. More...
virtual su2double	GetSurface_CFx_Visc (unsigned short val_marker)
	A virtual member. More...
virtual su2double	GetSurface_CFy_Visc (unsigned short val_marker)
	A virtual member. More...
virtual su2double	GetSurface_CFz_Visc (unsigned short val_marker)
	A virtual member. More...
virtual su2double	GetSurface_CMx_Visc (unsigned short val_marker)
	A virtual member. More...
virtual su2double	GetSurface_CMy_Visc (unsigned short val_marker)
	A virtual member. More...
virtual su2double	GetSurface_CMz_Visc (unsigned short val_marker)
	A virtual member. More...
virtual su2double	GetCSF_Visc (unsigned short val_marker)
	A virtual member. More...
virtual su2double	GetSurface_HF_Visc (unsigned short val_marker)
	A virtual member. More...
virtual su2double	GetSurface_MaxHF_Visc (unsigned short val_marker)
	A virtual member. More...
virtual su2double	GetCD_Visc (unsigned short val_marker)
	A virtual member. More...
virtual su2double	Get_PressureDrag (void)
	Provide the total (inviscid + viscous) non dimensional drag coefficient. More...
virtual su2double	Get_ViscDrag (void)
	Provide the total (inviscid + viscous) non dimensional drag coefficient. More...
virtual su2double	GetTotal_CFEA (void)
	A virtual member. More...
virtual void	SetTotal_CFEA (su2double val_cfea)
	A virtual member. More...
virtual su2double	GetTotal_CWave (void)
	A virtual member. More...
virtual su2double	GetTotal_CHeat (void)
	A virtual member. More...
virtual su2double	GetAllBound_CL_Visc (void)
	A virtual member. More...
virtual su2double	GetAllBound_CD_Visc (void)
	A virtual member. More...
virtual su2double	GetAllBound_CSF_Visc (void)
	A virtual member. More...
virtual su2double	GetAllBound_CEff_Visc (void)
	A virtual member. More...
virtual su2double	GetAllBound_CMx_Visc (void)
	A virtual member. More...
virtual su2double	GetAllBound_CMy_Visc (void)
	A virtual member. More...
virtual su2double	GetAllBound_CMz_Visc (void)
	A virtual member. More...
virtual su2double	GetAllBound_CFx_Visc (void)
	A virtual member. More...
virtual su2double	GetAllBound_CFy_Visc (void)
	A virtual member. More...
virtual su2double	GetAllBound_CFz_Visc (void)
	A virtual member. More...
virtual void	SetDonorAdjVar (unsigned short val_marker, unsigned long val_vertex, unsigned short val_var, su2double val_value)
	A virtual member. More...
virtual su2double *	GetDonorAdjVar (unsigned short val_marker, unsigned long val_vertex)
	A virtual member. More...
virtual su2double	GetDonorAdjVar (unsigned short val_marker, unsigned long val_vertex, unsigned short val_var)
	A virtual member. More...
virtual su2double	GetCSkinFriction (unsigned short val_marker, unsigned long val_vertex, unsigned short val_dim)
	A virtual member. More...
virtual su2double	GetHeatFlux (unsigned short val_marker, unsigned long val_vertex)
	A virtual member. More...
virtual su2double	GetHeatFluxTarget (unsigned short val_marker, unsigned long val_vertex)
	A virtual member. More...
virtual void	SetHeatFluxTarget (unsigned short val_marker, unsigned long val_vertex, su2double val_heat)
	A virtual member. More...
virtual su2double	GetYPlus (unsigned short val_marker, unsigned long val_vertex)
	A virtual member. More...
virtual su2double	GetStrainMag_Max (void)
	A virtual member. More...
virtual su2double	GetOmega_Max (void)
	A virtual member. More...
virtual void	SetStrainMag_Max (su2double val_strainmag_max)
	A virtual member. More...
virtual void	SetOmega_Max (su2double val_omega_max)
	A virtual member. More...
virtual su2double	GetPsiRho_Inf (void)
	A virtual member. More...
virtual su2double *	GetPsiRhos_Inf (void)
	A virtual member. More...
virtual su2double	GetPsiE_Inf (void)
	A virtual member. More...
virtual su2double	GetPhi_Inf (unsigned short val_dim)
	A virtual member. More...
virtual su2double	GetTotal_Sens_Geo (void)
	A virtual member. More...
virtual su2double	GetTotal_Sens_Mach (void)
	A virtual member. More...
virtual su2double	GetTotal_Sens_AoA (void)
	A virtual member. More...
virtual su2double	GetTotal_Sens_Press (void)
	Set the total farfield pressure sensitivity coefficient. More...
virtual su2double	GetTotal_Sens_Temp (void)
	Set the total farfield temperature sensitivity coefficient. More...
virtual su2double	GetTotal_Sens_BPress (void)
	Get the total back pressure sensitivity coefficient. More...
virtual su2double	GetDensity_Inf (unsigned short val_var)
	A virtual member. More...
virtual su2double	GetDensity_Velocity_Inf (unsigned short val_dim, unsigned short val_var)
	A virtual member. More...
virtual su2double	GetViscosity_Inf (void)
	A virtual member. More...
virtual su2double	GetTke_Inf (void)
	A virtual member. More...
virtual su2double	GetCSensitivity (unsigned short val_marker, unsigned long val_vertex)
	A virtual member. More...
virtual su2double *	GetConstants ()
	A virtual member. More...
virtual void	SetFEA_Load (CSolver ***flow_solution, CGeometry **fea_geometry, CGeometry **flow_geometry, CConfig *fea_config, CConfig *flow_config, CNumerics *fea_numerics)
	A virtual member. More...
virtual void	SetFEA_Load_Int (CSolver ***flow_solution, CGeometry **fea_geometry, CGeometry **flow_geometry, CConfig *fea_config, CConfig *flow_config, CNumerics *fea_numerics)
	A virtual member. More...
virtual void	Copy_Zone_Solution (CSolver ***solver1_solution, CGeometry **solver1_geometry, CConfig *solver1_config, CSolver ***solver2_solution, CGeometry **solver2_geometry, CConfig *solver2_config)
	A virtual member. More...
virtual void	ResetInitialCondition (CGeometry **geometry, CSolver ***solver_container, CConfig *config, unsigned long ExtIter)
	A virtual member. More...
virtual void	PredictStruct_Displacement (CGeometry **fea_geometry, CConfig *fea_config, CSolver ***fea_solution)
	A virtual member. More...
virtual void	ComputeAitken_Coefficient (CGeometry **fea_geometry, CConfig *fea_config, CSolver ***fea_solution, unsigned long iFSIIter)
	A virtual member. More...
virtual void	SetAitken_Relaxation (CGeometry **fea_geometry, CConfig *fea_config, CSolver ***fea_solution)
	A virtual member. More...
virtual void	Update_StructSolution (CGeometry **fea_geometry, CConfig *fea_config, CSolver ***fea_solution)
	A virtual member. More...
virtual void	LoadRestart_FSI (CGeometry *geometry, CSolver ***solver, CConfig *config, int val_iter)
	A virtual member. More...
void	Gauss_Elimination (su2double **A, su2double *rhs, unsigned short nVar)
	Gauss method for solving a linear system. More...
void	Aeroelastic (CSurfaceMovement *surface_movement, CGeometry *geometry, CConfig *config, unsigned long ExtIter)
	Prepares and solves the aeroelastic equations. More...
void	SetUpTypicalSectionWingModel (vector< vector< su2double > > &PHI, vector< su2double > &w, CConfig *config)
	Sets up the generalized eigenvectors and eigenvalues needed to solve the aeroelastic equations. More...
void	SolveTypicalSectionWingModel (CGeometry *geometry, su2double Cl, su2double Cm, CConfig *config, unsigned short val_Marker, vector< su2double > &displacements)
	Solve the typical section wing model. More...
virtual void	RegisterSolution (CGeometry *geometry, CConfig *config)
	A virtual member. More...
virtual void	RegisterOutput (CGeometry *geometry, CConfig *config)
	A virtual member. More...
virtual void	SetAdjoint_Output (CGeometry *geometry, CConfig *config)
	A virtual member. More...
virtual void	ExtractAdjoint_Solution (CGeometry *geometry, CConfig *config)
	A virtual member. More...
virtual void	RegisterObj_Func (CConfig *config)
	A virtual member. More...
virtual void	SetSurface_Sensitivity (CGeometry *geometry, CConfig *config)
	A virtual member. More...
virtual void	SetSensitivity (CGeometry *geometry, CConfig *config)
	A virtual member. More...
virtual void	SetAdj_ObjFunc (CGeometry *geometry, CConfig *config)
virtual void	SetFSI_ConvValue (unsigned short val_index, su2double val_criteria)
	A virtual member. More...
virtual su2double	GetFSI_ConvValue (unsigned short val_index)
	A virtual member. More...
virtual void	Set_Prestretch (CGeometry *geometry, CConfig *config)
	A virtual member. More...
virtual void	Compute_StiffMatrix (CGeometry *geometry, CSolver **solver_container, CNumerics **numerics, CConfig *config)
	A virtual member. More...
virtual void	Compute_StiffMatrix_NodalStressRes (CGeometry *geometry, CSolver **solver_container, CNumerics **numerics, CConfig *config)
	A virtual member. More...
virtual void	Compute_MassMatrix (CGeometry *geometry, CSolver **solver_container, CNumerics **numerics, CConfig *config)
	A virtual member. More...
virtual void	Compute_NodalStressRes (CGeometry *geometry, CSolver **solver_container, CNumerics **numerics, CConfig *config)
	A virtual member. More...
virtual void	Compute_NodalStress (CGeometry *geometry, CSolver **solver_container, CNumerics **numerics, CConfig *config)
	A virtual member. More...
virtual void	Compute_DeadLoad (CGeometry *geometry, CSolver **solver_container, CNumerics **numerics, CConfig *config)
	A virtual member. More...
virtual void	Solve_System (CGeometry *geometry, CSolver **solver_container, CConfig *config)
	A virtual member. More...
virtual void	Initialize_SystemMatrix (CGeometry *geometry, CSolver **solver_container, CConfig *config)
	A virtual member. More...
virtual void	Compute_IntegrationConstants (CConfig *config)
	A virtual member. More...
virtual su2double	GetWAitken_Dyn (void)
	A virtual member. More...
virtual su2double	GetWAitken_Dyn_tn1 (void)
	A virtual member. More...
virtual void	SetWAitken_Dyn (su2double waitk)
	A virtual member. More...
virtual void	SetWAitken_Dyn_tn1 (su2double waitk_tn1)
	A virtual member. More...
virtual void	SetLoad_Increment (su2double val_loadIncrement)
	A virtual member. More...
virtual void	SetRecording (CGeometry *geometry, CConfig *config, unsigned short kind_recording)
	A virtual member. More...
virtual void	RegisterVariables (CGeometry *geometry, CConfig *config, bool reset=false)
	A virtual member. More...
virtual void	ExtractAdjoint_Variables (CGeometry *geometry, CConfig *config)
	A virtual member. More...

Static Public Member Functions
static bool	Compareval (std::vector< su2double > a, std::vector< su2double > b)
	compare to values. More...

Protected Attributes
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
	Energy at the infinity.
su2double	Pressure_Inf
	Pressure at the infinity.
su2double *	Velocity_Inf
	Flow Velocity vector at the infinity.
su2double *	CD_Inv
	Drag coefficient (inviscid contribution) for each boundary.
su2double *	CL_Inv
	Lift coefficient (inviscid contribution) for each boundary.
su2double *	CSF_Inv
	Sideforce coefficient (inviscid contribution) for each boundary.
su2double *	CMx_Inv
	x Moment coefficient (inviscid contribution) for each boundary.
su2double *	CMy_Inv
	y Moment coefficient (inviscid contribution) for each boundary.
su2double *	CMz_Inv
	z Moment coefficient (inviscid contribution) for each boundary.
su2double *	CFx_Inv
	x Force coefficient (inviscid contribution) for each boundary.
su2double *	CFy_Inv
	y Force coefficient (inviscid contribution) for each boundary.
su2double *	CFz_Inv
	z Force coefficient (inviscid contribution) for each boundary.
su2double *	Surface_CL_Inv
	Lift coefficient (inviscid contribution) for each monitoring surface.
su2double *	Surface_CD_Inv
	Drag coefficient (inviscid contribution) for each monitoring surface.
su2double *	Surface_CSF_Inv
	Side-force coefficient (inviscid contribution) for each monitoring surface.
su2double *	Surface_CEff_Inv
	Side-force coefficient (inviscid contribution) for each monitoring surface.
su2double *	Surface_CFx_Inv
	x Force coefficient (inviscid contribution) for each monitoring surface.
su2double *	Surface_CFy_Inv
	y Force coefficient (inviscid contribution) for each monitoring surface.
su2double *	Surface_CFz_Inv
	z Force coefficient (inviscid contribution) for each monitoring surface.
su2double *	Surface_CMx_Inv
	x Moment coefficient (inviscid contribution) for each monitoring surface.
su2double *	Surface_CMy_Inv
	y Moment coefficient (inviscid contribution) for each monitoring surface.
su2double *	Surface_CMz_Inv
	z Moment coefficient (inviscid contribution) for each monitoring surface.
su2double *	CEff_Inv
	Efficiency (Cl/Cd) (inviscid contribution) for each boundary.
su2double *	CMerit_Inv
	Rotor Figure of Merit (inviscid contribution) for each boundary.
su2double *	CT_Inv
	Thrust coefficient (force in -x direction, inviscid contribution) for each boundary.
su2double *	CQ_Inv
	Torque coefficient (moment in -x direction, inviscid contribution) for each boundary.
su2double *	CEquivArea_Inv
	Equivalent area (inviscid contribution) for each boundary.
su2double *	CNearFieldOF_Inv
	Near field pressure (inviscid contribution) for each boundary.
su2double *	CD_Mnt
	Drag coefficient (inviscid contribution) for each boundary.
su2double *	CL_Mnt
	Lift coefficient (inviscid contribution) for each boundary.
su2double *	CSF_Mnt
	Sideforce coefficient (inviscid contribution) for each boundary.
su2double *	CMx_Mnt
	x Moment coefficient (inviscid contribution) for each boundary.
su2double *	CMy_Mnt
	y Moment coefficient (inviscid contribution) for each boundary.
su2double *	CMz_Mnt
	z Moment coefficient (inviscid contribution) for each boundary.
su2double *	CFx_Mnt
	x Force coefficient (inviscid contribution) for each boundary.
su2double *	CFy_Mnt
	y Force coefficient (inviscid contribution) for each boundary.
su2double *	CFz_Mnt
	z Force coefficient (inviscid contribution) for each boundary.
su2double *	Surface_CL_Mnt
	Lift coefficient (inviscid contribution) for each monitoring surface.
su2double *	Surface_CD_Mnt
	Drag coefficient (inviscid contribution) for each monitoring surface.
su2double *	Surface_CSF_Mnt
	Side-force coefficient (inviscid contribution) for each monitoring surface.
su2double *	Surface_CEff_Mnt
	Side-force coefficient (inviscid contribution) for each monitoring surface.
su2double *	Surface_CFx_Mnt
	x Force coefficient (inviscid contribution) for each monitoring surface.
su2double *	Surface_CFy_Mnt
	y Force coefficient (inviscid contribution) for each monitoring surface.
su2double *	Surface_CFz_Mnt
	z Force coefficient (inviscid contribution) for each monitoring surface.
su2double *	Surface_CMx_Mnt
	x Moment coefficient (inviscid contribution) for each monitoring surface.
su2double *	Surface_CMy_Mnt
	y Moment coefficient (inviscid contribution) for each monitoring surface.
su2double *	Surface_CMz_Mnt
	z Moment coefficient (inviscid contribution) for each monitoring surface.
su2double *	CEff_Mnt
	Efficiency (Cl/Cd) (inviscid contribution) for each boundary.
su2double *	CMerit_Mnt
	Rotor Figure of Merit (inviscid contribution) for each boundary.
su2double *	CT_Mnt
	Thrust coefficient (force in -x direction, inviscid contribution) for each boundary.
su2double *	CQ_Mnt
	Torque coefficient (moment in -x direction, inviscid contribution) for each boundary.
su2double *	CEquivArea_Mnt
	Equivalent area (inviscid contribution) for each boundary.
su2double **	CPressure
	Pressure coefficient for each boundary and vertex.
su2double **	CPressureTarget
	Target Pressure coefficient for each boundary and vertex.
su2double **	HeatFlux
	Heat transfer coefficient for each boundary and vertex.
su2double **	HeatFluxTarget
	Heat transfer coefficient for each boundary and vertex.
su2double **	YPlus
	Yplus for each boundary and vertex.
su2double ***	CharacPrimVar
	Value of the characteristic variables at each boundary.
su2double ***	DonorPrimVar
	Value of the donor variables at each boundary.
su2double *	ForceInviscid
	Inviscid force for each boundary.
su2double *	MomentInviscid
	Inviscid moment for each boundary.
su2double *	ForceMomentum
	Inviscid force for each boundary.
su2double *	MomentMomentum
	Inviscid moment for each boundary.
su2double *	Inflow_MassFlow
	Mass flow rate for each boundary.
su2double *	Exhaust_MassFlow
	Mass flow rate for each boundary.
su2double *	Inflow_Pressure
	Fan face pressure for each boundary.
su2double *	Inflow_Mach
	Fan face mach number for each boundary.
su2double *	Inflow_Area
	Boundary total area.
su2double *	Exhaust_Area
	Boundary total area.
su2double *	Exhaust_Pressure
	Fan face pressure for each boundary.
su2double *	Exhaust_Temperature
	Fan face mach number for each boundary.
su2double	Inflow_MassFlow_Total
	Mass flow rate for each boundary.
su2double	Exhaust_MassFlow_Total
	Mass flow rate for each boundary.
su2double	Inflow_Pressure_Total
	Fan face pressure for each boundary.
su2double	Inflow_Mach_Total
	Fan face mach number for each boundary.
su2double	InverseDesign
	Inverse design functional for each boundary.
unsigned long **	DonorGlobalIndex
	Value of the donor global index.
su2double **	ActDisk_DeltaP
	Value of the Delta P.
su2double **	ActDisk_DeltaT
	Value of the Delta T.
su2double **	Inlet_Ptotal
	Value of the Total P.
su2double **	Inlet_Ttotal
	Value of the Total T.
su2double ***	Inlet_FlowDir
	Value of the Flow Direction.
su2double	AllBound_CD_Inv
	Total drag coefficient (inviscid contribution) for all the boundaries.
su2double	AllBound_CL_Inv
	Total lift coefficient (inviscid contribution) for all the boundaries.
su2double	AllBound_CSF_Inv
	Total sideforce coefficient (inviscid contribution) for all the boundaries.
su2double	AllBound_CMx_Inv
	Total x moment coefficient (inviscid contribution) for all the boundaries.
su2double	AllBound_CMy_Inv
	Total y moment coefficient (inviscid contribution) for all the boundaries.
su2double	AllBound_CMz_Inv
	Total z moment coefficient (inviscid contribution) for all the boundaries.
su2double	AllBound_CFx_Inv
	Total x force coefficient (inviscid contribution) for all the boundaries.
su2double	AllBound_CFy_Inv
	Total y force coefficient (inviscid contribution) for all the boundaries.
su2double	AllBound_CFz_Inv
	Total z force coefficient (inviscid contribution) for all the boundaries.
su2double	AllBound_CEff_Inv
	Efficient coefficient (inviscid contribution) for all the boundaries.
su2double	AllBound_CMerit_Inv
	Rotor Figure of Merit (inviscid contribution) for all the boundaries.
su2double	AllBound_CT_Inv
	Total thrust coefficient (inviscid contribution) for all the boundaries.
su2double	AllBound_CQ_Inv
	Total torque coefficient (inviscid contribution) for all the boundaries.
su2double	AllBound_CEquivArea_Inv
	equivalent area coefficient (inviscid contribution) for all the boundaries.
su2double	AllBound_CNearFieldOF_Inv
	Near-Field press coefficient (inviscid contribution) for all the boundaries.
su2double	AllBound_CD_Mnt
	Total drag coefficient (inviscid contribution) for all the boundaries.
su2double	AllBound_CL_Mnt
	Total lift coefficient (inviscid contribution) for all the boundaries.
su2double	AllBound_CSF_Mnt
	Total sideforce coefficient (inviscid contribution) for all the boundaries.
su2double	AllBound_CMx_Mnt
	Total x moment coefficient (inviscid contribution) for all the boundaries.
su2double	AllBound_CMy_Mnt
	Total y moment coefficient (inviscid contribution) for all the boundaries.
su2double	AllBound_CMz_Mnt
	Total z moment coefficient (inviscid contribution) for all the boundaries.
su2double	AllBound_CFx_Mnt
	Total x force coefficient (inviscid contribution) for all the boundaries.
su2double	AllBound_CFy_Mnt
	Total y force coefficient (inviscid contribution) for all the boundaries.
su2double	AllBound_CFz_Mnt
	Total z force coefficient (inviscid contribution) for all the boundaries.
su2double	AllBound_CEff_Mnt
	Efficient coefficient (inviscid contribution) for all the boundaries.
su2double	AllBound_CMerit_Mnt
	Rotor Figure of Merit (inviscid contribution) for all the boundaries.
su2double	AllBound_CT_Mnt
	Total thrust coefficient (inviscid contribution) for all the boundaries.
su2double	AllBound_CQ_Mnt
	Total torque coefficient (inviscid contribution) for all the boundaries.
su2double	OneD_TotalPress
	average total pressure evaluated at an exit
su2double	OneD_Mach
	area average Mach evaluated at an exit
su2double	OneD_Temp
	area average Temperature evaluated at an exit
su2double	OneD_PressureRef
	area average Pressure evaluated at an exit
su2double	OneD_MassFlowRate
	Mass flow rate at an exit.
su2double	OneD_DensityRef
	flux average density evaluated at an exit
su2double	OneD_EnthalpyRef
	flux average enthalpy evaluated at an exit
su2double	OneD_VelocityRef
	flux average velocity evaluated at an exit
su2double	Total_ComboObj
	Total 'combo' objective for all monitored boundaries.
su2double	AoA_Prev
	Old value of the AoA for fixed lift mode.
su2double	Total_CD
	Total drag coefficient for all the boundaries.
su2double	Total_CL
	Total lift coefficient for all the boundaries.
su2double	Total_CL_Prev
	Total lift coefficient for all the boundaries (fixed lift mode).
su2double	Total_CD_SolidSurf
	Total drag coefficient for all the boundaries.
su2double	Total_CD_Prev
	Total drag coefficient for all the boundaries (fixed lift mode).
su2double	Total_NetCThrust
	Total drag coefficient for all the boundaries.
su2double	Total_Power
	Total drag coefficient for all the boundaries.
su2double	Total_ReverseFlow
	Total drag coefficient for all the boundaries.
su2double	Total_IDC
	Total IDC coefficient for all the boundaries.
su2double	Total_IDC_Mach
	Total IDC coefficient for all the boundaries.
su2double	Total_IDR
	Total IDC coefficient for all the boundaries.
su2double	Total_DC60
	Total IDC coefficient for all the boundaries.
su2double	Total_MFR
	Total Mass Flow Ratio for all the boundaries.
su2double	Total_Prop_Eff
	Total Mass Flow Ratio for all the boundaries.
su2double	Total_ByPassProp_Eff
	Total Mass Flow Ratio for all the boundaries.
su2double	Total_Adiab_Eff
	Total Mass Flow Ratio for all the boundaries.
su2double	Total_Poly_Eff
	Total Mass Flow Ratio for all the boundaries.
su2double	Total_NetCThrust_Prev
	Total lift coefficient for all the boundaries.
su2double	Total_BCThrust_Prev
	Total lift coefficient for all the boundaries.
su2double	Total_Custom
	Total IDC coefficient for all the boundaries.
su2double	Total_CSF
	Total sideforce coefficient for all the boundaries.
su2double	Total_CMx
	Total x moment coefficient for all the boundaries.
su2double	Total_CMy
	Total y moment coefficient for all the boundaries.
su2double	Total_CMz
	Total z moment coefficient for all the boundaries.
su2double	Total_CFx
	Total x force coefficient for all the boundaries.
su2double	Total_CFy
	Total y force coefficient for all the boundaries.
su2double	Total_CFz
	Total z force coefficient for all the boundaries.
su2double	Total_CEff
	Total efficiency coefficient for all the boundaries.
su2double	Total_CMerit
	Total rotor Figure of Merit for all the boundaries.
su2double	Total_CT
	Total thrust coefficient for all the boundaries.
su2double	Total_CQ
	Total torque 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	Total_AeroCD
	Total aero drag coefficient for all the boundaries.
su2double	Total_RadialDistortion
	Total fan face radial distortion for all the boundaries.
su2double	Total_CircumferentialDistortion
	Total fan face circumferential distortion for all the boundaries.
su2double	Total_CEquivArea
	Total Equivalent Area coefficient for all the boundaries.
su2double	Total_CNearFieldOF
	Total Near-Field Pressure coefficient for all the boundaries.
su2double	Total_CpDiff
	Total Equivalent Area coefficient for all the boundaries.
su2double	Total_HeatFluxDiff
	Total Equivalent Area coefficient for all the boundaries.
su2double	Total_MassFlowRate
	Total Mass Flow Rate on monitored boundaries.
su2double *	Surface_CL
	Lift coefficient for each monitoring surface.
su2double *	Surface_CD
	Drag coefficient for each monitoring surface.
su2double *	Surface_CSF
	Side-force coefficient for each monitoring surface.
su2double *	Surface_CEff
	Side-force coefficient for each monitoring surface.
su2double *	Surface_CFx
	x Force coefficient for each monitoring surface.
su2double *	Surface_CFy
	y Force coefficient for each monitoring surface.
su2double *	Surface_CFz
	z Force coefficient for each monitoring surface.
su2double *	Surface_CMx
	x Moment coefficient for each monitoring surface.
su2double *	Surface_CMy
	y Moment coefficient for each monitoring surface.
su2double *	Surface_CMz
	z Moment coefficient for each monitoring surface.
su2double *	Surface_HF_Visc
	Total (integrated) heat flux for each monitored surface.
su2double *	Surface_MaxHF_Visc
	Maximum heat flux for each monitored surface.
su2double *	iPoint_UndLapl
	Auxiliary variable for the undivided Laplacians.
su2double *	jPoint_UndLapl
	Auxiliary variable for the undivided Laplacians.
su2double *	SecondaryVar_i
	Auxiliary vector for storing the solution at point i.
su2double *	SecondaryVar_j
	Auxiliary vector for storing the solution at point j.
su2double *	PrimVar_i
	Auxiliary vector for storing the solution at point i.
su2double *	PrimVar_j
	Auxiliary vector for storing the solution at point j.
su2double **	LowMach_Precontioner
	Auxiliary vector for storing the inverse of Roe-turkel preconditioner.
unsigned long	nMarker
	Total number of markers using the grid information.
unsigned long *	nVertex
	Store nVertex at each marker for deallocation.
bool	space_centered
	True if space centered scheeme 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 .
su2double *	Primitive
	Auxiliary nPrimVar vector.
su2double *	Primitive_i
	Auxiliary nPrimVar vector for storing the primitive at point i.
su2double *	Primitive_j
	Auxiliary nPrimVar vector for storing the primitive at point j.
su2double *	Secondary
	Auxiliary nPrimVar vector.
su2double *	Secondary_i
	Auxiliary nPrimVar vector for storing the primitive at point i.
su2double *	Secondary_j
	Auxiliary nPrimVar vector for storing the primitive at point j.
su2double	Cauchy_Value
	Summed value of the convergence indicator.
su2double	Cauchy_Func
	Current value of the convergence indicator at one iteration.
unsigned short	Cauchy_Counter
	Number of elements of the Cauchy serial.
su2double *	Cauchy_Serie
	Complete Cauchy serial.
su2double	Old_Func
	Old value of the objective function (the function which is monitored).
su2double	New_Func
	Current value of the objective function (the function which is monitored).
su2double	AoA_old
	Old value of the angle of attack (monitored).
unsigned long	AoA_Counter
unsigned long	BCThrust_Counter
CFluidModel *	FluidModel
	fluid model used in the solver
su2double **	AveragedVelocity
su2double **	AveragedNormal
su2double **	AveragedGridVel
su2double **	AveragedFlux
su2double **	TotalFlux
su2double *	TotalArea
su2double *	AveragedNormalVelocity
su2double *	ExtAveragedNormalVelocity
su2double *	AveragedTangVelocity
su2double *	ExtAveragedTangVelocity
su2double *	AveragedTangGridVelocity
su2double *	AveragedMach
su2double *	AveragedNormalMach
su2double *	AveragedTangMach
su2double *	AveragedEnthalpy
su2double *	AveragedPressure
su2double *	AveragedTotTemperature
su2double *	AveragedTotPressure
su2double *	ExtAveragedPressure
su2double *	ExtAveragedTotTemperature
su2double *	ExtAveragedTotPressure
su2double *	AveragedDensity
su2double *	ExtAveragedDensity
su2double *	AveragedSoundSpeed
su2double *	AveragedEntropy
su2double *	MassFlow
su2double *	FlowAngle
su2double *	TotalStaticEfficiency
su2double *	TotalTotalEfficiency
su2double *	KineticEnergyLoss
su2double *	TotalPressureLoss
su2double *	MassFlowIn
su2double *	MassFlowOut
su2double *	FlowAngleIn
su2double *	FlowAngleOut
su2double *	EulerianWork
su2double *	TotalEnthalpyIn
su2double *	PressureRatio
su2double *	PressureOut
su2double *	EnthalpyOut
su2double *	MachIn
su2double *	MachOut
su2double *	NormalMachIn
su2double *	NormalMachOut
su2double *	VelocityOutIs
su2double ***	SlidingState
Protected Attributes inherited from CSolver
unsigned short	IterLinSolver
	Linear solver iterations.
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	nSecondaryVarGrad
	Number of primitive variables of the problem in the gradient computation.
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 *	Residual_RMS
	Vector with the mean residual for each variable.
su2double *	Residual_Max
	Vector with the maximal residual for each variable.
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.
unsigned long *	Point_Max
	Vector with the maximal residual for each variable.
su2double **	Point_Max_Coord
	Vector with pointers to the coords of the maximal residual for each variable.
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.
su2double **	Smatrix
	Auxiliary structure for computing gradients by least-squares.
su2double **	Cvector
	Auxiliary structure for computing gradients by least-squares.
unsigned short	nOutputVariables
	Number of variables to write.

Additional Inherited Members
Public Attributes inherited from CSolver
CSysVector	LinSysSol
	vector to store iterative solution of implicit linear system.
CSysVector	LinSysRes
	vector to store iterative residual of implicit linear system.
CSysVector	LinSysAux
	vector to store iterative residual of implicit linear system.
CSysMatrix	Jacobian
	Complete sparse Jacobian structure for implicit computations.
CSysMatrix	StiffMatrix
	Sparse structure for storing the stiffness matrix in Galerkin computations, and grid movement.
CSysVector	OutputVariables
	vector to store the extra variables to be written.
string *	OutputHeadingNames
CVariable **	node
	Vector which the define the variables for each problem.
CVariable *	node_infty
	CVariable storing the free stream conditions.

Detailed Description

Main class for defining the Euler's flow solver.

Author

F. Palacios

Version

5.0.0 "Raven"

Constructor & Destructor Documentation

CEulerSolver()

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

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

Parameters

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

Member Function Documentation

AddTotal_ComboObj()

void CEulerSolver::AddTotal_ComboObj ( su2double  val_obj )

inlinevirtual

Add to the value of the total 'combo' objective.

Author

H. Kline

Parameters

[in]

val_obj

- Value of the contribution to the 'combo' objective.

Reimplemented from CSolver.

AddTotal_Custom()

void CEulerSolver::AddTotal_Custom ( su2double  val_Total_Custom, su2double  val_coeff  )

inlinevirtual

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

Parameters

[in]

val_Total_CD

- Value of the total drag coefficient.

Reimplemented from CSolver.

BC_ActDisk()

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

virtual

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_Inlet()

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

virtual

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  )

virtual

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_Custom()

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

virtual

Impose the dirichlet boundary condition.

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]	val_marker	- Surface marker where the boundary condition is applied.

Reimplemented from CSolver.

BC_Dirichlet()

void CEulerSolver::BC_Dirichlet ( CGeometry *  geometry, CSolver **  solver_container, CConfig *  config, unsigned short  val_marker  )

virtual

Impose the dirichlet boundary condition using the residual.

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]	val_marker	- Surface marker where the boundary condition is applied.

Reimplemented from CSolver.

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  )

virtual

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  )

virtual

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_Euler_Wall()

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

virtual

Impose via the residual the Euler wall boundary condition.

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]	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  )

virtual

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_Fluid_Interface()

void CEulerSolver::BC_Fluid_Interface ( CGeometry *  geometry, CSolver **  solver_container, CNumerics *  numerics, CConfig *  config  )

virtual

Impose the interface state across sliding meshes.

Parameters

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

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  )

virtual

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_Interface_Boundary()

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

virtual

Impose the interface boundary condition using the residual.

Parameters

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

Reimplemented from CSolver.

BC_NearField_Boundary()

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

virtual

Impose the near-field boundary condition using the residual.

Parameters

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

Reimplemented from CSolver.

BC_NonReflecting()

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

virtual

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_Outlet()

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

virtual

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  )

virtual

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  )

virtual

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  )

virtual

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_Sym_Plane()

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

virtual

Impose the symmetry boundary condition using the residual.

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.

Boundary_Fourier() [1/2]

void CEulerSolver::Boundary_Fourier ( CGeometry *  geometry, CSolver **  solver_container, CConfig *  config, unsigned short  val_Marker, vector< std::complex< su2double > > &  c4k, signed long &  nboundaryvertex  )

virtual

it performs a fourier transformation of a characteristic value.

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]	val_marker	- Surface marker where the boundary condition is applied.
[in]	c4k	- Fourier transformation coefficients.
[in]	nboundaryvertex	- pithcwise ordered vertex.

Reimplemented from CSolver.

Boundary_Fourier() [2/2]

void CEulerSolver::Boundary_Fourier ( CGeometry *  geometry, CSolver **  solver_container, CConfig *  config, unsigned short  val_Marker, vector< std::complex< su2double > > &  c2k, vector< std::complex< su2double > > &  c3k, signed long &  nboundaryvertex  )

virtual

it performs a fourier transformation of a characteristic value.

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]	val_marker	- Surface marker where the boundary condition is applied.
[in]	c2k	- Fourier transformation coefficients.
[in]	c3k	- Fourier transformation coefficients.
[in]	nboundaryvertex	- pithcwise ordered vertex.

Reimplemented from CSolver.

Centered_Residual()

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

virtual

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	- 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.

Compareval()

static bool CEulerSolver::Compareval ( std::vector< su2double >  a, std::vector< su2double >  b  )

static

compare to values.

Parameters

[in]	a	- value 1.
[in]	b	- value 2.

Compute_ComboObj()

void CEulerSolver::Compute_ComboObj ( CConfig *  config )

virtual

Compute weighted-sum "combo" objective output.

Author

H. Kline

Parameters

[in]

config

- Definition of the particular problem.

Reimplemented from CSolver.

ComputeConsExtrapolation()

void CEulerSolver::ComputeConsExtrapolation

(

CConfig *

config

)

Compute the extrapolated quantities, for MUSCL upwind 2nd reconstruction, in a more thermodynamic consistent way.

Parameters

[in]

config

- Definition of the particular problem.

ExplicitEuler_Iteration()

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

virtual

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  )

virtual

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.

GetActDisk_DeltaP()

su2double CEulerSolver::GetActDisk_DeltaP ( unsigned short  val_marker, unsigned long  val_vertex  )

inlinevirtual

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.

GetActDisk_DeltaT()

su2double CEulerSolver::GetActDisk_DeltaT ( unsigned short  val_marker, unsigned long  val_vertex  )

inlinevirtual

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.

GetAllBound_CD_Inv()

su2double CEulerSolver::GetAllBound_CD_Inv ( void  )

inlinevirtual

Get the inviscid contribution to the drag coefficient.

Returns

Value of the drag coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CD_Mnt()

su2double CEulerSolver::GetAllBound_CD_Mnt ( void  )

inlinevirtual

Get the inviscid contribution to the drag coefficient.

Returns

Value of the drag coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CEff_Inv()

su2double CEulerSolver::GetAllBound_CEff_Inv ( void  )

inlinevirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CEff_Mnt()

su2double CEulerSolver::GetAllBound_CEff_Mnt ( void  )

inlinevirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CFx_Inv()

su2double CEulerSolver::GetAllBound_CFx_Inv ( void  )

inlinevirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CFx_Mnt()

su2double CEulerSolver::GetAllBound_CFx_Mnt ( void  )

inlinevirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CFy_Inv()

su2double CEulerSolver::GetAllBound_CFy_Inv ( void  )

inlinevirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CFy_Mnt()

su2double CEulerSolver::GetAllBound_CFy_Mnt ( void  )

inlinevirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CFz_Inv()

su2double CEulerSolver::GetAllBound_CFz_Inv ( void  )

inlinevirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CFz_Mnt()

su2double CEulerSolver::GetAllBound_CFz_Mnt ( void  )

inlinevirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CL_Inv()

su2double CEulerSolver::GetAllBound_CL_Inv ( void  )

inlinevirtual

Get the inviscid contribution to the lift coefficient.

Returns

Value of the lift coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CL_Mnt()

su2double CEulerSolver::GetAllBound_CL_Mnt ( void  )

inlinevirtual

Get the inviscid contribution to the lift coefficient.

Returns

Value of the lift coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CMx_Inv()

su2double CEulerSolver::GetAllBound_CMx_Inv ( void  )

inlinevirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CMx_Mnt()

su2double CEulerSolver::GetAllBound_CMx_Mnt ( void  )

inlinevirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CMy_Inv()

su2double CEulerSolver::GetAllBound_CMy_Inv ( void  )

inlinevirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CMy_Mnt()

su2double CEulerSolver::GetAllBound_CMy_Mnt ( void  )

inlinevirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CMz_Inv()

su2double CEulerSolver::GetAllBound_CMz_Inv ( void  )

inlinevirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CMz_Mnt()

su2double CEulerSolver::GetAllBound_CMz_Mnt ( void  )

inlinevirtual

Get the inviscid contribution to the efficiency coefficient.

Returns

Value of the efficiency coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CSF_Inv()

su2double CEulerSolver::GetAllBound_CSF_Inv ( void  )

inlinevirtual

Get the inviscid contribution to the sideforce coefficient.

Returns

Value of the sideforce coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAllBound_CSF_Mnt()

su2double CEulerSolver::GetAllBound_CSF_Mnt ( void  )

inlinevirtual

Get the inviscid contribution to the sideforce coefficient.

Returns

Value of the sideforce coefficient (inviscid contribution).

Reimplemented from CSolver.

GetAveragedDensity()

su2double CEulerSolver::GetAveragedDensity ( unsigned short  valMarker )

inlinevirtual

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.

GetAveragedEnthalpy()

su2double CEulerSolver::GetAveragedEnthalpy ( unsigned short  valMarker )

inlinevirtual

Provide the average enthalpy at the boundary of interest.

Parameters

[in]

val_marker

- bound marker.

Returns

Value of the Average Enthalpy on the surface val_marker.

Reimplemented from CSolver.

GetAveragedEntropy()

su2double CEulerSolver::GetAveragedEntropy ( unsigned short  valMarker )

inlinevirtual

Provide the average pressure at the boundary of interest.

Parameters

[in]

val_marker

- bound marker.

Returns

Value of the Average Entropy on the surface val_marker.

Reimplemented from CSolver.

GetAveragedGridVelocity()

su2double * CEulerSolver::GetAveragedGridVelocity ( unsigned short  valMarker )

inlinevirtual

Provide the average grid velocity at the boundary of interest.

Parameters

[in]

val_marker

- bound marker.

Returns

Value of the Average Grid Velocity on the surface val_marker.

Reimplemented from CSolver.

GetAveragedMach()

su2double CEulerSolver::GetAveragedMach ( unsigned short  valMarker )

inlinevirtual

Provide the Mach number at the boundary of interest.

Parameters

[in]

val_marker

- bound marker.

Returns

Value of the Mach number on the surface val_marker.

Reimplemented from CSolver.

GetAveragedNormalMach()

su2double CEulerSolver::GetAveragedNormalMach ( unsigned short  valMarker )

inlinevirtual

Provide the Normal Mach number at the boundary of interest.

Parameters

[in]

val_marker

- bound marker.

Returns

Value of the Normal Mach number on the surface val_marker.

Reimplemented from CSolver.

GetAveragedNormalVelocity()

su2double CEulerSolver::GetAveragedNormalVelocity ( unsigned short  valMarker )

inlinevirtual

Provide the Average Normal Velocity at the boundary of interest.

Parameters

[in]

val_marker

- bound marker.

Returns

Value of the Average Normal Velocity on the surface val_marker.

Reimplemented from CSolver.

GetAveragedPressure()

su2double CEulerSolver::GetAveragedPressure ( unsigned short  valMarker )

inlinevirtual

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.

GetAveragedTangVelocity()

su2double CEulerSolver::GetAveragedTangVelocity ( unsigned short  valMarker )

inlinevirtual

Provide the Tangent Velocity at the boundary of interest.

Parameters

[in]

val_marker

- bound marker.

Returns

Value of the Average Tangent Velocity on the surface val_marker.

Reimplemented from CSolver.

GetAveragedTotPressure()

su2double CEulerSolver::GetAveragedTotPressure ( unsigned short  valMarker )

inlinevirtual

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.

GetAveragedTotTemperature()

su2double CEulerSolver::GetAveragedTotTemperature ( unsigned short  valMarker )

inlinevirtual

Provide Averaged Total Temperature 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.

GetAveragedVelocity()

su2double * CEulerSolver::GetAveragedVelocity ( unsigned short  valMarker )

inlinevirtual

Provide the average pressure at the boundary of interest.

Parameters

[in]

val_marker

- bound marker.

Returns

Components of the Average Velocity on the surface val_marker.

Reimplemented from CSolver.

GetCD_Inv()

su2double CEulerSolver::GetCD_Inv ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional drag coefficient (inviscid contribution).

Parameters

val_marker

Surface where the coeficient is going to be computed.

Returns

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

Reimplemented from CSolver.

GetCEff_Inv()

su2double CEulerSolver::GetCEff_Inv ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional efficiency coefficient (inviscid contribution).

Parameters

val_marker

Surface where the coeficient is going to be computed.

Returns

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

Reimplemented from CSolver.

GetCharacPrimVar()

su2double * CEulerSolver::GetCharacPrimVar ( unsigned short  val_marker, unsigned long  val_vertex  )

inlinevirtual

Value of the characteristic variables at the boundaries.

Parameters

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

Returns

Value of the pressure coefficient.

Reimplemented from CSolver.

GetCL_Inv()

su2double CEulerSolver::GetCL_Inv ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional lift coefficient (inviscid contribution).

Parameters

val_marker

Surface where the coefficient is going to be computed.

Returns

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

Reimplemented from CSolver.

GetCMz_Inv()

su2double CEulerSolver::GetCMz_Inv ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional z moment coefficient (inviscid contribution).

Parameters

val_marker

Surface where the coefficient is going to be computed.

Returns

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

Reimplemented from CSolver.

GetCPressure()

su2double CEulerSolver::GetCPressure ( unsigned short  val_marker, unsigned long  val_vertex  )

inlinevirtual

Provide the Pressure coefficient.

Parameters

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

Returns

Value of the pressure coefficient.

Reimplemented from CSolver.

GetCPressureTarget()

su2double CEulerSolver::GetCPressureTarget ( unsigned short  val_marker, unsigned long  val_vertex  )

inlinevirtual

Provide the Target Pressure coefficient.

Parameters

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

Returns

Value of the pressure coefficient.

Reimplemented from CSolver.

GetCSF_Inv()

su2double CEulerSolver::GetCSF_Inv ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional sideforce coefficient (inviscid contribution).

Parameters

val_marker

Surface where the coeficient is going to be computed.

Returns

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

Reimplemented from CSolver.

GetDensity_Energy_Inf()

su2double CEulerSolver::GetDensity_Energy_Inf ( void  )

inlinevirtual

Compute the density multiply by energy at the infinity.

Returns

Value of the density multiply by energy at the infinity.

Reimplemented from CSolver.

GetDensity_Inf()

su2double CEulerSolver::GetDensity_Inf ( void  )

inlinevirtual

Compute the density at the infinity.

Returns

Value of the density at the infinity.

Reimplemented from CSolver.

GetDensity_Velocity_Inf()

su2double CEulerSolver::GetDensity_Velocity_Inf ( unsigned short  val_dim )

inlinevirtual

Compute the density multiply by velocity at the infinity.

Parameters

[in]

val_dim

- Index of the velocity vector.

Returns

Value of the density multiply by the velocity at the infinity.

Reimplemented from CSolver.

GetDonorGlobalIndex()

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

inlinevirtual

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.

GetDonorPrimVar() [1/2]

su2double * CEulerSolver::GetDonorPrimVar ( unsigned short  val_marker, unsigned long  val_vertex  )

inlinevirtual

Value of the characteristic variables at the boundaries.

Parameters

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

Returns

Value of the pressure coefficient.

Reimplemented from CSolver.

GetDonorPrimVar() [2/2]

su2double CEulerSolver::GetDonorPrimVar ( unsigned short  val_marker, unsigned long  val_vertex, unsigned short  val_var  )

inlinevirtual

Value of the characteristic variables at the boundaries.

Parameters

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

Returns

Value of the pressure coefficient.

Reimplemented from CSolver.

GetEnthalpyOut()

su2double CEulerSolver::GetEnthalpyOut ( unsigned short  inMarkerTP )

inlinevirtual

Provide the Outlet Enthalpy (turbomachinery performance).

Parameters

[in]

inMarkerTP

- turboperformance marker.

Returns

Value of the Outlet Enthalpy.

Reimplemented from CSolver.

GetEulerianWork()

su2double CEulerSolver::GetEulerianWork ( unsigned short  inMarkerTP )

inlinevirtual

Provide the Eulerian Work (turbomachinery performance).

Parameters

[in]

inMarkerTP

- turboperformance marker.

Returns

Value of the Eulerian Work.

Reimplemented from CSolver.

GetExhaust_MassFlow()

su2double CEulerSolver::GetExhaust_MassFlow ( unsigned short  val_marker )

inlinevirtual

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.

GetFlowAngle()

su2double CEulerSolver::GetFlowAngle ( unsigned short  valMarker )

inlinevirtual

Provide the Flow Angle at the boundary of interest.

Parameters

[in]

val_marker

- bound marker.

Returns

Value of the Flow Angle on the surface val_marker.

Reimplemented from CSolver.

GetFlowAngleIn()

su2double CEulerSolver::GetFlowAngleIn ( unsigned short  inMarkerTP )

inlinevirtual

Provide the Inlet Flow Angle (turbomachinery performance).

Parameters

[in]

inMarkerTP

- turboperformance marker.

Returns

Value of the Inlet Flow Angle.

Reimplemented from CSolver.

GetFlowAngleOut()

su2double CEulerSolver::GetFlowAngleOut ( unsigned short  inMarkerTP )

inlinevirtual

Provide the Outlet Flow Angle (turbomachinery performance).

Parameters

[in]

inMarkerTP

- turboperformance marker.

Returns

Value of the Outlet FLow Angle.

Reimplemented from CSolver.

GetFluidModel()

CFluidModel * CEulerSolver::GetFluidModel ( void  )

inlinevirtual

Compute the pressure at the infinity.

Returns

Value of the pressure at the infinity.

Reimplemented from CSolver.

GetInflow_Mach()

su2double CEulerSolver::GetInflow_Mach ( unsigned short  val_marker )

inlinevirtual

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 )

inlinevirtual

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 )

inlinevirtual

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.

GetInlet_FlowDir()

su2double CEulerSolver::GetInlet_FlowDir ( unsigned short  val_marker, unsigned long  val_vertex, unsigned short  val_dim  )

inlinevirtual

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.

GetInlet_Ptotal()

su2double CEulerSolver::GetInlet_Ptotal ( unsigned short  val_marker, unsigned long  val_vertex  )

inlinevirtual

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.

GetInlet_Ttotal()

su2double CEulerSolver::GetInlet_Ttotal ( unsigned short  val_marker, unsigned long  val_vertex  )

inlinevirtual

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.

GetKineticEnergyLoss()

su2double CEulerSolver::GetKineticEnergyLoss ( unsigned short  inMarkerTP )

inlinevirtual

Provide Kinetic Energy Losses (turbomachinery performance).

Parameters

[in]

inMarkerTP

- turboperformance marker.

Returns

Value of the Kinetic Energy Losses.

Reimplemented from CSolver.

GetMachIn()

su2double CEulerSolver::GetMachIn ( unsigned short  inMarkerTP )

inlinevirtual

Provide the Inlet Mach number (turbomachinery performance).

Parameters

[in]

inMarkerTP

- turboperformance marker.

Returns

Value of the Inlet Mach number.

Reimplemented from CSolver.

GetMachOut()

su2double CEulerSolver::GetMachOut ( unsigned short  inMarkerTP )

inlinevirtual

Provide the Outlet Mach number (turbomachinery performance).

Parameters

[in]

inMarkerTP

- turboperformance marker.

Returns

Value of the Outlet Mach number.

Reimplemented from CSolver.

GetMassFlow()

su2double CEulerSolver::GetMassFlow ( unsigned short  valMarker )

inlinevirtual

Provide the MassFlow at the boundary of interest.

Parameters

[in]

val_marker

- bound marker.

Returns

Value of the MassFLow on the surface val_marker.

Reimplemented from CSolver.

GetMassFlowIn()

su2double CEulerSolver::GetMassFlowIn ( unsigned short  inMarkerTP )

inlinevirtual

Provide the Inlet Mass Flow (turbomachinery performance).

Parameters

[in]

inMarkerTP

- turboperformance marker.

Returns

Value of the Inlet Mass Flow.

Reimplemented from CSolver.

GetMassFlowOut()

su2double CEulerSolver::GetMassFlowOut ( unsigned short  inMarkerTP )

inlinevirtual

Provide the Outlet Mass Flow (turbomachinery performance).

Parameters

[in]

inMarkerTP

- turboperformance marker.

Returns

Value of the Outlet Mass Flow.

Reimplemented from CSolver.

GetModVelocity_Inf()

su2double CEulerSolver::GetModVelocity_Inf ( void  )

inlinevirtual

Compute 2-norm of the velocity at the infinity.

Returns

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

Reimplemented from CSolver.

GetNormalMachIn()

su2double CEulerSolver::GetNormalMachIn ( unsigned short  inMarkerTP )

inlinevirtual

Provide the normal component of the Inlet Mach number (turbomachinery performance).

Parameters

[in]

inMarkerTP

- turboperformance marker.

Returns

Value of the normal component of the Inlet Mach number.

Reimplemented from CSolver.

GetNormalMachOut()

su2double CEulerSolver::GetNormalMachOut ( unsigned short  inMarkerTP )

inlinevirtual

Provide the normal component of the Outlet Mach number (turbomachinery performance).

Parameters

[in]

inMarkerTP

- turboperformance marker.

Returns

Value of the normal component of the Outlet Mach number.

Reimplemented from CSolver.

GetPower_Properties()

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

virtual

Compute the Fan face Mach number.

Parameters

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

Reimplemented from CSolver.

GetPressure_Inf()

su2double CEulerSolver::GetPressure_Inf ( void  )

inlinevirtual

Compute the pressure at the infinity.

Returns

Value of the pressure at the infinity.

Reimplemented from CSolver.

GetPressureOut()

su2double CEulerSolver::GetPressureOut ( unsigned short  inMarkerTP )

inlinevirtual

Provide the Outlet Pressure (turbomachinery performance).

Parameters

[in]

inMarkerTP

- turboperformance marker.

Returns

Value of the Outlet Pressure.

Reimplemented from CSolver.

GetPressureRatio()

su2double CEulerSolver::GetPressureRatio ( unsigned short  inMarkerTP )

inlinevirtual

Provide Pressure Ratio (tubomachinery performance).

Parameters

[in]

inMarkerTP

- turboperformance marker.

Returns

Value of the Pressure Ratio.

Reimplemented from CSolver.

GetSlidingState()

su2double CEulerSolver::GetSlidingState ( unsigned short  val_marker, unsigned long  val_vertex, unsigned short  val_state  )

inlinevirtual

Get the outer state for fluid interface nodes.

Parameters

[in]	val_marker	- marker index
[in]	val_vertex	- vertex index
[in]	val_state	- requested state component

Reimplemented from CSolver.

GetSurface_CD()

su2double CEulerSolver::GetSurface_CD ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional drag coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the drag coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CD_Inv()

su2double CEulerSolver::GetSurface_CD_Inv ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional drag coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the drag coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CD_Mnt()

su2double CEulerSolver::GetSurface_CD_Mnt ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional drag coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the drag coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CEff()

su2double CEulerSolver::GetSurface_CEff ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional side-force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

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

Reimplemented from CSolver.

GetSurface_CEff_Inv()

su2double CEulerSolver::GetSurface_CEff_Inv ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional side-force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

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

Reimplemented from CSolver.

GetSurface_CEff_Mnt()

su2double CEulerSolver::GetSurface_CEff_Mnt ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional side-force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

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

Reimplemented from CSolver.

GetSurface_CFx()

su2double CEulerSolver::GetSurface_CFx ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional x force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the x force coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CFx_Inv()

su2double CEulerSolver::GetSurface_CFx_Inv ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional x force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the x force coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CFx_Mnt()

su2double CEulerSolver::GetSurface_CFx_Mnt ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional x force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the x force coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CFy()

su2double CEulerSolver::GetSurface_CFy ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional y force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the y force coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CFy_Inv()

su2double CEulerSolver::GetSurface_CFy_Inv ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional y force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the y force coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CFy_Mnt()

su2double CEulerSolver::GetSurface_CFy_Mnt ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional y force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the y force coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CFz()

su2double CEulerSolver::GetSurface_CFz ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional z force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the z force coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CFz_Inv()

su2double CEulerSolver::GetSurface_CFz_Inv ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional z force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the z force coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CFz_Mnt()

su2double CEulerSolver::GetSurface_CFz_Mnt ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional z force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the z force coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CL()

su2double CEulerSolver::GetSurface_CL ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional lift coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the lift coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CL_Inv()

su2double CEulerSolver::GetSurface_CL_Inv ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional lift coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the lift coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CL_Mnt()

su2double CEulerSolver::GetSurface_CL_Mnt ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional lift coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the lift coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CMx()

su2double CEulerSolver::GetSurface_CMx ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional x moment coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the x moment coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CMx_Inv()

su2double CEulerSolver::GetSurface_CMx_Inv ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional x moment coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the x moment coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CMx_Mnt()

su2double CEulerSolver::GetSurface_CMx_Mnt ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional x moment coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the x moment coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CMy()

su2double CEulerSolver::GetSurface_CMy ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional y moment coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the y moment coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CMy_Inv()

su2double CEulerSolver::GetSurface_CMy_Inv ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional y moment coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the y moment coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CMy_Mnt()

su2double CEulerSolver::GetSurface_CMy_Mnt ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional y moment coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the y moment coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CMz()

su2double CEulerSolver::GetSurface_CMz ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional z moment coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the z moment coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CMz_Inv()

su2double CEulerSolver::GetSurface_CMz_Inv ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional z moment coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the z moment coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CMz_Mnt()

su2double CEulerSolver::GetSurface_CMz_Mnt ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional z moment coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

Value of the z moment coefficient on the surface val_marker.

Reimplemented from CSolver.

GetSurface_CSF()

su2double CEulerSolver::GetSurface_CSF ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional side-force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

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

Reimplemented from CSolver.

GetSurface_CSF_Inv()

su2double CEulerSolver::GetSurface_CSF_Inv ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional side-force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

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

Reimplemented from CSolver.

GetSurface_CSF_Mnt()

su2double CEulerSolver::GetSurface_CSF_Mnt ( unsigned short  val_marker )

inlinevirtual

Provide the non dimensional side-force coefficient.

Parameters

[in]

val_marker

- Surface marker where the coefficient is computed.

Returns

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

Reimplemented from CSolver.

GetSurface_Distortion()

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

virtual

Compute the Fan face Mach number.

Parameters

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

Reimplemented from CSolver.

GetSurface_Properties()

void CEulerSolver::GetSurface_Properties ( CGeometry *  geometry, CNumerics *  conv_numerics, CNumerics *  visc_numerics, CConfig *  config, unsigned short  iMesh, bool  Output  )

virtual

Compute the Fan face Mach number.

Parameters

[in]	geometry	- Geometrical definition of the problem.
[in]	solution	- Container vector with all the solutions.
[in]	Output	- boolean to determine whether to print output.

Reimplemented from CSolver.

GetTotal_Adiab_Eff()

su2double CEulerSolver::GetTotal_Adiab_Eff ( void  )

inlinevirtual

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 ( void  )

inlinevirtual

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 ( void  )

inlinevirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_CD()

su2double CEulerSolver::GetTotal_CD ( void  )

inlinevirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_CD_SolidSurf()

su2double CEulerSolver::GetTotal_CD_SolidSurf ( void  )

inlinevirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_CEff()

su2double CEulerSolver::GetTotal_CEff ( void  )

inlinevirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_CEquivArea()

su2double CEulerSolver::GetTotal_CEquivArea ( void  )

inlinevirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_CFx()

su2double CEulerSolver::GetTotal_CFx ( void  )

inlinevirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_CFy()

su2double CEulerSolver::GetTotal_CFy ( void  )

inlinevirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_CFz()

su2double CEulerSolver::GetTotal_CFz ( void  )

inlinevirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_CircumferentialDistortion()

su2double CEulerSolver::GetTotal_CircumferentialDistortion ( void  )

inlinevirtual

Provide the total (inviscid + viscous) non dimensional fan face distortion.

Returns

Value of the fan face distortion (inviscid + viscous contribution).

Reimplemented from CSolver.

GetTotal_CL()

su2double CEulerSolver::GetTotal_CL ( void  )

inlinevirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_CMerit()

su2double CEulerSolver::GetTotal_CMerit ( void  )

inlinevirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_CMx()

su2double CEulerSolver::GetTotal_CMx ( void  )

inlinevirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_CMy()

su2double CEulerSolver::GetTotal_CMy ( void  )

inlinevirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_CMz()

su2double CEulerSolver::GetTotal_CMz ( void  )

inlinevirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_CNearFieldOF()

su2double CEulerSolver::GetTotal_CNearFieldOF ( void  )

inlinevirtual

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_ComboObj()

su2double CEulerSolver::GetTotal_ComboObj ( void  )

inlinevirtual

Provide the total "combo" objective (weighted sum of other values).

Author

H. Kline

Returns

Value of the "combo" objective values.

Reimplemented from CSolver.

GetTotal_CpDiff()

su2double CEulerSolver::GetTotal_CpDiff ( void  )

inlinevirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_CQ()

su2double CEulerSolver::GetTotal_CQ ( void  )

inlinevirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_CSF()

su2double CEulerSolver::GetTotal_CSF ( void  )

inlinevirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_CT()

su2double CEulerSolver::GetTotal_CT ( void  )

inlinevirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_Custom()

su2double CEulerSolver::GetTotal_Custom ( void  )

inlinevirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_DC60()

su2double CEulerSolver::GetTotal_DC60 ( void  )

inlinevirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_HeatFlux()

su2double CEulerSolver::GetTotal_HeatFlux ( void  )

inlinevirtual

Provide the total heat load.

Returns

Value of the heat load (viscous contribution).

Reimplemented from CSolver.

GetTotal_HeatFluxDiff()

su2double CEulerSolver::GetTotal_HeatFluxDiff ( void  )

inlinevirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_IDC()

su2double CEulerSolver::GetTotal_IDC ( void  )

inlinevirtual

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 ( void  )

inlinevirtual

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 ( void  )

inlinevirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_MaxHeatFlux()

su2double CEulerSolver::GetTotal_MaxHeatFlux ( void  )

inlinevirtual

Provide the total heat load.

Returns

Value of the heat load (viscous contribution).

Reimplemented from CSolver.

GetTotal_MFR()

su2double CEulerSolver::GetTotal_MFR ( void  )

inlinevirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_NetCThrust()

su2double CEulerSolver::GetTotal_NetCThrust ( void  )

inlinevirtual

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 ( void  )

inlinevirtual

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 ( void  )

inlinevirtual

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 ( void  )

inlinevirtual

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

Returns

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

Reimplemented from CSolver.

GetTotal_RadialDistortion()

su2double CEulerSolver::GetTotal_RadialDistortion ( void  )

inlinevirtual

Provide the total (inviscid + viscous) non dimensional fan face distortion.

Returns

Value of the fan face distortion (inviscid + viscous contribution).

Reimplemented from CSolver.

GetTotal_ReverseFlow()

su2double CEulerSolver::GetTotal_ReverseFlow ( void  )

inlinevirtual

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

Returns

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

Reimplemented from CSolver.

GetTotalEnthalpyIn()

su2double CEulerSolver::GetTotalEnthalpyIn ( unsigned short  inMarkerTP )

inlinevirtual

Provide the Inlet Total Enthalpy (turbomachinery performance).

Parameters

[in]

inMarkerTP

- turboperformance marker.

Returns

Value of the Inlet Total Enthalpy.

Reimplemented from CSolver.

GetTotalPressureLoss()

su2double CEulerSolver::GetTotalPressureLoss ( unsigned short  inMarkerTP )

inlinevirtual

Provide Total Pressure Losses (turbomachinery performance).

Parameters

[in]

inMarkerTP

- turboperformance marker.

Returns

Value of Total Pressure Losses.

Reimplemented from CSolver.

GetTotalStaticEfficiency()

su2double CEulerSolver::GetTotalStaticEfficiency ( unsigned short  inMarkerTP )

inlinevirtual

Provide Total-Static Efficiency (turbomachinery performance).

Parameters

[in]

inMarkerTP

- turboperformance marker.

Returns

Value of the Total-Static Efficiency.

Reimplemented from CSolver.

GetTotalTotalEfficiency()

su2double CEulerSolver::GetTotalTotalEfficiency ( unsigned short  inMarkerTP )

inlinevirtual

Provide Total-Total Efficiency (turbomachinery performance).

Parameters

[in]

inMarkerTP

- turboperformance marker.

Returns

Value of the Total-Total Efficiency.

Reimplemented from CSolver.

GetVelocity_Inf() [1/2]

su2double CEulerSolver::GetVelocity_Inf ( unsigned short  val_dim )

inlinevirtual

Get the velocity at the infinity.

Parameters

[in]

val_dim

- Index of the velocity vector.

Returns

Value of the velocity at the infinity.

Reimplemented from CSolver.

GetVelocity_Inf() [2/2]

su2double * CEulerSolver::GetVelocity_Inf ( void  )

inlinevirtual

Get the velocity at the infinity.

Returns

Value of the velocity at the infinity.

Reimplemented from CSolver.

GetVelocityOutIs()

su2double CEulerSolver::GetVelocityOutIs ( unsigned short  inMarkerTP )

inlinevirtual

Provide the Isentropic Outlet Velocity (turbomachinery performance).

Parameters

[in]

inMarkerTP

- turboperformance marker.

Returns

Value of the Isentropic Outlet Velocity.

Reimplemented from CSolver.

ImplicitEuler_Iteration()

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

virtual

Update the solution using an implicit 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.

LoadRestart()

void CEulerSolver::LoadRestart ( CGeometry **  geometry, CSolver ***  solver, CConfig *  config, int  val_iter  )

virtual

Load a solution from a restart file.

Parameters

[in]	geometry	- Geometrical definition of the problem.
[in]	solver	- Container vector with all of the solvers.
[in]	config	- Definition of the particular problem.
[in]	val_iter	- Current external iteration number.

Reimplemented from CSolver.

MixedOut_Average()

void CEulerSolver::MixedOut_Average ( su2double  val_init_pressure, su2double *  val_Averaged_Flux, su2double *  val_normal, su2double *  pressure_mix, su2double *  density_mix  )

virtual

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.

Reimplemented from CSolver.

MixedOut_Root_Function()

void CEulerSolver::MixedOut_Root_Function ( su2double *  pressure, su2double *  val_Averaged_Flux, su2double *  val_normal, su2double *  valfunc, su2double *  density  )

virtual

it finds the root of an implicit equation that relates pressure and density.

Parameters

[in]	pressure	- pressure value
[in]	val_Averaged_Flux	- flux averaged values.
[in]	val_normal	- normal vector.
[in]	valfunc	- Description of the numerical method.
[in]	density	- value of the mixed-out avaraged density.

Reimplemented from CSolver.

Mixing_Process()

void CEulerSolver::Mixing_Process ( CGeometry *  geometry, CSolver **  solver_container, CConfig *  config, unsigned short  val_Marker  )

virtual

It avarage the fluxes value along a boundary.

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]	val_marker	- Surface marker where the boundary condition is applied.

Reimplemented from CSolver.

Momentum_Forces()

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

virtual

Compute the pressure forces and all the adimensional coefficients.

Parameters

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

Reimplemented from CSolver.

Postprocessing()

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

virtual

A virtual member.

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.

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  )

virtual

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.

Pressure_Forces()

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

virtual

Compute the pressure forces and all the adimensional coefficients.

Parameters

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

Reimplemented from CSolver.

Set_MPI_ActDisk()

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

virtual

Parallelization of Undivided Laplacian.

Parameters

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

Reimplemented from CSolver.

Set_MPI_Dissipation_Switch()

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

virtual

Parallelization of SetDissipation_Switch.

Parameters

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

Reimplemented from CSolver.

Set_MPI_Interface()

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

virtual

Parallelization of Undivided Laplacian.

Parameters

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

Reimplemented from CSolver.

Set_MPI_MaxEigenvalue()

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

virtual

Parallelization of the Max eigenvalue.

Parameters

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

Reimplemented from CSolver.

Set_MPI_Nearfield()

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

virtual

Parallelization of Undivided Laplacian.

Parameters

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

Reimplemented from CSolver.

Set_MPI_Primitive_Gradient()

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

virtual

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

Parameters

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

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

Parameters

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

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

Parameters

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

Reimplemented from CSolver.

Set_MPI_Primitive_Limiter()

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

virtual

Impose the send-receive boundary condition.

Parameters

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

Reimplemented from CSolver.

Set_MPI_Solution()

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

virtual

Impose the send-receive boundary condition.

Parameters

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

Reimplemented from CSolver.

Set_MPI_Solution_Gradient()

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

virtual

Impose the send-receive boundary condition.

Parameters

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

Reimplemented from CSolver.

Set_MPI_Solution_Limiter()

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

virtual

Impose the send-receive boundary condition.

Parameters

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

Reimplemented from CSolver.

Set_MPI_Solution_Old()

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

virtual

Impose the send-receive boundary condition.

Parameters

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

Reimplemented from CSolver.

Set_MPI_Undivided_Laplacian()

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

virtual

Parallelization of Undivided Laplacian.

Parameters

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

Reimplemented from CSolver.

SetActDisk_BCThrust()

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

virtual

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.

Reimplemented from CSolver.

SetActDisk_DeltaP()

void CEulerSolver::SetActDisk_DeltaP ( unsigned short  val_marker, unsigned long  val_vertex, su2double  val_deltap  )

inlinevirtual

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.

SetActDisk_DeltaT()

void CEulerSolver::SetActDisk_DeltaT ( unsigned short  val_marker, unsigned long  val_vertex, su2double  val_deltat  )

inlinevirtual

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.

SetCharacPrimVar()

void CEulerSolver::SetCharacPrimVar ( unsigned short  val_marker, unsigned long  val_vertex, unsigned short  val_var, su2double  val_value  )

inlinevirtual

Value of the characteristic variables at the boundaries.

Parameters

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

Returns

Value of the pressure coefficient.

Reimplemented from CSolver.

SetCPressureTarget()

void CEulerSolver::SetCPressureTarget ( unsigned short  val_marker, unsigned long  val_vertex, su2double  val_pressure  )

inlinevirtual

Set the value of the target Pressure coefficient.

Parameters

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

Returns

Value of the pressure coefficient.

Reimplemented from CSolver.

SetDissipation_Switch()

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

virtual

Compute a pressure sensor switch.

Parameters

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

Reimplemented from CSolver.

SetDonorGlobalIndex()

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

inlinevirtual

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.

SetDonorPrimVar()

void CEulerSolver::SetDonorPrimVar ( unsigned short  val_marker, unsigned long  val_vertex, unsigned short  val_var, su2double  val_value  )

inlinevirtual

Value of the characteristic variables at the boundaries.

Parameters

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

Returns

Value of the pressure coefficient.

Reimplemented from CSolver.

SetExtAveragedValue()

void CEulerSolver::SetExtAveragedValue ( CSolver *  solver_container, unsigned short  intMarker, unsigned short  extMarker  )

inlinevirtual

A virtual member.

Parameters

[in]	solver_container	- Container vector with all the solutions.
[in]	intMarker	- internal marker.
[in]	extMarker	- external marker.

Reimplemented from CSolver.

SetFarfield_AoA()

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

virtual

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.

Reimplemented from CSolver.

SetFlow_Displacement()

void CEulerSolver::SetFlow_Displacement ( CGeometry **  flow_geometry, CVolumetricMovement *  flow_grid_movement, CConfig *  flow_config, CConfig *  fea_config, CGeometry **  fea_geometry, CSolver ***  fea_solution  )

virtual

A virtual member.

Parameters

[in]	flow_geometry	- Geometrical definition of the problem.
[in]	flow_grid_movement	- Geometrical definition of the problem.
[in]	flow_config	- Geometrical definition of the problem.
[in]	fea_geometry	- Definition of the particular problem.

Reimplemented from CSolver.

SetFlow_Displacement_Int()

void CEulerSolver::SetFlow_Displacement_Int ( CGeometry **  flow_geometry, CVolumetricMovement *  flow_grid_movement, CConfig *  flow_config, CConfig *  fea_config, CGeometry **  fea_geometry, CSolver ***  fea_solution  )

virtual

A virtual member.

Parameters

[in]	flow_geometry	- Geometrical definition of the problem.
[in]	flow_grid_movement	- Geometrical definition of the problem.
[in]	flow_config	- Geometrical definition of the problem.
[in]	fea_geometry	- Definition of the particular problem.

Reimplemented from CSolver.

SetFreeStream_Solution()

void CEulerSolver::SetFreeStream_Solution ( CConfig *  config )

virtual

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  ExtIter  )

virtual

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.

SetInlet_FlowDir()

void CEulerSolver::SetInlet_FlowDir ( unsigned short  val_marker, unsigned long  val_vertex, unsigned short  val_dim, su2double  val_flowdir  )

inlinevirtual

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.

SetInlet_Ptotal()

void CEulerSolver::SetInlet_Ptotal ( unsigned short  val_marker, unsigned long  val_vertex, su2double  val_ptotal  )

inlinevirtual

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.

SetInlet_Ttotal()

void CEulerSolver::SetInlet_Ttotal ( unsigned short  val_marker, unsigned long  val_vertex, su2double  val_ttotal  )

inlinevirtual

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.

SetMax_Eigenvalue()

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

virtual

Compute the max eigenvalue.

Parameters

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

Reimplemented from CSolver.

SetNondimensionalization()

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

virtual

Impose the send-receive boundary condition.

Parameters

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

Set the fluid solver nondimensionalization.

Parameters

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

Reimplemented from CSolver.

SetOneD_TotalPress()

void CEulerSolver::SetOneD_TotalPress ( su2double  AveragePressure )

inlinevirtual

Set the value of averaged total pressure.

Parameters

[in]

val_exit_pt

- value of the averaged pressure

Reimplemented from CSolver.

SetPreconditioner()

void CEulerSolver::SetPreconditioner ( CConfig *  config, unsigned long  iPoint  )

virtual

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

Parameters

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

Compute the limiter of the primitive variables.

Parameters

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

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

Parameters

[in]	iPoint	- Index of the grid point
[in]	config	- Definition of the particular problem.

Reimplemented from CSolver.

SetPressure_Inf()

void CEulerSolver::SetPressure_Inf ( su2double  p_inf )

inlinevirtual

Set the freestream pressure.

Parameters

[in]

Value

of freestream pressure.

Reimplemented from CSolver.

SetPrimitive_Gradient_GG()

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

virtual

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

Parameters

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

Reimplemented from CSolver.

SetPrimitive_Gradient_LS()

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

virtual

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

Parameters

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

Reimplemented from CSolver.

SetPrimitive_Limiter()

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

virtual

Compute the limiter of the primitive variables.

Parameters

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

Reimplemented from CSolver.

SetPrimitive_Variables()

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

virtual

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.
[in]	Output	- boolean to determine whether to print output.

Returns

- The number of non-physical points.

Reimplemented from CSolver.

Reimplemented in CNSSolver.

SetResidual_DualTime()

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

virtual

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

Parameters

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

Reimplemented from CSolver.

SetSlidingState()

void CEulerSolver::SetSlidingState ( unsigned short  val_marker, unsigned long  val_vertex, unsigned short  val_state, su2double  component  )

inlinevirtual

Set the outer state for fluid interface nodes.

Parameters

[in]	val_marker	- marker index
[in]	val_vertex	- vertex index
[in]	val_state	- requested state component
[in]	component	- set value

Reimplemented from CSolver.

SetTemperature_Inf()

void CEulerSolver::SetTemperature_Inf ( su2double  t_inf )

inlinevirtual

Set the freestream temperature.

Parameters

[in]

Value

of freestream temperature.

Reimplemented from CSolver.

SetTime_Step()

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

virtual

Compute the time step for solving the Euler equations.

Parameters

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

Reimplemented from CSolver.

Reimplemented in CNSSolver.

SetTotal_Adiab_Eff()

void CEulerSolver::SetTotal_Adiab_Eff ( su2double  val_Total_Adiab_Eff )

inlinevirtual

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 )

inlinevirtual

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 )

inlinevirtual

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

Parameters

[in]

val_Total_CD

- Value of the total drag coefficient.

Reimplemented from CSolver.

SetTotal_CD()

void CEulerSolver::SetTotal_CD ( su2double  val_Total_CD )

inlinevirtual

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

Parameters

[in]

val_Total_CD

- Value of the total drag coefficient.

Reimplemented from CSolver.

SetTotal_CD_SolidSurf()

void CEulerSolver::SetTotal_CD_SolidSurf ( su2double  val_Total_CD_SolidSurf )

inlinevirtual

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

Parameters

[in]

val_Total_CD

- Value of the total drag coefficient.

Reimplemented from CSolver.

SetTotal_CEquivArea()

void CEulerSolver::SetTotal_CEquivArea ( su2double  val_cequivarea )

inlinevirtual

Set the value of the Equivalent Area coefficient.

Parameters

[in]

val_cequivarea

- Value of the Equivalent Area coefficient.

Reimplemented from CSolver.

SetTotal_CircumferentialDistortion()

void CEulerSolver::SetTotal_CircumferentialDistortion ( su2double  val_distortion )

inlinevirtual

Set the value of the fan face distortion.

Parameters

[in]

val_cequivarea

- Value of the fan face distortion.

Reimplemented from CSolver.

SetTotal_CL()

void CEulerSolver::SetTotal_CL ( su2double  val_Total_CL )

inlinevirtual

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

Parameters

[in]

val_Total_CL

- Value of the total lift coefficient.

Reimplemented from CSolver.

SetTotal_CNearFieldOF()

void CEulerSolver::SetTotal_CNearFieldOF ( su2double  val_cnearfieldpress )

inlinevirtual

Set the value of the Near-Field pressure oefficient.

Parameters

[in]

val_cnearfieldpress

- Value of the Near-Field pressure coefficient.

Reimplemented from CSolver.

SetTotal_ComboObj()

void CEulerSolver::SetTotal_ComboObj ( su2double  ComboObj )

inlinevirtual

Set the total "combo" objective (weighted sum of other values).

Author

H. Kline

Parameters

[in]

ComboObj

- Value of the combined objective.

Reimplemented from CSolver.

SetTotal_CpDiff()

void CEulerSolver::SetTotal_CpDiff ( su2double  val_pressure )

inlinevirtual

Set the value of the Equivalent Area coefficient.

Parameters

[in]

val_cequivarea

- Value of the Equivalent Area coefficient.

Reimplemented from CSolver.

SetTotal_CQ()

void CEulerSolver::SetTotal_CQ ( su2double  val_Total_CQ )

inlinevirtual

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

Parameters

[in]

val_Total_CQ

- Value of the total torque coefficient.

Reimplemented from CSolver.

SetTotal_CT()

void CEulerSolver::SetTotal_CT ( su2double  val_Total_CT )

inlinevirtual

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

Parameters

[in]

val_Total_CT

- Value of the total thrust coefficient.

Reimplemented from CSolver.

SetTotal_Custom()

void CEulerSolver::SetTotal_Custom ( su2double  val_Total_Custom, su2double  val_coeff  )

inlinevirtual

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 )

inlinevirtual

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

Parameters

[in]

val_Total_CD

- Value of the total drag coefficient.

Reimplemented from CSolver.

SetTotal_HeatFlux()

void CEulerSolver::SetTotal_HeatFlux ( su2double  val_Total_Heat )

inlinevirtual

Store the total heat load.

Parameters

[in]

val_Total_Heat

- Value of the heat load.

Reimplemented from CSolver.

SetTotal_HeatFluxDiff()

void CEulerSolver::SetTotal_HeatFluxDiff ( su2double  val_heat )

inlinevirtual

Set the value of the Equivalent Area coefficient.

Parameters

[in]

val_cequivarea

- Value of the Equivalent Area coefficient.

Reimplemented from CSolver.

SetTotal_IDC()

void CEulerSolver::SetTotal_IDC ( su2double  val_Total_IDC )

inlinevirtual

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 )

inlinevirtual

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 )

inlinevirtual

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

Parameters

[in]

val_Total_CD

- Value of the total drag coefficient.

Reimplemented from CSolver.

SetTotal_MaxHeatFlux()

void CEulerSolver::SetTotal_MaxHeatFlux ( su2double  val_Total_MaxHeat )

inlinevirtual

Store the total heat load.

Parameters

[in]

val_Total_Heat

- Value of the heat load.

Reimplemented from CSolver.

SetTotal_MFR()

void CEulerSolver::SetTotal_MFR ( su2double  val_Total_MFR )

inlinevirtual

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

Parameters

[in]

val_Total_CD

- Value of the total drag coefficient.

Reimplemented from CSolver.

SetTotal_NetCThrust()

void CEulerSolver::SetTotal_NetCThrust ( su2double  val_Total_NetCThrust )

inlinevirtual

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 )

inlinevirtual

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 )

inlinevirtual

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 )

inlinevirtual

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

Parameters

[in]

val_Total_CD

- Value of the total drag coefficient.

Reimplemented from CSolver.

SetTotal_RadialDistortion()

void CEulerSolver::SetTotal_RadialDistortion ( su2double  val_distortion )

inlinevirtual

Set the value of the fan face distortion.

Parameters

[in]

val_cequivarea

- Value of the fan face distortion.

Reimplemented from CSolver.

SetTotal_ReverseFlow()

void CEulerSolver::SetTotal_ReverseFlow ( su2double  val_ReverseFlow )

inlinevirtual

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

Parameters

[in]

val_Total_CD

- Value of the total drag coefficient.

Reimplemented from CSolver.

SetUndivided_Laplacian()

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

virtual

Compute the undivided laplacian for the solution, except the energy equation.

Parameters

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

Reimplemented from CSolver.

Source_Residual()

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

virtual

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]	second_numerics	- Description of the second 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  )

virtual

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.

StoreTurboPerformance()

void CEulerSolver::StoreTurboPerformance ( CSolver *  solver, unsigned short  inMarkerTP  )

inlinevirtual

Compute turbomachinery performance.

Parameters

[in]	solver	- solver containing the outlet information.
[in]	inMarker	- marker related to the inlet.
[in]	outMarker	- marker related to the outlet.

Reimplemented from CSolver.

TurboPerformance()

void CEulerSolver::TurboPerformance ( CSolver *  solver, CConfig *  config, unsigned short  inMarker, unsigned short  outMarker, unsigned short  Kind_TurboPerf, unsigned short  inMarkerTP  )

virtual

Compute turbomachinery performance.

Parameters

[in]	solver	- solver containing the outlet information.
[in]	inMarker	- marker related to the inlet.
[in]	outMarker	- marker related to the outlet.

Reimplemented from CSolver.

Upwind_Residual()

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

virtual

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

Reimplemented from CSolver.

---

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

• SU2_CFD/include/solver_structure.hpp
• SU2_CFD/include/solver_structure.inl
• SU2_CFD/src/solver_direct_mean.cpp