Output Fields Reference

This page lists the screen, history and volume output fields that each output class of SU2 can write. It is made from the AddHistoryOutput and AddVolumeOutput calls in SU2_CFD/src/output/. Generated from SU2 commit 6b54b78464.

  • A field is written only when the case needs it (for example turbulence fields only with a turbulence model). For the exact list of your case, run a dry run: SU2_CFD -d your_config.cfg. It prints “Available screen/history output fields” and “Available volume output fields”.
  • How to select fields: Custom Output. How to add one: Adding Output Fields.
  • Names in italics are built at run time (for example one field per species or per marker).

COutput

Used by: All solvers. Source: SU2_CFD/src/output/COutput.cpp.

History fields (16)

Field Group Description
“REL_” + fieldIdentifier   Relative residual.
“AVG_” + it->first, “avg[” + AverageGroupName[it->first] + “]”, ScreenOutputFormat::FIXED, “AVG_” + it->first , “Average residual over all solution variables.”, HistoryFieldType::AUTO_RESIDUAL   no description
“TAVG_” + fieldIdentifier   Time averaged values.
“D_” + fieldIdentifier   Derivative value (DIRECT_DIFF=YES)
“D_TAVG_” + fieldIdentifier   Derivative of the time averaged value (DIRECT_DIFF=YES)
“CAUCHY_” + convField CAUCHY Cauchy residual value of field set with CONV_FIELD.
“CAUCHY_” + wndConvField CAUCHY Cauchy residual value of field set with WND_CONV_FIELD.
TIME_ITER ITER Time iteration index
OUTER_ITER ITER Outer iteration index
INNER_ITER ITER Inner iteration index
CUR_TIME TIME_DOMAIN Current physical time (s)
TIME_STEP TIME_DOMAIN Current time step (s)
ITER_TIME WALL_TIME Time per iteration (s)
WALL_TIME WALL_TIME Average wall-clock time since the start of inner iterations.
NONPHYSICAL_POINTS NONPHYSICAL_POINTS The number of non-physical points in the solution
output.name CUSTOM Custom output

CFVMOutput

Used by: All finite volume solvers. Source: SU2_CFD/src/output/CFVMOutput.cpp.

Volume fields (9)

Field Group Description
COORD-X COORDINATES x-component of the coordinate vector
COORD-Y COORDINATES y-component of the coordinate vector
COORD-Z COORDINATES z-component of the coordinate vector
ORTHOGONALITY MESH_QUALITY Orthogonality Angle (deg.)
ASPECT_RATIO MESH_QUALITY CV Face Area Aspect Ratio
VOLUME_RATIO MESH_QUALITY CV Sub-Volume Ratio
RANK MPI Rank of the MPI-partition
key.str() MULTIGRID Coarse mesh
LINELET LINELET Mesh lines built for the line implicit preconditioner

CFlowOutput

Used by: All flow solvers (compressible, incompressible, NEMO), also for their turbulence and species fields. Source: SU2_CFD/src/output/CFlowOutput.cpp.

History fields (117)

Field Group Description
[*” must not be split over multiple lines to ensure proper python parsing // clang-format off void CFlowOutput::AddAnalyzeSurfaceOutput(const CConfig *config){ /// DESCRIPTION: Average mass flow AddHistoryOutput(“SURFACE_MASSFLOW”, “Avg_Massflow”, ScreenOutputFormat::SCIENTIFIC, “FLOW_COEFF”, “Total average mass flow on all markers set in MARKER_ANALYZE”, HistoryFieldType::COEFFICIENT); /// DESCRIPTION: Average Mach number AddHistoryOutput(“SURFACE_MACH”, “Avg_Mach”, ScreenOutputFormat::SCIENTIFIC, “FLOW_COEFF”, “Total average mach number on all markers set in MARKER_ANALYZE”, HistoryFieldType::COEFFICIENT); /// DESCRIPTION: Average Temperature AddHistoryOutput(“SURFACE_STATIC_TEMPERATURE”,”Avg_Temp”, ScreenOutputFormat::SCIENTIFIC, “FLOW_COEFF”, “Total average temperature on all markers set in MARKER_ANALYZE”, HistoryFieldType::COEFFICIENT); /// DESCRIPTION: Average Pressure AddHistoryOutput(“SURFACE_STATIC_PRESSURE”, “Avg_Press”, ScreenOutputFormat::SCIENTIFIC, “FLOW_COEFF”, “Total average pressure on all markers set in MARKER_ANALYZE”, HistoryFieldType::COEFFICIENT); /// DESCRIPTION: Average Density AddHistoryOutput(“AVG_DENSITY”, “Avg_Density”, ScreenOutputFormat::SCIENTIFIC, “FLOW_COEFF”, “Total average density on all markers set in MARKER_ANALYZE”, HistoryFieldType::COEFFICIENT); /// DESCRIPTION: Average Enthalpy AddHistoryOutput(“AVG_ENTHALPY”, “Avg_Enthalpy”, ScreenOutputFormat::SCIENTIFIC, “FLOW_COEFF”, “Total average enthalpy on all markers set in MARKER_ANALYZE”, HistoryFieldType::COEFFICIENT); /// DESCRIPTION: Average velocity in normal direction of the surface AddHistoryOutput(“AVG_NORMALVEL”, “Avg_NormalVel”, ScreenOutputFormat::SCIENTIFIC, “FLOW_COEFF”, “Total average normal velocity on all markers set in MARKER_ANALYZE”, HistoryFieldType::COEFFICIENT); /// DESCRIPTION: Flow uniformity AddHistoryOutput(“SURFACE_UNIFORMITY”, “Uniformity”, ScreenOutputFormat::SCIENTIFIC, “FLOW_COEFF”, “Total flow uniformity on all markers set in MARKER_ANALYZE”, HistoryFieldType::COEFFICIENT); /// DESCRIPTION: Secondary strength AddHistoryOutput(“SURFACE_SECONDARY”, “Secondary_Strength”, ScreenOutputFormat::SCIENTIFIC, “FLOW_COEFF”, “Total secondary strength on all markers set in MARKER_ANALYZE”, HistoryFieldType::COEFFICIENT); /// DESCRIPTION: Momentum distortion AddHistoryOutput(“SURFACE_MOM_DISTORTION”, “Momentum_Distortion”, ScreenOutputFormat::SCIENTIFIC, “FLOW_COEFF”, “Total momentum distortion on all markers set in MARKER_ANALYZE”, HistoryFieldType::COEFFICIENT); /// DESCRIPTION: Secondary over uniformity AddHistoryOutput(“SURFACE_SECOND_OVER_UNIFORM”,”Secondary_Over_Uniformity”,ScreenOutputFormat::SCIENTIFIC,”FLOW_COEFF”, “Total secondary over uniformity on all markers set in MARKER_ANALYZE”, HistoryFieldType::COEFFICIENT); /// DESCRIPTION: Average total temperature AddHistoryOutput(“SURFACE_TOTAL_TEMPERATURE”,”Avg_TotalTemp”, ScreenOutputFormat::SCIENTIFIC, “FLOW_COEFF”, “Total average total temperature all markers set in MARKER_ANALYZE”, HistoryFieldType::COEFFICIENT); /// DESCRIPTION: Average total pressure AddHistoryOutput(“SURFACE_TOTAL_PRESSURE”, “Avg_TotalPress”, ScreenOutputFormat::SCIENTIFIC, “FLOW_COEFF”, “Total average total pressure on all markers set in MARKER_ANALYZE”, HistoryFieldType::COEFFICIENT); /// DESCRIPTION: Pressure drop if (config->GetnMarker_Analyze() >= 2) { AddHistoryOutput(“SURFACE_PRESSURE_DROP”, “Pressure_Drop”, ScreenOutputFormat::SCIENTIFIC, “FLOW_COEFF”, “Total pressure drop on all markers set in MARKER_ANALYZE”, HistoryFieldType::COEFFICIENT); } else if (rank == MASTER_NODE) { cout « “\nWARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, …)\n” « endl; } if (config->GetKind_Species_Model() == SPECIES_MODEL::SPECIES_TRANSPORT) { /// DESCRIPTION: Average Species for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++) { AddHistoryOutput(“SURFACE_SPECIES_” + std::to_string(iVar), “Avg_Species_” + std::to_string(iVar), ScreenOutputFormat::FIXED, “SPECIES_COEFF”, “Total average species “ + std::to_string(iVar) + “ on all markers set in MARKER_ANALYZE”, HistoryFieldType::COEFFICIENT); } /// DESCRIPTION: Species Variance AddHistoryOutput(“SURFACE_SPECIES_VARIANCE”, “Species_Variance”, ScreenOutputFormat::SCIENTIFIC, “SPECIES_COEFF”, “Total species variance, measure for mixing quality. On all markers set in MARKER_ANALYZE”, HistoryFieldType::COEFFICIENT); } /// END_GROUP /// BEGIN_GROUP: AERO_COEFF_SURF, DESCRIPTION: Surface values on non-solid markers. vector Marker_Analyze; for (unsigned short iMarker_Analyze = 0; iMarker_Analyze < config->GetnMarker_Analyze(); iMarker_Analyze++){ Marker_Analyze.push_back(config->GetMarker_Analyze_TagBound(iMarker_Analyze)); } /// DESCRIPTION: Average mass flow AddHistoryOutputPerSurface("SURFACE_MASSFLOW", "Avg_Massflow", ScreenOutputFormat::SCIENTIFIC, "FLOW_COEFF_SURF", Marker_Analyze, HistoryFieldType::COEFFICIENT); /// DESCRIPTION: Average Mach number AddHistoryOutputPerSurface("SURFACE_MACH", "Avg_Mach", ScreenOutputFormat::SCIENTIFIC, "FLOW_COEFF_SURF", Marker_Analyze, HistoryFieldType::COEFFICIENT); /// DESCRIPTION: Average Temperature AddHistoryOutputPerSurface("SURFACE_STATIC_TEMPERATURE","Avg_Temp", ScreenOutputFormat::SCIENTIFIC, "FLOW_COEFF_SURF", Marker_Analyze, HistoryFieldType::COEFFICIENT); /// DESCRIPTION: Average Pressure AddHistoryOutputPerSurface("SURFACE_STATIC_PRESSURE", "Avg_Press", ScreenOutputFormat::SCIENTIFIC, "FLOW_COEFF_SURF", Marker_Analyze, HistoryFieldType::COEFFICIENT); /// DESCRIPTION: Average Density AddHistoryOutputPerSurface("AVG_DENSITY", "Avg_Density", ScreenOutputFormat::SCIENTIFIC, "FLOW_COEFF_SURF", Marker_Analyze, HistoryFieldType::COEFFICIENT); /// DESCRIPTION: Average Enthalpy AddHistoryOutputPerSurface("AVG_ENTHALPY", "Avg_Enthalpy", ScreenOutputFormat::SCIENTIFIC, "FLOW_COEFF_SURF", Marker_Analyze, HistoryFieldType::COEFFICIENT); /// DESCRIPTION: Average velocity in normal direction of the surface AddHistoryOutputPerSurface("AVG_NORMALVEL", "Avg_NormalVel", ScreenOutputFormat::SCIENTIFIC, "FLOW_COEFF_SURF", Marker_Analyze, HistoryFieldType::COEFFICIENT); /// DESCRIPTION: Flow uniformity AddHistoryOutputPerSurface("SURFACE_UNIFORMITY", "Uniformity", ScreenOutputFormat::SCIENTIFIC, "FLOW_COEFF_SURF", Marker_Analyze, HistoryFieldType::COEFFICIENT); /// DESCRIPTION: Secondary strength AddHistoryOutputPerSurface("SURFACE_SECONDARY", "Secondary_Strength", ScreenOutputFormat::SCIENTIFIC, "FLOW_COEFF_SURF", Marker_Analyze, HistoryFieldType::COEFFICIENT); /// DESCRIPTION: Momentum distortion AddHistoryOutputPerSurface("SURFACE_MOM_DISTORTION", "Momentum_Distortion", ScreenOutputFormat::SCIENTIFIC, "FLOW_COEFF_SURF", Marker_Analyze, HistoryFieldType::COEFFICIENT); /// DESCRIPTION: Secondary over uniformity AddHistoryOutputPerSurface("SURFACE_SECOND_OVER_UNIFORM","Secondary_Over_Uniformity",ScreenOutputFormat::SCIENTIFIC,"FLOW_COEFF_SURF", Marker_Analyze, HistoryFieldType::COEFFICIENT); /// DESCRIPTION: Average total temperature AddHistoryOutputPerSurface("SURFACE_TOTAL_TEMPERATURE","Avg_TotalTemp", ScreenOutputFormat::SCIENTIFIC, "FLOW_COEFF_SURF", Marker_Analyze, HistoryFieldType::COEFFICIENT); /// DESCRIPTION: Average total pressure AddHistoryOutputPerSurface("SURFACE_TOTAL_PRESSURE", "Avg_TotalPress", ScreenOutputFormat::SCIENTIFIC, "FLOW_COEFF_SURF", Marker_Analyze, HistoryFieldType::COEFFICIENT); if (config->GetKind_Species_Model() == SPECIES_MODEL::SPECIES_TRANSPORT) { /// DESCRIPTION: Average Species for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++) { AddHistoryOutputPerSurface("SURFACE_SPECIES_" + std::to_string(iVar), "Avg_Species_" + std::to_string(iVar), ScreenOutputFormat::FIXED, "SPECIES_COEFF_SURF", Marker_Analyze, HistoryFieldType::COEFFICIENT); } /// DESCRIPTION: Species Variance AddHistoryOutputPerSurface("SURFACE_SPECIES_VARIANCE", "Species_Variance", ScreenOutputFormat::SCIENTIFIC, "SPECIES_COEFF_SURF", Marker_Analyze, HistoryFieldType::COEFFICIENT); } } // clang-format on void CFlowOutput::SetAnalyzeSurface(const CSolver* const*solver*](https://github.com/rois1995/SU2/blob/6b54b78464/SU2_CFD/src/output/CFlowOutput.cpp#L48)   no description
SURFACE_MASSFLOW FLOW_COEFF Total average mass flow on all markers set in MARKER_ANALYZE
SURFACE_MACH FLOW_COEFF Total average mach number on all markers set in MARKER_ANALYZE
SURFACE_STATIC_TEMPERATURE FLOW_COEFF Total average temperature on all markers set in MARKER_ANALYZE
SURFACE_STATIC_PRESSURE FLOW_COEFF Total average pressure on all markers set in MARKER_ANALYZE
AVG_DENSITY FLOW_COEFF Total average density on all markers set in MARKER_ANALYZE
AVG_ENTHALPY FLOW_COEFF Total average enthalpy on all markers set in MARKER_ANALYZE
AVG_NORMALVEL FLOW_COEFF Total average normal velocity on all markers set in MARKER_ANALYZE
SURFACE_UNIFORMITY FLOW_COEFF Total flow uniformity on all markers set in MARKER_ANALYZE
SURFACE_SECONDARY FLOW_COEFF Total secondary strength on all markers set in MARKER_ANALYZE
SURFACE_MOM_DISTORTION FLOW_COEFF Total momentum distortion on all markers set in MARKER_ANALYZE
SURFACE_SECOND_OVER_UNIFORM FLOW_COEFF Total secondary over uniformity on all markers set in MARKER_ANALYZE
SURFACE_TOTAL_TEMPERATURE FLOW_COEFF Total average total temperature all markers set in MARKER_ANALYZE
SURFACE_TOTAL_PRESSURE FLOW_COEFF Total average total pressure on all markers set in MARKER_ANALYZE
SURFACE_PRESSURE_DROP FLOW_COEFF Total pressure drop on all markers set in MARKER_ANALYZE
“SURFACE_SPECIES_” + std::to_string(iVar) SPECIES_COEFF no description
SURFACE_SPECIES_VARIANCE SPECIES_COEFF no description
” must not be split over multiple lines to ensure proper python parsing // clang-format off void CFlowOutput::AddHistoryOutputFields_ScalarRMS_RES(const CConfig config) { switch (TurbModelFamily(config->GetKind_Turb_Model())) { case TURB_FAMILY::SA: /// DESCRIPTION: Root-mean square residual of nu tilde (SA model). AddHistoryOutput(“RMS_NU_TILDE”, “rms[nu]”, ScreenOutputFormat::FIXED, “RMS_RES”, “Root-mean square residual of nu tilde (SA model).”, HistoryFieldType::RESIDUAL); if (config->GetSBSParam().StochasticBackscatter && config->GetSBSParam().SBS_Ctau > 0.0) { /// DESCRIPTION: Root-mean square residual of stochastic vector x-component (Stochastic Backscatter Model). AddHistoryOutput(“RMS_STOCH_VAR-X”* RMS_RES Root-mean square residual of stochastic vector x-component (Stochastic Backscatter Model).
RMS_NU_TILDE RMS_RES Root-mean square residual of nu tilde (SA model).
RMS_STOCH_VAR-X RMS_RES Root-mean square residual of stochastic vector x-component (Stochastic Backscatter Model).
RMS_STOCH_VAR-Y RMS_RES Root-mean square residual of stochastic vector y-component (Stochastic Backscatter Model).
RMS_STOCH_VAR-Z RMS_RES Root-mean square residual of stochastic vector z-component (Stochastic Backscatter Model).
RMS_TKE RMS_RES Root-mean square residual of kinetic energy (SST model).
RMS_DISSIPATION RMS_RES Root-mean square residual of dissipation (SST model).
RMS_INTERMITTENCY RMS_RES Root-mean square residual of intermittency (LM model).
RMS_RE_THETA_T RMS_RES Root-mean square residual of momentum thickness Reynolds number (LM model).
“RMS_SPECIES_” + std::to_string(iVar) RMS_RES Root-mean square residual of transported species.
“RMS_“+CV_name RMS_RES no description
THICKNESS FLAME_THICKNESS Flame thickness used for thickened flame correction model.
“RMS_“+scalar_name RMS_RES no description
MAX_NU_TILDE MAX_RES Maximum residual of nu tilde (SA model).
MAX_STOCH_VAR-X MAX_RES Maximum residual of stochastic vector x-component (Stochastic Backscatter Model).
MAX_STOCH_VAR-Y MAX_RES Maximum residual of stochastic vector y-component (Stochastic Backscatter Model).
MAX_STOCH_VAR-Z MAX_RES Maximum residual of stochastic vector z-component (Stochastic Backscatter Model).
MAX_TKE MAX_RES Maximum residual of kinetic energy (SST model).
MAX_DISSIPATION MAX_RES Maximum residual of dissipation (SST model).
MAX_INTERMITTENCY MAX_RES Maximum residual of the intermittency (LM model).
MAX_RE_THETA_T MAX_RES Maximum residual of the momentum thickness Reynolds number (LM model).
“MAX_SPECIES_” + std::to_string(iVar) MAX_RES Maximum residual of transported species.
“MAX_” + cv_name MAX_RES no description
“MAX_” + scalar_name MAX_RES no description
BGS_NU_TILDE BGS_RES BGS residual of nu tilde (SA model).
BGS_STOCH_VAR-X BGS_RES BGS residual of stochastic vector x-component (Stochastic Backscatter Model).
BGS_STOCH_VAR-Y BGS_RES BGS residual of stochastic vector y-component (Stochastic Backscatter Model).
BGS_STOCH_VAR-Z BGS_RES BGS residual of stochastic vector z-component (Stochastic Backscatter Model).
BGS_TKE BGS_RES BGS residual of kinetic energy (SST model).
BGS_DISSIPATION BGS_RES BGS residual of dissipation (SST model).
BGS_INTERMITTENCY BGS_RES BGS residual of the intermittency (LM model).
BGS_RE_THETA_T BGS_RES BGS residual of the momentum thickness Reynolds number (LM model).
“BGS_SPECIES_” + std::to_string(iVar) BGS_RES Maximum residual of transported species.
“BGS_” + cv_name BGS_RES no description
“BGS_“+scalar_name BGS_RES no description
LINSOL_ITER_TURB LINSOL Number of iterations of the linear solver for turbulence solver.
LINSOL_RESIDUAL_TURB LINSOL Residual of the linear solver for turbulence solver.
LINSOL_ITER_TRANS LINSOL Number of iterations of the linear solver for transition solver.
LINSOL_RESIDUAL_TRANS LINSOL Residual of the linear solver for transition solver.
LINSOL_ITER_SPECIES LINSOL Number of iterations of the linear solver for species solver.
LINSOL_RESIDUAL_SPECIES LINSOL Residual of the linear solver for species solver.
LINSOL_ITER_FLAMELET LINSOL Number of iterations of the linear solver for flamelet solver.
LINSOL_RESIDUAL_FLAMELET LINSOL Residual of the linear solver for flamelet solver.
REFERENCE_FORCE AERO_COEFF Reference force used to compute aerodynamic coefficients
DRAG AERO_COEFF Total drag coefficient on all surfaces set with MARKER_MONITORING
LIFT AERO_COEFF Total lift coefficient on all surfaces set with MARKER_MONITORING
SIDEFORCE AERO_COEFF Total sideforce coefficient on all surfaces set with MARKER_MONITORING
MOMENT_X AERO_COEFF Total momentum x-component on all surfaces set with MARKER_MONITORING
MOMENT_Y AERO_COEFF Total momentum y-component on all surfaces set with MARKER_MONITORING
MOMENT_Z AERO_COEFF Total momentum z-component on all surfaces set with MARKER_MONITORING
FORCE_X AERO_COEFF Total force x-component on all surfaces set with MARKER_MONITORING
FORCE_Y AERO_COEFF Total force y-component on all surfaces set with MARKER_MONITORING
FORCE_Z AERO_COEFF Total force z-component on all surfaces set with MARKER_MONITORING
EFFICIENCY AERO_COEFF Total lift-to-drag ratio on all surfaces set with MARKER_MONITORING
AOA AOA Angle of attack
COMBO COMBO Combined obj. function value.
CUSTOM_OBJFUNC COMBO Custom obj. function value.
TOTAL_HEATFLUX HEAT Total heatflux on all surfaces set with MARKER_MONITORING.
MAXIMUM_HEATFLUX HEAT Maximum heatflux across all surfaces set with MARKER_MONITORING.
FIGURE_OF_MERIT ROTATING_FRAME Thrust over torque
THRUST ROTATING_FRAME Thrust coefficient
TORQUE ROTATING_FRAME Torque coefficient
INVERSE_DESIGN_PRESSURE CP_DIFF Cp difference for inverse design
EQUIVALENT_AREA EQUIVALENT_AREA Equivalent area
“EntropyIn_” + tag TURBO_PERF no description
“EntropyOut_” + tag TURBO_PERF no description
“TotalEntahalpyIn_” + tag TURBO_PERF no description
“TotalEnthalpyOut_” + tag TURBO_PERF no description
“TotalPressureIn_” + tag TURBO_PERF no description
“TotalPressureOut_” + tag TURBO_PERF no description
“PressureIn_” + tag TURBO_PERF no description
“PressureOut_” + tag TURBO_PERF no description
“TotalTemperatureIn_” + tag TURBO_PERF no description
“TotalTemperatureOut_” + tag TURBO_PERF no description
“TemperatureIn_” + tag TURBO_PERF no description
“TemperatureOut_” + tag TURBO_PERF no description
“DensityIn_” + tag TURBO_PERF no description
“DensityOut_” + tag TURBO_PERF no description
“NormalVelocityIn_” + tag TURBO_PERF no description
“NormalVelocityOut_” + tag TURBO_PERF no description
“TangentialVelocityIn_” + tag TURBO_PERF no description
“TangentialVelocityOut_” + tag TURBO_PERF no description
“MassFlowIn_” + tag TURBO_PERF no description
“MassFlowOut_” + tag TURBO_PERF no description
“MachIn_” + tag TURBO_PERF no description
“MachOut_” + tag TURBO_PERF no description
“AbsFlowAngleIn_” + tag TURBO_PERF no description
“AbsFlowAngleOut_” + tag TURBO_PERF no description
“RelFlowAngleIn_” + tag TURBO_PERF no description
“RelFlowAngleOut_” + tag TURBO_PERF no description
“KineticEnergyLoss_” + tag TURBO_PERF Blade Kinetic Energy Loss Coefficient
“TotPressureLoss_” + tag TURBO_PERF Blade Pressure Loss Coefficient
EntropyGeneration TURBO_PERF Machine entropy generation
EulerianWork TURBO_PERF Machine Eulerian work
TotalStaticEfficiency TURBO_PERF Machine total-to-static efficiency
TotalTotalEfficiency TURBO_PERF Machine total-to-total efficiency
PressureRatioTS TURBO_PERF Machine total-to-static pressure ratio
PressureRatioTT TURBO_PERF Machine total-to-toal pressure ratio
KineticEnergyLoss_Stage TURBO_PERF Machine Kinetic Energy Loss Coefficient
TotPressureLoss_Stage TURBO_PERF Machine Pressure Loss Coefficient

History, per surface fields (27)

Field Group Description
SURFACE_MASSFLOW FLOW_COEFF_SURF no description
SURFACE_MACH FLOW_COEFF_SURF no description
SURFACE_STATIC_TEMPERATURE FLOW_COEFF_SURF no description
SURFACE_STATIC_PRESSURE FLOW_COEFF_SURF no description
AVG_DENSITY FLOW_COEFF_SURF no description
AVG_ENTHALPY FLOW_COEFF_SURF no description
AVG_NORMALVEL FLOW_COEFF_SURF no description
SURFACE_UNIFORMITY FLOW_COEFF_SURF no description
SURFACE_SECONDARY FLOW_COEFF_SURF no description
SURFACE_MOM_DISTORTION FLOW_COEFF_SURF no description
SURFACE_SECOND_OVER_UNIFORM FLOW_COEFF_SURF no description
SURFACE_TOTAL_TEMPERATURE FLOW_COEFF_SURF no description
SURFACE_TOTAL_PRESSURE FLOW_COEFF_SURF no description
“SURFACE_SPECIES_” + std::to_string(iVar) SPECIES_COEFF_SURF no description
SURFACE_SPECIES_VARIANCE SPECIES_COEFF_SURF no description
DRAG_ON_SURFACE AERO_COEFF_SURF no description
LIFT_ON_SURFACE AERO_COEFF_SURF no description
SIDEFORCE_ON_SURFACE AERO_COEFF_SURF no description
MOMENT-X_ON_SURFACE AERO_COEFF_SURF no description
MOMENT-Y_ON_SURFACE AERO_COEFF_SURF no description
MOMENT-Z_ON_SURFACE AERO_COEFF_SURF no description
FORCE-X_ON_SURFACE AERO_COEFF_SURF no description
FORCE-Y_ON_SURFACE AERO_COEFF_SURF no description
FORCE-Z_ON_SURFACE AERO_COEFF_SURF no description
EFFICIENCY_ON_SURFACE AERO_COEFF_SURF no description
TOTAL_HEATFLUX_ON_SURFACE HEAT_SURF no description
MAXIMUM_HEATFLUX_ON_SURFACE HEAT_SURF no description

Volume fields (85)

Field Group Description
NU_TILDE SOLUTION Spalart-Allmaras variable
STOCHVAR_X SOLUTION x-component of the stochastic vector potential
STOCHVAR_Y SOLUTION y-component of the stochastic vector potential
STOCHVAR_Z SOLUTION z-component of the stochastic vector potential
TKE SOLUTION Turbulent kinetic energy
DISSIPATION SOLUTION Rate of dissipation
INTERMITTENCY SOLUTION LM intermittency
RE_THETA_T SOLUTION LM RE_THETA_T
“SPECIES_” + std::to_string(iVar) SOLUTION no description
cv_name SOLUTION no description
species_name SOLUTION no description
RES_NU_TILDE RESIDUAL Residual of the Spalart-Allmaras variable
RES_STOCHVAR_X RESIDUAL Residual of the x-component of the stochastic vector potential
RES_STOCHVAR_Y RESIDUAL Residual of the y-component of the stochastic vector potential
RES_STOCHVAR_Z RESIDUAL Residual of the z-component of the stochastic vector potential
RES_TKE RESIDUAL Residual of turbulent kinetic energy
RES_DISSIPATION RESIDUAL Residual of the rate of dissipation
“RES_SPECIES_” + std::to_string(iVar) RESIDUAL no description
“RES_“+cv_name RESIDUAL no description
“RES_” + species_name RESIDUAL no description
RES_INTERMITTENCY RESIDUAL Residual of LM intermittency
RES_RE_THETA_T RESIDUAL Residual of LM RE_THETA_T
LIMITER_NU_TILDE LIMITER Limiter value of the Spalart-Allmaras variable
LIMITER_TKE LIMITER Limiter value of turb. kinetic energy
LIMITER_DISSIPATION LIMITER Limiter value of dissipation rate
“LIMITER_SPECIES_” + std::to_string(iVar) LIMITER no description
“LIMITER_” + cv_name LIMITER no description
“LIMITER_” + species_name LIMITER no description
“DIFFUSIVITY_” + std::to_string(iVar) PRIMITIVE no description
INTERMITTENCY_SEP PRIMITIVE LM intermittency
INTERMITTENCY_EFF PRIMITIVE LM RE_THETA_T
TURB_INDEX PRIMITIVE Turbulence index
EDDY_VISCOSITY PRIMITIVE Turbulent eddy viscosity
“SPECIES_UDS_” + std::to_string(iVar) SOURCE no description
“SOURCE_“+cv_name SOURCE no description
“SOURCE_” + species_name SOURCE no description
flamelet_config_options.lookup_names[i_lookup] LOOKUP no description
TABLE_MISSES LOOKUP Lookup table misses
DES_LENGTHSCALE DDES DES length scale value
WALL_DISTANCE DDES Wall distance value
LES_SENSOR DDES LES sensor value
STOCHSOURCE_X BACKSCATTER x-component of the stochastic source vector
STOCHSOURCE_Y BACKSCATTER y-component of the stochastic source vector
STOCHSOURCE_Z BACKSCATTER z-component of the stochastic source vector
ENERGY_BACKSCATTER_RATIO BACKSCATTER Energy backscatter from unresolved to resolved scales (divided by the turbulent dissipation of resolved kinetic energy)
VORTICITY_X VORTEX_IDENTIFICATION x-component of the vorticity vector
VORTICITY_Y VORTEX_IDENTIFICATION y-component of the vorticity vector
VORTICITY_Z VORTEX_IDENTIFICATION z-component of the vorticity vector
VORTICITY VORTEX_IDENTIFICATION Value of the vorticity
Q_CRITERION VORTEX_IDENTIFICATION Value of the Q-Criterion
DELTA_TIME TIMESTEP Value of the local timestep for the flow variables
CFL TIMESTEP Value of the local CFL for the flow variables
TURB_DELTA_TIME TIMESTEP Value of the local timestep for the turbulence variables
TURB_CFL TIMESTEP Value of the local CFL for the turbulence variables
MEAN_DENSITY TIME_AVERAGE Mean density
MEAN_VELOCITY-X TIME_AVERAGE Mean velocity x-component
MEAN_VELOCITY-Y TIME_AVERAGE Mean velocity y-component
MEAN_VELOCITY-Z TIME_AVERAGE Mean velocity z-component
MEAN_PRESSURE TIME_AVERAGE Mean pressure
MEAN_SKIN_FRICTION-X TIME_AVERAGE Mean skin friction x-component
MEAN_SKIN_FRICTION-Y TIME_AVERAGE Mean skin friction y-component
MEAN_SKIN_FRICTION-Z TIME_AVERAGE Mean skin friction z-component
RMS_U TIME_AVERAGE RMS u
RMS_V TIME_AVERAGE RMS v
RMS_UV TIME_AVERAGE RMS uv
RMS_P TIME_AVERAGE RMS Pressure
UUPRIME TIME_AVERAGE Mean Reynolds-stress component u’u’
VVPRIME TIME_AVERAGE Mean Reynolds-stress component v’v’
UVPRIME TIME_AVERAGE Mean Reynolds-stress component u’v’
PPRIME TIME_AVERAGE Mean pressure fluctuation p’p’
RMS_W TIME_AVERAGE RMS u
RMS_UW TIME_AVERAGE RMS uw
RMS_VW TIME_AVERAGE RMS vw
WWPRIME TIME_AVERAGE Mean Reynolds-stress component w’w’
UWPRIME TIME_AVERAGE Mean Reynolds-stress component w’u’
VWPRIME TIME_AVERAGE Mean Reynolds-stress component w’v’
MODELED_REYNOLDS_STRESS_XX TIME_AVERAGE Modeled Reynolds stress xx-component
MODELED_REYNOLDS_STRESS_YY TIME_AVERAGE Modeled Reynolds stress yy-component
MODELED_REYNOLDS_STRESS_XY TIME_AVERAGE Modeled Reynolds stress xy-component
MODELED_REYNOLDS_STRESS_ZZ TIME_AVERAGE Modeled Reynolds stress zz-component
MODELED_REYNOLDS_STRESS_XZ TIME_AVERAGE Modeled Reynolds stress xz-component
MODELED_REYNOLDS_STRESS_YZ TIME_AVERAGE Modeled Reynolds stress yz-component
STOCHASTIC_REYNOLDS_STRESS_XY TIME_AVERAGE Stochastic Reynolds stress xy-component
STOCHASTIC_REYNOLDS_STRESS_XZ TIME_AVERAGE Stochastic Reynolds stress xz-component
STOCHASTIC_REYNOLDS_STRESS_YZ TIME_AVERAGE Stochastic Reynolds stress yz-component

CFlowCompOutput

Used by: Compressible flow. Source: SU2_CFD/src/output/CFlowCompOutput.cpp.

History fields (31)

Field Group Description
RMS_DENSITY RMS_RES Root-mean square residual of the density.
RMS_MOMENTUM-X RMS_RES Root-mean square residual of the momentum x-component.
RMS_MOMENTUM-Y RMS_RES Root-mean square residual of the momentum y-component.
RMS_MOMENTUM-Z RMS_RES Root-mean square residual of the momentum z-component.
RMS_ENERGY RMS_RES Root-mean square residual of the energy.
MAX_DENSITY MAX_RES Maximum square residual of the density.
MAX_MOMENTUM-X MAX_RES Maximum square residual of the momentum x-component.
MAX_MOMENTUM-Y MAX_RES Maximum square residual of the momentum y-component.
MAX_MOMENTUM-Z MAX_RES Maximum residual of the z-component.
MAX_ENERGY MAX_RES Maximum residual of the energy.
BGS_DENSITY BGS_RES BGS residual of the density.
BGS_MOMENTUM-X BGS_RES BGS residual of the momentum x-component.
BGS_MOMENTUM-Y BGS_RES BGS residual of the momentum y-component.
BGS_MOMENTUM-Z BGS_RES BGS residual of the z-component.
BGS_ENERGY BGS_RES BGS residual of the energy.
LINSOL_ITER LINSOL Number of iterations of the linear solver.
LINSOL_RESIDUAL LINSOL Residual of the linear solver.
MIN_DELTA_TIME CFL_NUMBER Current minimum local time step
MAX_DELTA_TIME CFL_NUMBER Current maximum local time step
MIN_CFL CFL_NUMBER Current minimum of the local CFL numbers
MAX_CFL CFL_NUMBER Current maximum of the local CFL numbers
AVG_CFL CFL_NUMBER Current average of the local CFL numbers
DELTA_CL FIXED_CL Difference between Target CL and current CL
PREV_AOA FIXED_CL Angle of Attack at the previous iteration of the Fixed CL driver
CHANGE_IN_AOA FIXED_CL Last change in Angle of Attack by Fixed CL Driver
CL_DRIVER_COMMAND FIXED_CL CL Driver’s control command
DEFORM_MIN_VOLUME DEFORM Minimum volume in the mesh
DEFORM_MAX_VOLUME DEFORM Maximum volume in the mesh
DEFORM_ITER DEFORM Linear solver iterations for the mesh deformation
DEFORM_RESIDUAL DEFORM Residual of the linear solver for the mesh deformation
BUFFET AERO_COEFF Buffet sensor

History, per surface fields (2)

Field Group Description
PLUNGE AEROELASTIC no description
PITCH AEROELASTIC no description

Volume fields (38)

Field Group Description
DENSITY SOLUTION Density
MOMENTUM-X SOLUTION x-component of the momentum vector
MOMENTUM-Y SOLUTION y-component of the momentum vector
MOMENTUM-Z SOLUTION z-component of the momentum vector
ENERGY SOLUTION Energy
GRID_VELOCITY-X GRID_VELOCITY x-component of the grid velocity vector
GRID_VELOCITY-Y GRID_VELOCITY y-component of the grid velocity vector
GRID_VELOCITY-Z GRID_VELOCITY z-component of the grid velocity vector
PRESSURE PRIMITIVE Pressure
TEMPERATURE PRIMITIVE Temperature
MACH PRIMITIVE Mach number
PRESSURE_COEFF PRIMITIVE Pressure coefficient
VELOCITY-X PRIMITIVE x-component of the velocity vector
VELOCITY-Y PRIMITIVE y-component of the velocity vector
VELOCITY-Z PRIMITIVE z-component of the velocity vector
EXTRAPOLATION PRIMITIVE no description
FLUIDMODEL_NEWTONITER PRIMITIVE Number of iterations evaluated by the Newton solver
ENTROPY PRIMITIVE Fluid entropy value
LAMINAR_VISCOSITY PRIMITIVE Laminar viscosity
SKIN_FRICTION-X PRIMITIVE x-component of the skin friction vector
SKIN_FRICTION-Y PRIMITIVE y-component of the skin friction vector
SKIN_FRICTION-Z PRIMITIVE z-component of the skin friction vector
HEAT_FLUX PRIMITIVE Heat-flux
Y_PLUS PRIMITIVE Non-dim. wall distance (Y-Plus)
RES_DENSITY RESIDUAL Residual of the density
RES_MOMENTUM-X RESIDUAL Residual of the x-momentum component
RES_MOMENTUM-Y RESIDUAL Residual of the y-momentum component
RES_MOMENTUM-Z RESIDUAL Residual of the z-momentum component
RES_ENERGY RESIDUAL Residual of the energy
LIMITER_TEMPERATURE LIMITER Limiter value of the temperature
LIMITER_VELOCITY-X LIMITER Limiter value of the x-velocity
LIMITER_VELOCITY-Y LIMITER Limiter value of the y-velocity
LIMITER_VELOCITY-Z LIMITER Limiter value of the z-velocity
LIMITER_PRESSURE LIMITER Limiter value of the pressure
LIMITER_DENSITY LIMITER Limiter value of the density
LIMITER_ENTHALPY LIMITER Limiter value of the enthalpy
MSW_SENSOR LIMITER Value of sensor used to switch from SW to MSW
ROE_DISSIPATION ROE_DISSIPATION Value of the Roe dissipation

CFlowIncOutput

Used by: Incompressible flow. Source: SU2_CFD/src/output/CFlowIncOutput.cpp.

History fields (38)

Field Group Description
RMS_PRESSURE RMS_RES Root-mean square residual of the pressure.
RMS_VELOCITY-X RMS_RES Root-mean square residual of the velocity x-component.
RMS_VELOCITY-Y RMS_RES Root-mean square residual of the velocity y-component.
RMS_VELOCITY-Z RMS_RES Root-mean square residual of the velocity z-component.
RMS_TEMPERATURE RMS_RES Root-mean square residual of the temperature.
RMS_ENTHALPY RMS_RES Root-mean square residual of the enthalpy.
RMS_RAD_ENERGY RMS_RES Root-mean square residual of the radiative energy.
MAX_PRESSURE MAX_RES Maximum residual of the pressure.
MAX_VELOCITY-X MAX_RES Maximum residual of the velocity x-component.
MAX_VELOCITY-Y MAX_RES Maximum residual of the velocity y-component.
MAX_VELOCITY-Z MAX_RES Maximum residual of the velocity z-component.
MAX_TEMPERATURE MAX_RES Root-mean square residual of the temperature.
MAX_ENTHALPY MAX_RES Maximum residual of the enthalpy.
BGS_PRESSURE BGS_RES BGS residual of the pressure.
BGS_VELOCITY-X BGS_RES BGS residual of the velocity x-component.
BGS_VELOCITY-Y BGS_RES BGS residual of the velocity y-component.
BGS_VELOCITY-Z BGS_RES BGS residual of the velocity z-component.
BGS_TEMPERATURE BGS_RES BGS residual of the temperature.
BGS_ENTHALPY BGS_RES BGS residual of the enthalpy.
BGS_RAD_ENERGY BGS_RES BGS residual of the radiative energy.
AOA AOA Angle of attack
LINSOL_ITER LINSOL Number of iterations of the linear solver.
LINSOL_RESIDUAL LINSOL Residual of the linear solver.
LINSOL_POISSON_ITER LINSOL Number of iterations of the poisson solver.
LINSOL_POISSON_RESIDUAL LINSOL Residual of the poisson solver.
MIN_DELTA_TIME CFL_NUMBER Current minimum local time step
MAX_DELTA_TIME CFL_NUMBER Current maximum local time step
MIN_CFL CFL_NUMBER Current minimum of the local CFL numbers
MAX_CFL CFL_NUMBER Current maximum of the local CFL numbers
AVG_CFL CFL_NUMBER Current average of the local CFL numbers
DEFORM_MIN_VOLUME DEFORM Minimum volume in the mesh
DEFORM_MAX_VOLUME DEFORM Maximum volume in the mesh
DEFORM_ITER DEFORM Linear solver iterations for the mesh deformation
DEFORM_RESIDUAL DEFORM Residual of the linear solver for the mesh deformation
STREAMWISE_MASSFLOW STREAMWISE_PERIODIC Massflow in streamwise periodic flow
STREAMWISE_DP STREAMWISE_PERIODIC Pressure drop in streamwise periodic flow
STREAMWISE_HEAT STREAMWISE_PERIODIC Integrated heat for streamwise periodic flow
AVG_TEMPERATURE HEAT Average temperature on all surfaces set with MARKER_MONITORING.

Volume fields (34)

Field Group Description
PRESSURE SOLUTION Pressure
VELOCITY-X SOLUTION x-component of the velocity vector
VELOCITY-Y SOLUTION y-component of the velocity vector
VELOCITY-Z SOLUTION z-component of the velocity vector
TEMPERATURE SOLUTION Temperature
ENTHALPY SOLUTION Enthalpy
P1-RAD SOLUTION Radiative Energy
GRID_VELOCITY-X GRID_VELOCITY x-component of the grid velocity vector
GRID_VELOCITY-Y GRID_VELOCITY y-component of the grid velocity vector
GRID_VELOCITY-Z GRID_VELOCITY z-component of the grid velocity vector
PRESSURE_COEFF PRIMITIVE Pressure coefficient
DENSITY PRIMITIVE Density
LAMINAR_VISCOSITY PRIMITIVE Laminar viscosity
HEAT_CAPACITY PRIMITIVE Heat capacity
THERMAL_CONDUCTIVITY PRIMITIVE Thermal conductivity
SKIN_FRICTION-X PRIMITIVE x-component of the skin friction vector
SKIN_FRICTION-Y PRIMITIVE y-component of the skin friction vector
SKIN_FRICTION-Z PRIMITIVE z-component of the skin friction vector
HEAT_FLUX PRIMITIVE Heat-flux
Y_PLUS PRIMITIVE Non-dim. wall distance (Y-Plus)
INTERMITTENCY INTERMITTENCY Intermittency
RES_PRESSURE RESIDUAL Residual of the pressure
RES_VELOCITY-X RESIDUAL Residual of the x-velocity component
RES_VELOCITY-Y RESIDUAL Residual of the y-velocity component
RES_VELOCITY-Z RESIDUAL Residual of the z-velocity component
RES_ENTHALPY RESIDUAL Residual of the enthalpy
LIMITER_PRESSURE LIMITER Limiter value of the pressure
LIMITER_VELOCITY-X LIMITER Limiter value of the x-velocity
LIMITER_VELOCITY-Y LIMITER Limiter value of the y-velocity
LIMITER_VELOCITY-Z LIMITER Limiter value of the z-velocity
LIMITER_TEMPERATURE LIMITER Limiter value of the temperature
LIMITER_ENTHALPY LIMITER Limiter value of the enthalpy
RECOVERED_PRESSURE SOLUTION Recovered physical pressure
RECOVERED_TEMPERATURE SOLUTION Recovered physical temperature

CNEMOCompOutput

Used by: Non-equilibrium flow (NEMO). Source: SU2_CFD/src/output/CNEMOCompOutput.cpp.

History fields (19)

Field Group Description
prefix + “_DENSITY_” + std::to_string(iSpecies)   no description
prefix + “_MOMENTUM-X”   no description
prefix + “_MOMENTUM-Y”   no description
prefix + “_MOMENTUM-Z”   no description
prefix + “_ENERGY”   no description
prefix + “_ENERGY_VE”   no description
LINSOL_ITER LINSOL Number of iterations of the linear solver.
LINSOL_RESIDUAL LINSOL Residual of the linear solver.
MIN_CFL CFL_NUMBER Current minimum of the local CFL numbers
MAX_CFL CFL_NUMBER Current maximum of the local CFL numbers
AVG_CFL CFL_NUMBER Current average of the local CFL numbers
DELTA_CL FIXED_CL Difference between Target CL and current CL
PREV_AOA FIXED_CL Angle of Attack at the previous iteration of the Fixed CL driver
CHANGE_IN_AOA FIXED_CL Last change in Angle of Attack by Fixed CL Driver
CL_DRIVER_COMMAND FIXED_CL CL Driver’s control command
DEFORM_MIN_VOLUME DEFORM Minimum volume in the mesh
DEFORM_MAX_VOLUME DEFORM Maximum volume in the mesh
DEFORM_ITER DEFORM Linear solver iterations for the mesh deformation
DEFORM_RESIDUAL DEFORM Residual of the linear solver for the mesh deformation

History, per surface fields (2)

Field Group Description
PLUNGE AEROELASTIC no description
PITCH AEROELASTIC no description

Volume fields (37)

Field Group Description
“DENSITY_” + std::to_string(iSpecies) SOLUTION no description
MOMENTUM-X SOLUTION x-component of the momentum vector
MOMENTUM-Y SOLUTION y-component of the momentum vector
MOMENTUM-Z SOLUTION z-component of the momentum vector
ENERGY SOLUTION Energy
ENERGY_VE SOLUTION Energy_ve
“MASSFRAC_” + std::to_string(iSpecies) AUXILIARY no description
GRID_VELOCITY-X GRID_VELOCITY x-component of the grid velocity vector
GRID_VELOCITY-Y GRID_VELOCITY y-component of the grid velocity vector
GRID_VELOCITY-Z GRID_VELOCITY z-component of the grid velocity vector
PRESSURE PRIMITIVE Pressure
TEMPERATURE_TR PRIMITIVE Temperature_tr
TEMPERATURE_VE PRIMITIVE Temperature_ve
VELOCITY-X PRIMITIVE x-component of the velocity vector
VELOCITY-Y PRIMITIVE y-component of the velocity vector
VELOCITY-Z PRIMITIVE z-component of the velocity vector
MACH PRIMITIVE Mach number
PRESSURE_COEFF PRIMITIVE Pressure coefficient
LAMINAR_VISCOSITY PRIMITIVE Laminar viscosity
SKIN_FRICTION-X PRIMITIVE x-component of the skin friction vector
SKIN_FRICTION-Y PRIMITIVE y-component of the skin friction vector
SKIN_FRICTION-Z PRIMITIVE z-component of the skin friction vector
THERMAL_CONDUCTIVITY_TR PRIMITIVE Translational-rotational thermal conductivity
THERMAL_CONDUCTIVITY_VE PRIMITIVE Vibrational-electronic thermal conductivity
HEAT_FLUX PRIMITIVE Heat-flux
Y_PLUS PRIMITIVE Non-dim. wall distance (Y-Plus)
“RES_DENSITY_” + std::to_string(iSpecies) RESIDUAL no description
RES_MOMENTUM-X RESIDUAL Residual of the x-momentum component
RES_MOMENTUM-Y RESIDUAL Residual of the y-momentum component
RES_MOMENTUM-Z RESIDUAL Residual of the z-momentum component
RES_ENERGY RESIDUAL Residual of the energy
RES_ENERGY_VE RESIDUAL Residual of the energy_ve
LIMITER_DENSITY LIMITER Limiter value of the density
LIMITER_MOMENTUM-X LIMITER Limiter value of the x-momentum
LIMITER_MOMENTUM-Y LIMITER Limiter value of the y-momentum
LIMITER_MOMENTUM-Z LIMITER Limiter value of the z-momentum
LIMITER_ENERGY LIMITER Limiter value of the energy

CFlowCompFEMOutput

Used by: Finite element flow (DG-FEM). Source: SU2_CFD/src/output/CFlowCompFEMOutput.cpp.

History fields (11)

Field Group Description
RMS_DENSITY RMS_RES Root-mean square residual of the density.
RMS_MOMENTUM-X RMS_RES Root-mean square residual of the momentum x-component.
RMS_MOMENTUM-Y RMS_RES Root-mean square residual of the momentum y-component.
RMS_MOMENTUM-Z RMS_RES Root-mean square residual of the momentum z-component.
RMS_ENERGY RMS_RES Root-mean square residual of the energy.
MAX_DENSITY MAX_RES Maximum square residual of the density.
MAX_MOMENTUM-X MAX_RES Maximum square residual of the momentum x-component.
MAX_MOMENTUM-Y MAX_RES Maximum square residual of the momentum y-component.
MAX_MOMENTUM-Z MAX_RES Maximum residual of the z-component.
MAX_ENERGY MAX_RES Maximum residual of the energy.
CFL_NUMBER CFL_NUMBER Current value of the CFL number

Volume fields (14)

Field Group Description
COORD-X COORDINATES x-component of the coordinate vector
COORD-Y COORDINATES y-component of the coordinate vector
COORD-Z COORDINATES z-component of the coordinate vector
DENSITY SOLUTION Density
MOMENTUM-X SOLUTION x-component of the momentum vector
MOMENTUM-Y SOLUTION y-component of the momentum vector
MOMENTUM-Z SOLUTION z-component of the momentum vector
ENERGY SOLUTION Energy
PRESSURE PRIMITIVE Pressure
TEMPERATURE PRIMITIVE Temperature
MACH PRIMITIVE Mach number
PRESSURE_COEFF PRIMITIVE Pressure coefficient
LAMINAR_VISCOSITY PRIMITIVE Laminar viscosity
EDDY_VISCOSITY PRIMITIVE Turbulent eddy viscosity

CHeatOutput

Used by: Heat equation. Source: SU2_CFD/src/output/CHeatOutput.cpp.

History fields (9)

Field Group Description
RMS_TEMPERATURE RMS_RES Root mean square residual of the temperature
MAX_TEMPERATURE MAX_RES Maximum residual of the temperature
BGS_TEMPERATURE BGS_RES Block-Gauss-Seidel residual of the temperature
TOTAL_HEATFLUX HEAT Total heatflux on all surfaces defined in MARKER_MONITORING
AVG_TEMPERATURE HEAT Average temperature on all surfaces defined in MARKER_MONITORING
CFL_NUMBER CFL_NUMBER Current value of the CFL number
LINSOL_ITER LINSOL Number of iterations of the linear solver.
LINSOL_RESIDUAL LINSOL Residual of the linear solver.
COMBO COMBO Combined obj. function value.

Volume fields (3)

Field Group Description
TEMPERATURE SOLUTION Temperature
HEAT_FLUX PRIMITIVE Heatflux
RES_TEMPERATURE RESIDUAL Residual of the temperature

CElasticityOutput

Used by: Structural analysis. Source: SU2_CFD/src/output/CElasticityOutput.cpp.

History fields (23)

Field Group Description
LINSOL_ITER LINSOL Number of iterations of the linear solver.
LINSOL_RESIDUAL LINSOL Residual of the linear solver.
RMS_UTOL RMS_RES Norm of displacement increment
RMS_RTOL RMS_RES Norm of residual
RMS_ETOL RMS_RES Norm of energy/work increment
RMS_DISP_X RMS_RES Residual of X displacement
RMS_DISP_Y RMS_RES Residual of Y displacement
RMS_DISP_Z RMS_RES Residual of Z displacement
BGS_DISP_X BGS_RES BGS residual of X displacement
BGS_DISP_Y BGS_RES BGS residual of Y displacement
BGS_DISP_Z BGS_RES BGS residual of Z displacement
VMS Maximum Von-Misses stress VMS
LOAD_RAMP Fraction of total load (ramped) LOAD_RAMP
LOAD_INCREMENT Percent of total load (incremental) LOAD_INCREMENT
REFERENCE_NODE STRUCT_COEFF Distance to reference node
TOPOL_COMPLIANCE STRUCT_COEFF Structural compliance
STRESS_PENALTY STRUCT_COEFF Aggregate stress penalty
REFERENCE_GEOMETRY STRUCT_COEFF L2 norm of difference wrt reference geometry
VOLUME_FRACTION STRUCT_COEFF Fraction of solid material
TOPOL_DISCRETENESS STRUCT_COEFF Discreteness of the material distribution
COMBO COMBO Combined obj. function value.
LINSOL_ITER_HEAT LINSOL Number of iterations of the linear solver.
LINSOL_RESIDUAL_HEAT LINSOL Residual of the linear solver.

Volume fields (23)

Field Group Description
COORD-X COORDINATES x-component of the coordinate vector
COORD-Y COORDINATES y-component of the coordinate vector
COORD-Z COORDINATES z-component of the coordinate vector
DISPLACEMENT-X SOLUTION x-component of the displacement vector
DISPLACEMENT-Y SOLUTION y-component of the displacement vector
DISPLACEMENT-Z SOLUTION z-component of the displacement vector
VELOCITY-X SOLUTION x-component of the velocity vector
VELOCITY-Y SOLUTION y-component of the velocity vector
VELOCITY-Z SOLUTION z-component of the velocity vector
ACCELERATION-X SOLUTION x-component of the acceleration vector
ACCELERATION-Y SOLUTION y-component of the acceleration vector
ACCELERATION-Z SOLUTION z-component of the acceleration vector
TEMPERATURE SOLUTION Temperature
STRESS-XX STRESS x-component of the normal stress vector
STRESS-YY STRESS y-component of the normal stress vector
STRESS-ZZ STRESS z-component of the normal stress vector
STRESS-XY STRESS xy shear stress component
STRESS-XZ STRESS xz shear stress component
STRESS-YZ STRESS yz shear stress component
VON_MISES_STRESS STRESS von-Mises stress
TOPOL_DENSITY TOPOLOGY filtered topology density
HEAT_FLUX PRIMITIVE Heatflux
RES_TEMPERATURE RESIDUAL Residual of the temperature

CAdjFlowOutput

Used by: All adjoint flow solvers. Source: SU2_CFD/src/output/CAdjFlowOutput.cpp.

History fields (25)

Field Group Description
[” must not be split over multiple lines to ensure proper python parsing // clang-format off void CAdjFlowOutput::AddHistoryOutputFields_AdjScalarRMS_RES(const CConfig config) { if (!frozen_visc) { switch (TurbModelFamily(turb_model)) { case TURB_FAMILY::SA: /// DESCRIPTION: Root-mean square residual of the adjoint nu tilde. AddHistoryOutput(“RMS_ADJ_NU_TILDE”, “rms[A_nu]”, ScreenOutputFormat::FIXED, “RMS_RES”, “Root-mean square residual of the adjoint nu tilde.”, HistoryFieldType::RESIDUAL); break; case TURB_FAMILY::KW: /// DESCRIPTION: Root-mean square residual of the adjoint kinetic energy. AddHistoryOutput(“RMS_ADJ_TKE”, “rms[A_k]”, ScreenOutputFormat::FIXED, “RMS_RES”, “Root-mean square residual of the adjoint kinetic energy.”, HistoryFieldType::RESIDUAL); /// DESCRIPTION: Root-mean square residual of the adjoint dissipation. AddHistoryOutput(“RMS_ADJ_DISSIPATION”, “rms[A_w]”, ScreenOutputFormat::FIXED, “RMS_RES”, “Root-mean square residual of the adjoint dissipation.”, HistoryFieldType::RESIDUAL); break; case TURB_FAMILY::NONE: break; } } if (config->GetKind_Species_Model() == SPECIES_MODEL::SPECIES_TRANSPORT) { for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++) { AddHistoryOutput(“RMS_ADJ_SPECIES_” + std::to_string(iVar), “rms[A_rhoY_” + std::to_string(iVar) + “]”, ScreenOutputFormat::FIXED, “RMS_RES”, “Root-mean square residual of the adjoint transported species.”, HistoryFieldType::RESIDUAL); } } if (config->GetKind_Species_Model() == SPECIES_MODEL::FLAMELET) { const auto& flamelet_config_options = config->GetFlameletParsedOptions(); for (auto iCV=0u; iCV < flamelet_config_options.n_control_vars; iCV++) { const auto& cv_name = flamelet_config_options.controlling_variable_names[iCV]; AddHistoryOutput(“RMS_ADJ_“+cv_name, “rms[” + cv_name + “]”, ScreenOutputFormat::FIXED, “RMS_RES”, “Root-mean square residual of the adjoint “ + cv_name, HistoryFieldType::RESIDUAL); } for (unsigned short i_scalar = 0; i_scalar < flamelet_config_options.n_user_scalars; i_scalar++) { const auto& scalar_name = flamelet_config_options.user_scalar_names[i_scalar]; AddHistoryOutput(“RMS_ADJ_” + scalar_name, “rms[” + scalar_name + “]”, ScreenOutputFormat::FIXED, “RMS_RES”, “Root-mean square residual of the adjoint of “ + scalar_name + “ .”, HistoryFieldType::RESIDUAL); } } } void CAdjFlowOutput::AddHistoryOutputFields_AdjScalarMAX_RES(const CConfig config) { if (!frozen_visc) { switch (TurbModelFamily(turb_model)) { case TURB_FAMILY::SA: /// DESCRIPTION: Maximum residual of the adjoint nu tilde. AddHistoryOutput(“MAX_ADJ_NU_TILDE”, “max[A_nu]”, ScreenOutputFormat::FIXED, “MAX_RES”, “Maximum residual of the adjoint nu tilde.”, HistoryFieldType::RESIDUAL); break; case TURB_FAMILY::KW: /// DESCRIPTION: Maximum residual of the adjoint kinetic energy. AddHistoryOutput(“MAX_ADJ_TKE”, “max[A_k]”, ScreenOutputFormat::FIXED, “MAX_RES”, “Maximum residual of the adjoint kinetic energy.”, HistoryFieldType::RESIDUAL); /// DESCRIPTION: Maximum residual of the adjoint dissipation. AddHistoryOutput(“MAX_ADJ_DISSIPATION”, “max[A_w]”, ScreenOutputFormat::FIXED, “MAX_RES”, “Maximum residual of the adjoint dissipation.”, HistoryFieldType::RESIDUAL); break; case TURB_FAMILY::NONE: break; } } if (config->GetKind_Species_Model() == SPECIES_MODEL::SPECIES_TRANSPORT) { for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++) { AddHistoryOutput(“MAX_ADJ_SPECIES_” + std::to_string(iVar), “max[A_rhoY_” + std::to_string(iVar) + “]”,ScreenOutputFormat::FIXED, “MAX_RES”, “Maximum residual of the adjoint transported species.”, HistoryFieldType::RESIDUAL); } } if (config->GetKind_Species_Model() == SPECIES_MODEL::FLAMELET) { const auto& flamelet_config_options = config->GetFlameletParsedOptions(); for (auto iCV=0u; iCV < flamelet_config_options.n_control_vars; iCV++) { const auto& cv_name = flamelet_config_options.controlling_variable_names[iCV]; AddHistoryOutput(“MAX_ADJ_” + cv_name, “max[“+cv_name +”]”, ScreenOutputFormat::FIXED, “MAX_RES”, “Maximum residual of the adjoint “ + cv_name, HistoryFieldType::RESIDUAL); } for (unsigned short i_scalar = 0; i_scalar < flamelet_config_options.n_user_scalars; i_scalar++) { const auto& scalar_name = flamelet_config_options.user_scalar_names[i_scalar]; AddHistoryOutput(“MAX_ADJ_” + scalar_name, “max[scalar_” + scalar_name + “]”,ScreenOutputFormat::FIXED, “MAX_RES”, “Maximum residual of the adjoint of “ + scalar_name + “ .”, HistoryFieldType::RESIDUAL); } } } void CAdjFlowOutput::AddHistoryOutputFields_AdjScalarBGS_RES(const CConfig config) { if (!multiZone) return; if (!frozen_visc) { switch (TurbModelFamily(turb_model)) { case TURB_FAMILY::SA: /// DESCRIPTION: BGS residual of the adjoint nu tilde. AddHistoryOutput(“BGS_ADJ_NU_TILDE”, “bgs[A_nu]”, ScreenOutputFormat::FIXED, “BGS_RES”, “BGS residual of the adjoint nu tilde.”, HistoryFieldType::RESIDUAL); break; case TURB_FAMILY::KW: /// DESCRIPTION: BGS residual of the adjoint kinetic energy. AddHistoryOutput(“BGS_ADJ_TKE”, “bgs[A_k]”, ScreenOutputFormat::FIXED, “BGS_RES”, “BGS residual of the adjoint kinetic energy.”, HistoryFieldType::RESIDUAL); /// DESCRIPTION: BGS residual of the adjoint dissipation. AddHistoryOutput(“BGS_ADJ_DISSIPATION”, “bgs[A_w]”, ScreenOutputFormat::FIXED, “BGS_RES”, “BGS residual of the adjoint dissipation.”, HistoryFieldType::RESIDUAL); break; case TURB_FAMILY::NONE: break; } } if (config->GetKind_Species_Model() == SPECIES_MODEL::SPECIES_TRANSPORT) { for (unsigned short iVar = 0; iVar < config->GetnSpecies(); iVar++) { AddHistoryOutput(“BGS_ADJ_SPECIES_” + std::to_string(iVar), “bgsA_rhoY_” + std::to_string(iVar) + “]”, ScreenOutputFormat::FIXED, “BGS_RES”, “BGS residual of the adjoint transported species.”, HistoryFieldType::RESIDUAL); } } if (config->GetKind_Species_Model() == SPECIES_MODEL::FLAMELET) { const auto& flamelet_config_options = config->GetFlameletParsedOptions(); for (auto iCV=0u; iCV < flamelet_config_options.n_control_vars; iCV++) { const auto& cv_name = flamelet_config_options.controlling_variable_names[iCV]; AddHistoryOutput(“BGS_ADJ_” + cv_name BGS_RES no description
RMS_ADJ_NU_TILDE RMS_RES Root-mean square residual of the adjoint nu tilde.
RMS_ADJ_TKE RMS_RES Root-mean square residual of the adjoint kinetic energy.
RMS_ADJ_DISSIPATION RMS_RES Root-mean square residual of the adjoint dissipation.
“RMS_ADJ_SPECIES_” + std::to_string(iVar) RMS_RES Root-mean square residual of the adjoint transported species.
“RMS_ADJ_“+cv_name RMS_RES no description
“RMS_ADJ_” + scalar_name RMS_RES no description
MAX_ADJ_NU_TILDE MAX_RES Maximum residual of the adjoint nu tilde.
MAX_ADJ_TKE MAX_RES Maximum residual of the adjoint kinetic energy.
MAX_ADJ_DISSIPATION MAX_RES Maximum residual of the adjoint dissipation.
“MAX_ADJ_SPECIES_” + std::to_string(iVar) MAX_RES Maximum residual of the adjoint transported species.
“MAX_ADJ_” + cv_name MAX_RES no description
“MAX_ADJ_” + scalar_name MAX_RES no description
BGS_ADJ_NU_TILDE BGS_RES BGS residual of the adjoint nu tilde.
BGS_ADJ_TKE BGS_RES BGS residual of the adjoint kinetic energy.
BGS_ADJ_DISSIPATION BGS_RES BGS residual of the adjoint dissipation.
“BGS_ADJ_SPECIES_” + std::to_string(iVar) BGS_RES BGS residual of the adjoint transported species.
“BGS_ADJ_” + cv_name BGS_RES no description
“BGS_ADJ_” + scalar_name BGS_RES no description
LINSOL_ITER_TURB LINSOL Number of iterations of the linear solver for turbulence.
LINSOL_RESIDUAL_TURB LINSOL Residual of the linear solver for turbulence.
LINSOL_ITER_SPECIES LINSOL Number of iterations of the linear solver for species solver.
LINSOL_RESIDUAL_SPECIES LINSOL Residual of the linear solver for species solver.
LINSOL_ITER_FLAMELET LINSOL Number of iterations of the linear solver for scalar solver.
LINSOL_RESIDUAL_FLAMELET LINSOL Residual of the linear solver for scalar solver.

Volume fields (12)

Field Group Description
ADJ_NU_TILDE SOLUTION Adjoint Spalart-Allmaras variable
ADJ_TKE SOLUTION Adjoint turbulent kinetic energy
ADJ_DISSIPATION SOLUTION Adjoint rate of dissipation
“ADJ_SPECIES_” + std::to_string(iVar) SOLUTION Adjoint Species variable
“ADJ_” + cv_name SOLUTION no description
“ADJ_” + scalar_name SOLUTION no description
RES_ADJ_NU_TILDE RESIDUAL Residual of the adjoint Spalart-Allmaras variable
RES_ADJ_TKE RESIDUAL Residual of the adjoint turb. kinetic energy
RES_ADJ_DISSIPATION RESIDUAL Residual of adjoint rate of dissipation
“RES_ADJ_SPECIES_” + std::to_string(iVar) RESIDUAL Residual of the adjoint Species variable
“RES_ADJ_” + cv_name RESIDUAL no description
“RES_ADJ_” + scalar_name RESIDUAL no description

CAdjFlowCompOutput

Used by: Compressible adjoint. Source: SU2_CFD/src/output/CAdjFlowCompOutput.cpp.

History fields (24)

Field Group Description
RMS_ADJ_DENSITY RMS_RES Root-mean square residual of the adjoint density.
RMS_ADJ_MOMENTUM-X RMS_RES Root-mean square residual of the adjoint momentum x-component.
RMS_ADJ_MOMENTUM-Y RMS_RES Root-mean square residual of the adjoint momentum y-component.
RMS_ADJ_MOMENTUM-Z RMS_RES Root-mean square residual of the adjoint momentum z-component.
RMS_ADJ_ENERGY RMS_RES Root-mean square residual of the adjoint energy.
MAX_ADJ_DENSITY MAX_RES Maximum residual of the adjoint density.
MAX_ADJ_MOMENTUM-X MAX_RES Maximum residual of the adjoint momentum x-component
MAX_ADJ_MOMENTUM-Y MAX_RES Maximum residual of the adjoint momentum y-component
MAX_ADJ_MOMENTUM-Z MAX_RES Maximum residual of the adjoint momentum z-component
MAX_ADJ_ENERGY MAX_RES Maximum residual of the adjoint energy.
BGS_ADJ_DENSITY BGS_RES BGS residual of the adjoint density.
BGS_ADJ_MOMENTUM-X BGS_RES BGS residual of the adjoint momentum x-component
BGS_ADJ_MOMENTUM-Y BGS_RES BGS residual of the adjoint momentum y-component
BGS_ADJ_MOMENTUM-Z BGS_RES BGS residual of the adjoint momentum z-component
BGS_ADJ_ENERGY BGS_RES BGS residual of the adjoint energy.
SENS_GEO SENSITIVITY Sum of the geometrical sensitivities on all markers set in MARKER_MONITORING.
SENS_AOA SENSITIVITY Sensitivity of the objective function with respect to the angle of attack (only for compressible solver).
SENS_MACH SENSITIVITY Sensitivity of the objective function with respect to the Mach number (only of compressible solver).
SENS_PRESS SENSITIVITY Sensitivity of the objective function with respect to the far-field pressure.
SENS_TEMP SENSITIVITY Sensitivity of the objective function with respect to the far-field temperature.
LINSOL_ITER LINSOL Number of iterations of the linear solver.
LINSOL_RESIDUAL LINSOL Residual of the linear solver.
DEFORM_ITER DEFORM Linear solver iterations for the mesh deformation
DEFORM_RESIDUAL DEFORM Residual of the linear solver for the mesh deformation

Volume fields (17)

Field Group Description
COORD-X COORDINATES x-component of the coordinate vector
COORD-Y COORDINATES y-component of the coordinate vector
COORD-Z COORDINATES z-component of the coordinate vector
ADJ_DENSITY SOLUTION Adjoint density
ADJ_MOMENTUM-X SOLUTION x-component of the adjoint momentum vector
ADJ_MOMENTUM-Y SOLUTION y-component of the adjoint momentum vector
ADJ_MOMENTUM-Z SOLUTION z-component of the adjoint momentum vector
ADJ_ENERGY SOLUTION Adjoint energy
RES_ADJ_DENSITY RESIDUAL Residual of the adjoint density
RES_ADJ_MOMENTUM-X RESIDUAL Residual of the adjoint x-momentum
RES_ADJ_MOMENTUM-Y RESIDUAL Residual of the adjoint y-momentum
RES_ADJ_MOMENTUM-Z RESIDUAL Residual of the adjoint z-momentum
RES_ADJ_ENERGY RESIDUAL Residual of the adjoint energy
SENSITIVITY-X SENSITIVITY x-component of the sensitivity vector
SENSITIVITY-Y SENSITIVITY y-component of the sensitivity vector
SENSITIVITY-Z SENSITIVITY z-component of the sensitivity vector
SENSITIVITY SENSITIVITY sensitivity in normal direction

CAdjFlowIncOutput

Used by: Incompressible adjoint. Source: SU2_CFD/src/output/CAdjFlowIncOutput.cpp.

History fields (30)

Field Group Description
RMS_ADJ_PRESSURE RMS_RES Root-mean square residual of the adjoint Pressure.
RMS_ADJ_VELOCITY-X RMS_RES Root-mean square residual of the adjoint Velocity x-component.
RMS_ADJ_VELOCITY-Y RMS_RES Root-mean square residual of the adjoint Velocity y-component.
RMS_ADJ_VELOCITY-Z RMS_RES Root-mean square residual of the adjoint Velocity z-component.
RMS_ADJ_TEMPERATURE RMS_RES Root-mean square residual of the adjoint temperature.
RMS_ADJ_ENTHALPY RMS_RES Root-mean square residual of the enthalpy.
ADJOINT_SOLEXTRA ADJOINT_SOLEXTRA Adjoint value of the first extra Solution.
RMS_ADJ_RAD_ENERGY RMS_RES Root-mean square residual of the P1 radiative energy.
MAX_ADJ_PRESSURE MAX_RES Maximum residual of the adjoint Pressure.
MAX_ADJ_VELOCITY-X MAX_RES Maximum residual of the adjoint Velocity x-component
MAX_ADJ_VELOCITY-Y MAX_RES Maximum residual of the adjoint Velocity y-component
MAX_ADJ_VELOCITY-Z MAX_RES Maximum residual of the adjoint Velocity z-component
MAX_ADJ_TEMPERATURE MAX_RES Maximum residual of the temperature.
MAX_ADJ_ENTHALPY MAX_RES Maximum residual of the enthalpy.
BGS_ADJ_PRESSURE BGS_RES BGS residual of the adjoint Pressure.
BGS_ADJ_VELOCITY-X BGS_RES BGS residual of the adjoint Velocity x-component
BGS_ADJ_VELOCITY-Y BGS_RES BGS residual of the adjoint Velocity y-component
BGS_ADJ_VELOCITY-Z BGS_RES BGS residual of the adjoint Velocity z-component
BGS_ADJ_TEMPERATURE BGS_RES BGS residual of the adjoint temperature.
BGS_ADJ_ENTHALPY BGS_RES BGS residual of the adjoint enthalpy.
BGS_ADJ_RAD_ENERGY BGS_RES BGS residual of the P1 radiative energy.
SENS_GEO SENSITIVITY Sum of the geometrical sensitivities on all markers set in MARKER_MONITORING.
SENS_PRESS SENSITIVITY Sensitivity of the objective function with respect to the far-field pressure.
SENS_TEMP SENSITIVITY Sensitivity of the objective function with respect to the far-field temperature.
SENS_VEL_IN SENSITIVITY Sensitivity of the objective function with respect to the inlet velocity.
SENS_PRESS_OUT SENSITIVITY Sensitivity of the objective function with respect to the outlet pressure.
LINSOL_ITER LINSOL Number of iterations of the linear solver.
LINSOL_RESIDUAL LINSOL Residual of the linear solver.
DEFORM_ITER DEFORM Linear solver iterations for the mesh deformation
DEFORM_RESIDUAL DEFORM Residual of the linear solver for the mesh deformation

Volume fields (24)

Field Group Description
COORD-X COORDINATES x-component of the coordinate vector
COORD-Y COORDINATES y-component of the coordinate vector
COORD-Z COORDINATES z-component of the coordinate vector
ADJ_PRESSURE SOLUTION Adjoint pressure
ADJ_VELOCITY-X SOLUTION x-component of the adjoint velocity vector
ADJ_VELOCITY-Y SOLUTION y-component of the adjoint velocity vector
ADJ_VELOCITY-Z SOLUTION z-component of the adjoint velocity vector
ADJ_TEMPERATURE SOLUTION Adjoint temperature
ADJ_ENTHALPY SOLUTION Adjoint_Enthalpy
ADJ_P1_ENERGY SOLUTION Adjoint radiative energy
GRID_VELOCITY-X GRID_VELOCITY x-component of the grid velocity vector
GRID_VELOCITY-Y GRID_VELOCITY y-component of the grid velocity vector
GRID_VELOCITY-Z GRID_VELOCITY z-component of the grid velocity vector
RES_ADJ_PRESSURE RESIDUAL Residual of the adjoint pressure
RES_ADJ_VELOCITY-X RESIDUAL Residual of the adjoint x-velocity
RES_ADJ_VELOCITY-Y RESIDUAL Residual of the adjoint y-velocity
RES_ADJ_VELOCITY-Z RESIDUAL Residual of the adjoint z-velocity
RES_ADJ_TEMPERATURE RESIDUAL Residual of the adjoint temperature
RES_ADJ_ENTHALPY RESIDUAL Residual of the adjoint enthalpy
RES_P1_ENERGY RESIDUAL Residual of adjoint radiative energy
SENSITIVITY-X SENSITIVITY x-component of the sensitivity vector
SENSITIVITY-Y SENSITIVITY y-component of the sensitivity vector
SENSITIVITY-Z SENSITIVITY z-component of the sensitivity vector
SENSITIVITY SENSITIVITY sensitivity in normal direction

CAdjHeatOutput

Used by: Heat adjoint. Source: SU2_CFD/src/output/CAdjHeatOutput.cpp.

History fields (8)

Field Group Description
RMS_ADJ_TEMPERATURE RMS_RES Root-mean square residual of the adjoint temperature.
MAX_ADJ_TEMPERATURE MAX_RES Maximum residual of the adjoint temperature.
BGS_ADJ_TEMPERATURE BGS_RES BGS residual of the adjoint temperature.
SENS_GEO SENSITIVITY Sum of the geometrical sensitivities on all markers set in MARKER_MONITORING.
LINSOL_ITER LINSOL Number of iterations of the linear solver.
LINSOL_RESIDUAL LINSOL Residual of the linear solver.
DEFORM_ITER DEFORM Linear solver iterations for the mesh deformation
DEFORM_RESIDUAL DEFORM Residual of the linear solver for the mesh deformation

Volume fields (11)

Field Group Description
COORD-X COORDINATES x-component of the coordinate vector
COORD-Y COORDINATES y-component of the coordinate vector
COORD-Z COORDINATES z-component of the coordinate vector
ADJ_TEMPERATURE SOLUTION Adjoint Temperature
RES_ADJ_TEMPERATURE RESIDUAL Residual of the Adjoint Temperature
SENSITIVITY-X SENSITIVITY x-component of the sensitivity vector
SENSITIVITY-Y SENSITIVITY y-component of the sensitivity vector
SENSITIVITY-Z SENSITIVITY z-component of the sensitivity vector
SENSITIVITY SENSITIVITY sensitivity in normal direction
SENS_TEMP_N SENSITIVITY_N sensitivity to the previous temperature
SENS_TEMP_N1 SENSITIVITY_N sensitivity to the previous-1 temperature

CAdjElasticityOutput

Used by: Structural adjoint. Source: SU2_CFD/src/output/CAdjElasticityOutput.cpp.

History fields (15)

Field Group Description
ADJOINT_DISP_X RMS_RES Root-mean square residual of the adjoint of the X displacements.
ADJOINT_DISP_Y RMS_RES Root-mean square residual of the adjoint of the Y displacements.
ADJOINT_DISP_Z RMS_RES Root-mean square residual of the adjoint of the Z displacements.
“SENS_E_” + iVarS SENSITIVITY d Objective / d Elasticity modulus
“SENS_NU_” + iVarS SENSITIVITY d Objective / d Poisson ratio
“SENS_RHO_” + iVarS SENSITIVITY d Objective / d Material density
“SENS_RHO_DL_” + iVarS SENSITIVITY d Objective / d Dead load density
“SENS_EFIELD_” + iVarS SENSITIVITY d Objective / d Electric field
LINSOL_ITER LINSOL Number of iterations of the linear solver.
LINSOL_RESIDUAL LINSOL Residual of the linear solver.
BGS_ADJ_DISP_X BGS_RES BGS residual of the adjoint X displacement.
BGS_ADJ_DISP_Y BGS_RES BGS residual of the adjoint Y displacement.
BGS_ADJ_DISP_Z BGS_RES BGS residual of the adjoint Z displacement.
LINSOL_ITER_HEAT LINSOL Number of iterations of the linear solver.
LINSOL_RESIDUAL_HEAT LINSOL Residual of the linear solver.

Volume fields (21)

Field Group Description
COORD-X COORDINATES x-component of the coordinate vector
COORD-Y COORDINATES y-component of the coordinate vector
COORD-Z COORDINATES z-component of the coordinate vector
ADJOINT-X SOLUTION adjoint of displacement in the x direction
ADJOINT-Y SOLUTION adjoint of displacement in the y direction
ADJOINT-Z SOLUTION adjoint of displacement in the z direction
ADJ_TEMPERATURE SOLUTION Adjoint Temperature
SENSITIVITY-X SENSITIVITY geometric sensitivity in the x direction
SENSITIVITY-Y SENSITIVITY geometric sensitivity in the y direction
SENSITIVITY-Z SENSITIVITY geometric sensitivity in the z direction
SENS_DISP-X SENSITIVITY_N sensitivity to the previous x displacement
SENS_DISP-Y SENSITIVITY_N sensitivity to the previous y displacement
SENS_DISP-Z SENSITIVITY_N sensitivity to the previous z displacement
SENS_VEL-X SENSITIVITY_N sensitivity to the previous x velocity
SENS_VEL-Y SENSITIVITY_N sensitivity to the previous y velocity
SENS_VEL-Z SENSITIVITY_N sensitivity to the previous z velocity
SENS_ACCEL-X SENSITIVITY_N sensitivity to the previous x acceleration
SENS_ACCEL-Y SENSITIVITY_N sensitivity to the previous y acceleration
SENS_ACCEL-Z SENSITIVITY_N sensitivity to the previous z acceleration
SENS_TEMP_N SENSITIVITY_N sensitivity to the previous temperature
SENS_TEMP_N1 SENSITIVITY_N sensitivity to the previous-1 temperature

CMultizoneOutput

Used by: Multizone problems. Source: SU2_CFD/src/output/CMultizoneOutput.cpp.

History fields (2)

Field Group Description
name   no description
COMBO COMBO Combined obj. function value.

History, per surface fields (1)

Field Group Description
name   no description

CMeshOutput

Used by: Mesh conversion (SU2_DEF, SU2_SOL). Source: SU2_CFD/src/output/CMeshOutput.cpp.

Volume fields (6)

Field Group Description
COORD-X COORDINATES x-component of the coordinate vector
COORD-Y COORDINATES y-component of the coordinate vector
COORD-Z COORDINATES z-component of the coordinate vector
ORTHOGONALITY MESH_QUALITY Orthogonality Angle (deg.)
ASPECT_RATIO MESH_QUALITY CV Face Area Aspect Ratio
VOLUME_RATIO MESH_QUALITY CV Sub-Volume Ratio

CBaselineOutput

Used by: Solution conversion (SU2_SOL). Source: SU2_CFD/src/output/CBaselineOutput.cpp.

Volume fields (4)

Field Group Description
fields[0] COORDINATES x-component of the coordinate vector
fields[1] COORDINATES y-component of the coordinate vector
fields[2] COORDINATES z-component of the coordinate vector
fields[iField] SOLUTION no description


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