Error Messages

This page lists the 860 error messages that can stop SU2 in commit 6b54b78464 (the SU2_MPI::Error calls in the code). Use the search of your browser (Ctrl+F) with a few words of the message you see. Parts of a message that SU2 fills in at run time are shown as “…”.

Each message links to the code that prints it, and to the options it names.

See also: Renamed and Removed Options.

Configuration checks (180)

Message Options Code
There is no geometry file called   CConfig.cpp:606
Error while reading the file   CConfig.cpp:615
The file … is not a valid SU2 binary file   CConfig.cpp:625
Failed to jump forward in the file   CConfig.cpp:632
Error while reading the file   CConfig.cpp:640
There is no geometry file called   CConfig.cpp:664
was not found or is not a properly formatted CGNS file. … Note that SU2 expects unstructured CGNS files in ADF data format.   CConfig.cpp:712
CGNS reader currently incapable of handling more than 1 database.   CConfig.cpp:734
SU2 built without CGNS support. … To use CGNS, build SU2 accordingly.   CConfig.cpp:759
The SU2 mesh file named … was not found.   CConfig.cpp:794
is not an SU2 mesh file or has the wrong format (‘NDIME=’ not found). Please check.   CConfig.cpp:820
was not found or is not a properly formatted CGNS file. … Note that SU2 expects unstructured CGNS files in ADF data format.   CConfig.cpp:846
CGNS reader currently incapable of handling more than 1 database.   CConfig.cpp:865
SU2 built without CGNS support. … To use CGNS, build SU2 accordingly.   CConfig.cpp:877
The configuration file (.cfg) is missing!!   CConfig.cpp:3278
CONFIG_LIST must be provided if PHYSICAL_PROBLEM=MULTIPHYSICS CONFIG_LIST CConfig.cpp:3621
Number of markers in MARKER_ZONE_INTERFACE must be a multiple of 2 MARKER_ZONE_INTERFACE CConfig.cpp:3630
Number of CONFIG_LIST must match number of zones in mesh file. CONFIG_LIST CConfig.cpp:3642
Config file … defined in CONFIG_FILES does not exist   CConfig.cpp:3661
Tecplot binary file requested in option OUTPUT_FILES but SU2 was built without TecIO support. OUTPUT_FILES CConfig.cpp:3757
CGNS file requested in option OUTPUT_FILES but SU2 was built without CGNS support. OUTPUT_FILES CConfig.cpp:3767
CoolProp can not be used with non-dimensionalization.   CConfig.cpp:3774
OUTPUT_FILES: ‘STL_BINARY’ output not implemented. Use ‘STL’ for ASCII output. OUTPUT_FILES CConfig.cpp:3780
OUTPUT_FILES: ‘STL(_BINARY)’ output only reasonable for 3D cases. OUTPUT_FILES CConfig.cpp:3783
KIND_TURB_MODEL must be NONE if SOLVER= NAVIER_STOKES KIND_TURB_MODEL, SOLVER CConfig.cpp:3804
KIND_TURB_MODEL must be NONE if SOLVER= INC_NAVIER_STOKES KIND_TURB_MODEL, SOLVER CConfig.cpp:3807
A turbulence model must be specified with KIND_TURB_MODEL if SOLVER= RANS KIND_TURB_MODEL, SOLVER CConfig.cpp:3810
A turbulence model must be specified with KIND_TURB_MODEL if SOLVER= INC_RANS KIND_TURB_MODEL, SOLVER CConfig.cpp:3813
KIND_TURB_MODEL cannot be NONE to use a transition model KIND_TURB_MODEL CConfig.cpp:3816
Euler solvers are only compatible with slip walls (MARKER_EULER) MARKER_EULER CConfig.cpp:3825
COMPRESSIBILITY-SARKAR only supported for SOLVER= RANS SOLVER CConfig.cpp:3840
COMPRESSIBILITY-WILCOX only supported for SOLVER= RANS SOLVER CConfig.cpp:3844
LM2015 is available only for 3D problems   CConfig.cpp:3853
For RANS problems, use NONE, STANDARD_WALL_FUNCTION or EQUILIBRIUM_WALL_MODEL.   CConfig.cpp:3869
Wall model STANDARD_FUNCTION only available for RANS or INC_RANS.   CConfig.cpp:3873
Wall model STANDARD_FUNCTION and WALL_ROUGHNESS migh not be compatible. Checking required! WALL_ROUGHNESS CConfig.cpp:3875
Fixed CL mode not implemented for the incompressible solver.   CConfig.cpp:3912
You probably want to set INC_ENERGY_EQUATION= YES for the fluid solver. INC_ENERGY_EQUATION CConfig.cpp:3917
Number of CHT interfaces does not match number of contact resistances.   CConfig.cpp:3931
Contact resistance value should be positive.   CConfig.cpp:3935
Centered schemes are not available for scalar transport   CConfig.cpp:3954
Centered schemes do not use MUSCL reconstruction (use MUSCL_FLOW= NO). MUSCL_FLOW CConfig.cpp:3964
Centered schemes do not use MUSCL reconstruction (use MUSCL_ADJFLOW= NO). MUSCL_ADJFLOW CConfig.cpp:3971
Marker lists supplied to MARKER_ACTDISK_BEM_CG and MARKER_ACTDISK_BEM_AXIS must be identical. MARKER_ACTDISK_BEM_AXIS, MARKER_ACTDISK_BEM_CG CConfig.cpp:3990
Marker lists supplied to MARKER_ACTDISK_BEM_CG and MARKER_ACTDISK_BEM_AXIS must be identical. MARKER_ACTDISK_BEM_AXIS, MARKER_ACTDISK_BEM_CG CConfig.cpp:3994
Marker lists supplied to MARKER_ACTDISK_BEM_CG and MARKER_ACTDISK_BEM_AXIS must be identical. MARKER_ACTDISK_BEM_AXIS, MARKER_ACTDISK_BEM_CG CConfig.cpp:4001
Marker lists supplied to MARKER_ACTDISK_BEM_CG and MARKER_ACTDISK_BEM_AXIS must be identical. MARKER_ACTDISK_BEM_AXIS, MARKER_ACTDISK_BEM_CG CConfig.cpp:4005
The following objectives can only be used for the first surface in a multi-objective … problem or as a single objective applied to multiple monitoring markers:   CConfig.cpp:4100
The expression for the custom objective function was not set.   CConfig.cpp:4117
TIME_DOMAIN must be set to YES if TIME_MARCHING is TIME_DOMAIN, TIME_MARCHING CConfig.cpp:4127
TIME_ITER must be larger than RESTART_ITER. RESTART_ITER, TIME_ITER CConfig.cpp:4143
WINDOW_START_ITER must be larger than or equal to: RESTART_ITER! RESTART_ITER, WINDOW_START_ITER CConfig.cpp:4149
Invalid value for TIME_STEP. TIME_STEP CConfig.cpp:4157
Appending iterations to the filename (WRT_RESTART_OVERWRITE=NO) is incompatible with transient problems. WRT_RESTART_OVERWRITE CConfig.cpp:4170
Appending iterations to the filename (WRT_SURFACE_OVERWRITE=NO) is incompatible with transient problems. WRT_SURFACE_OVERWRITE CConfig.cpp:4173
Appending iterations to the filename (WRT_VOLUME_OVERWRITE=NO) is incompatible with transient problems. WRT_VOLUME_OVERWRITE CConfig.cpp:4176
LINEAR_SOLVER_ILU_GPU_SWEEPS must be at least 1; 0 sweeps never factorizes the preconditioner. LINEAR_SOLVER_ILU_GPU_SWEEPS CConfig.cpp:4228
Harmonic Balance not yet implemented for the incompressible solver.   CConfig.cpp:4237
KIND_INCOMP_SYSTEM= PRESSURE_BASED does not support MGLEVEL > 0, … the Poisson solver is single-grid only. KIND_INCOMP_SYSTEM, MGLEVEL CConfig.cpp:4249
KIND_INCOMP_SYSTEM= PRESSURE_BASED has no adjoint formulation. KIND_INCOMP_SYSTEM CConfig.cpp:4253
KIND_INCOMP_SYSTEM= PRESSURE_BASED does not support MARKER_PERIODIC. KIND_INCOMP_SYSTEM, MARKER_PERIODIC CConfig.cpp:4256
KIND_INCOMP_SYSTEM= PRESSURE_BASED does not support streamwise periodicity. KIND_INCOMP_SYSTEM CConfig.cpp:4259
KIND_PB_ITER= SIMPLEC requires TRANSIENT_TERM_REMOVAL_FACTOR= 0. KIND_PB_ITER, TRANSIENT_TERM_REMOVAL_FACTOR CConfig.cpp:4271
The use of FLUID_MIXTURE requires the INC_DENSITY_MODEL option to be VARIABLE INC_DENSITY_MODEL CConfig.cpp:4337
The use of FLUID_MIXTURE requires the KIND_SCALAR_MODEL option to be SPECIES_TRANSPORT KIND_SCALAR_MODEL CConfig.cpp:4344
Fluid mixture: viscosity model not available.   CConfig.cpp:4368
The use of FLUID_MIXTURE requires the number of entries for THERMAL_CONDUCTIVITY_CONSTANT and THERMAL_CONDUCTIVITY_CONSTANT CConfig.cpp:4377
Conductivity model not available.   CConfig.cpp:4410
The use of SCALAR_MODEL= FLAMELET requires the FLUID_MODEL option to be FLUID_FLAMELET FLUID_MODEL CConfig.cpp:4419
The use of FLUID_FLAMELET requires the INC_DENSITY_MODEL option to be VARIABLE or FLAMELET INC_DENSITY_MODEL CConfig.cpp:4424
The use of FLUID_FLAMELET requires the CONDUCTIVITY_MODEL option to be FLAMELET CONDUCTIVITY_MODEL CConfig.cpp:4429
The use of FLUID_FLAMELET requires the DIFFUSIVITY_MODEL option to be FLAMELET DIFFUSIVITY_MODEL CConfig.cpp:4434
The use of FLUID_FLAMELET requires the VISCOSITY_MODEL option to be FLAMELET VISCOSITY_MODEL CConfig.cpp:4439
The use of FLUID_FLAMELET is incompatible with WEAKLY_COUPLED_HEAT in the same zone.   CConfig.cpp:4444
Only STANDARD_AIR fluid model can be used with US Measurement System   CConfig.cpp:4452
A turbulence model is not yet available for the NEMO solver.   CConfig.cpp:4457
Only Gupta-Yos transport model available for ionized flows using SU2TCLIB.   CConfig.cpp:4466
Catalytic wall recombination is not yet available for ionized flows in SU2_NEMO.   CConfig.cpp:4476
Giles Boundary conditions can only be used with turbomachinery markers   CConfig.cpp:4493
Insufficient TURBO_PERF_KIND options specified with turbomachinery markers TURBO_PERF_KIND CConfig.cpp:4498
Riemann Boundary conditions or Giles must be used for inlet and outlet with Not Ideal Compressible … Fluids   CConfig.cpp:4505
Riemann Boundary conditions or Giles must be used outlet with Not Ideal Compressible Fluids   CConfig.cpp:4511
Riemann Boundary conditions or Giles must be used outlet with Not Ideal Compressible Fluids   CConfig.cpp:4516
Only SUTHERLAND viscosity model can be used with US Measurement   CConfig.cpp:4527
Reynolds number required for NAVIER_STOKES and RANS !!   CConfig.cpp:4534
Number of SURFACE_MOVEMENT must match number of MARKER_MOVING MARKER_MOVING, SURFACE_MOVEMENT CConfig.cpp:4539
ITER must not be used when running multizone and/or unsteady problems. ITER CConfig.cpp:4561
Unsupported kind of grid movement for steady state problems.   CConfig.cpp:4577
Unsupported kind of surface movement for steady state problems.   CConfig.cpp:4581
Number of MOVE_MOTION_ORIGIN must match number of MARKER_MOVING. MARKER_MOVING, MOVE_MOTION_ORIGIN CConfig.cpp:4673
Not a valid value for time period!!   CConfig.cpp:4682
Length of omega_HB must match the number TIME_INSTANCES!! TIME_INSTANCES CConfig.cpp:4691
RAMP_MUSCL_POWER cannot be less than or equal to zero! RAMP_MUSCL_POWER CConfig.cpp:4783
ERROR: Length of REF_ORIGIN_MOMENT_X must match number of Monitoring Markers!! REF_ORIGIN_MOMENT_X CConfig.cpp:4874
ERROR: Length of REF_ORIGIN_MOMENT_Y must match number of Monitoring Markers!! REF_ORIGIN_MOMENT_Y CConfig.cpp:4894
ERROR: Length of REF_ORIGIN_MOMENT_Z must match number of Monitoring Markers!! REF_ORIGIN_MOMENT_Z CConfig.cpp:4914
ERROR: Please specify non-zero UPDATE_AOA_ITER_LIMIT. UPDATE_AOA_ITER_LIMIT CConfig.cpp:5070
ALIGNED_BYTES_MATMUL must be a multiple of 64. ALIGNED_BYTES_MATMUL CConfig.cpp:5086
ERROR: Unsteady CFL not specified for time accurate local time stepping.   CConfig.cpp:5121
PHYSICAL_PROBLEM must be set in the configuration file   CConfig.cpp:5210
SU2_CFD: Config option DIRECT_DIFF= YES requires AD support. … Please use SU2_CFD_DIRECTDIFF (meson.py … -Denable-directdiff=true …). DIRECT_DIFF CConfig.cpp:5300
Config option AUTO_DIFF= YES requires AD support. … Please use SU2_???_AD (meson.py … -Denable-autodiff=true …). AUTO_DIFF CConfig.cpp:5335
Inviscid incompressible problems must be constant density (no energy eqn.). Use DENSITY_MODEL= CONSTANT and ENERGY_EQUATION= NO.   CConfig.cpp:5381
Body force and Boussinesq source terms are not currently compatible.   CConfig.cpp:5399
Variable density incompressible solver limited to ideal gases. Check the fluid model options (use INC_IDEAL_GAS, INC_IDEAL_GAS_POLY).   CConfig.cpp:5405
CONSTANT_DENSITY fluid model can only be used with INIT_OPTION_INC= DENSITY_INIT. INIT_OPTION_INC CConfig.cpp:5418
Fluid model not compatible with compressible flows. CONSTANT_DENSITY/INC_IDEAL_GAS/INC_IDEAL_GAS_POLY are for incompressible only.   CConfig.cpp:5423
Vorticity confinement feature currently not supported for incompressible or non-equilibrium model or axisymmetric flows.   CConfig.cpp:5444
Actuator disk BEM method for propellers feature currently not supported for incompressible or non-equilibrium model or axisymmetric flows.   CConfig.cpp:5456
POLYNOMIAL_VISCOSITY and POLYNOMIAL_CONDUCTIVITY are for incompressible only currently.   CConfig.cpp:5463
Data-driven fluid model can only be used for compressible flows.   CConfig.cpp:5469
CP_POLYCOEFFS not set for fluid model INC_IDEAL_GAS_POLY. CP_POLYCOEFFS CConfig.cpp:5478
MU_POLYCOEFFS not set for viscosity model POLYNOMIAL_VISCOSITY. MU_POLYCOEFFS CConfig.cpp:5487
KT_POLYCOEFFS not set for conductivity model POLYNOMIAL_CONDUCTIVITY. KT_POLYCOEFFS CConfig.cpp:5496
Must use SI units for incompressible solver.   CConfig.cpp:5502
Undefined incompressible inlet type. VELOCITY_INLET or PRESSURE_INLET possible.   CConfig.cpp:5521
Undefined incompressible outlet type. PRESSURE_OUTLET or MASS_FLOW_OUTLET possible.   CConfig.cpp:5534
Must list the first two markers for the pressure drop objective function. Expected format: MARKER_ANALYZE= (outlet_name, inlet_name, …). MARKER_ANALYZE CConfig.cpp:5544
Streamwise Periodic Flow currently only implemented for incompressible flow.   CConfig.cpp:5551
Streamwise Periodic Flow + Incompressible Euler: Not tested yet.   CConfig.cpp:5553
A MARKER_PERIODIC pair has to be set with KIND_STREAMWISE_PERIODIC != NONE. KIND_STREAMWISE_PERIODIC, MARKER_PERIODIC CConfig.cpp:5555
Streamwise Periodicity terms does not not have axisymmetric corrections.   CConfig.cpp:5561
Marker … is not a viscous wall.   CConfig.cpp:5583
Different number of topology filter kernels and respective parameters.   CConfig.cpp:5613
Different number of topology filter kernels and respective radii.   CConfig.cpp:5632
COMM_LEVEL = NONE not yet implemented. COMM_LEVEL CConfig.cpp:5652
MESH_BOX_SIZE specified without 3 values. MESH_BOX_SIZE CConfig.cpp:5675
SU2_CFD: Config option MATH_PROBLEM= DISCRETE_ADJOINT requires AD support! … Please use SU2_CFD_AD (configuration/compilation is done using the preconfigure.py script). MATH_PROBLEM CConfig.cpp:5692
Invalid iteration number requested for unsteady adjoint. … Make sure EXT_ITER is larger or equal than UNST_ADJOINT_ITER. UNST_ADJOINT_ITER CConfig.cpp:5707
MUSCL_ADJTURB= YES not currently supported. Please select MUSCL_ADJTURB= NO (first-order). MUSCL_ADJTURB CConfig.cpp:5764
MUSCL_KAPPA_FLOW should be in range [-1.0, 1.0]. MUSCL_KAPPA_FLOW CConfig.cpp:5770
MUSCL_KAPPA_TURB should be in range [-1.0, 1.0]. MUSCL_KAPPA_TURB CConfig.cpp:5773
MUSCL_KAPPA_HEAT should be in range [-1.0, 1.0]. MUSCL_KAPPA_HEAT CConfig.cpp:5776
MUSCL_KAPPA_ADJFLOW should be in range [-1.0, 1.0]. MUSCL_KAPPA_ADJFLOW CConfig.cpp:5779
MUSCL_KAPPA_SPECIES should be in range [-1.0, 1.0]. MUSCL_KAPPA_SPECIES CConfig.cpp:5782
For centered schemes the option NUM_METHOD_GRAD_RECON should not be set. NUM_METHOD_GRAD_RECON CConfig.cpp:5810
LEAST_SQUARES gradient method not allowed for viscous / source terms. … Please select either WEIGHTED_LEAST_SQUARES or GREEN_GAUSS.   CConfig.cpp:5823
CFL adaption only available for finite-volume fluid solvers. … Please select CFL_ADAPT = NO. CFL_ADAPT CConfig.cpp:5832
CFL adaption not available for TIME_STEPPING integration. … Please select CFL_ADAPT = NO. CFL_ADAPT CConfig.cpp:5838
CFL adaption factor down should be less than 1.0.   CConfig.cpp:5846
CFL adaption factor up should be greater than 1.0.   CConfig.cpp:5850
CFL adaption minimum CFL is larger than the maximum CFL.   CConfig.cpp:5854
The use of MARKER_INLET_TURBULENT requires the number of entries when SST Model is used … to be equal to 2 : Turbulent intensity and ratio turbulent to laminar viscosity MARKER_INLET_TURBULENT CConfig.cpp:5878
The use of MARKER_INLET_TURBULENT requires the number of entries when SA Model is used … to be equal to 1 : ratio turbulent to laminar viscosity MARKER_INLET_TURBULENT CConfig.cpp:5883
Species transport currently only available for compressible and incompressible flow.   CConfig.cpp:5899
Dual-time stepping with species-dependent variable density does not support MGLEVEL > 0. MGLEVEL CConfig.cpp:5906
SURFACE_SPECIES_0 and SURFACE_SPECIES_VARIANCE currently can only handle one entry to MARKER_ANALYZE. MARKER_ANALYZE CConfig.cpp:5914
SPECIES_CLIPPING= YES requires the options SPECIES_CLIPPING_MIN/MAX to set the clipping values. SPECIES_CLIPPING, SPECIES_CLIPPING_MIN CConfig.cpp:5926
A DIFFUSIVITY_CONSTANT= has to be set with DIFFUSIVITY_MODEL= CONSTANT_DIFFUSIVITY. DIFFUSIVITY_CONSTANT, DIFFUSIVITY_MODEL CConfig.cpp:5931
Make sure all species inputs have the same size.   CConfig.cpp:5963
Number of initial species incompatible with number of controlling variables and user scalars.   CConfig.cpp:5994
FLAME_INIT_METHOD= SPARK requires SPARK_INIT to be defined in the config file. FLAME_INIT_METHOD, SPARK_INIT CConfig.cpp:6002
FLAME_INIT_METHOD= SPARK requires SPARK_REACTION_RATES to be defined in the config file. FLAME_INIT_METHOD, SPARK_REACTION_RATES CConfig.cpp:6006
SPARK_REACTION_RATES must have at least SPARK_REACTION_RATES CConfig.cpp:6009
Flame ignition temperature must be higher than the initial temperature of the flow field.   CConfig.cpp:6015
DV_MARKER contains marker names that do not exist in the lists of BCs in the config file. DV_MARKER CConfig.cpp:6533
No turbulence model has been selected but LM transition model is active.   CConfig.cpp:6728
Stochastic Backscatter Model available for 3D flow simulations only.   CConfig.cpp:6747
Backscatter intensity coefficient must be non-negative.   CConfig.cpp:6750
Backscatter lengthscale coefficient must be non-negative.   CConfig.cpp:6759
Stochastic Backscatter can only be activated with Hybrid RANS/LES.   CConfig.cpp:6788
ENFORCE_LES can only be activated with Hybrid RANS/LES. ENFORCE_LES CConfig.cpp:6791
Subgrid Scale model not specified.   CConfig.cpp:6820
No valid solver was chosen   CConfig.cpp:6853
Unknown or invalid limiter type.   CConfig.cpp:7346
LD2 scheme not yet implemented for the compressible flow solver.   CConfig.cpp:7367
LD2 scheme available for constant density flows only.   CConfig.cpp:7369
Implicit time scheme is not yet implemented with Mutation++. Use EULER_EXPLICIT.   CConfig.cpp:7598
Cauchy elements are no viable input. Please check your configuration file.   CConfig.cpp:7817
Cauchy elements are no viable input. Please check your configuration file.   CConfig.cpp:7826
The configuration file doesn’t have any definition for marker   CConfig.cpp:8455
Requesting a negative iteration number for the restart file!!   CConfig.cpp:8929
Option TIME_DOMAIN must be the same in all zones. TIME_DOMAIN CConfig.cpp:10598
Option TIME_ITER must be the same in all zones. TIME_ITER CConfig.cpp:10601
Option OUTER_ITER must be the same in all zones. OUTER_ITER CConfig.cpp:10604
Option TIME_STEP must be the same in all zones. TIME_STEP CConfig.cpp:10607
Option MULTIZONE must be the same in all zones. MULTIZONE CConfig.cpp:10614
Option MULTIZONE_MESH must be the same in all zones. MULTIZONE_MESH CConfig.cpp:10617
Option WINDOW_CAUCHY_CRIT must be deactivated for multizone problems. WINDOW_CAUCHY_CRIT CConfig.cpp:10620
Option WINDOW_CAUCHY_CRIT must be deactivated for multizone problems. WINDOW_CAUCHY_CRIT CConfig.cpp:10624

Common/include (15)

Message Options Code
Unrecognized mesh format specified!   CConfig.hpp:5815
Unrecognized mesh_out format specified!   CConfig.hpp:5855
Invalid floating point precision in the header of a binary SU2 solution file.   option_structure.hpp:226
Two versions (1994 and 2003) selected for SST_OPTIONS. Please choose only one. SST_OPTIONS option_structure.hpp:1185
Please select only one SST production term modifier (VORTICITY, KATO-LAUNDER, or UQ).   option_structure.hpp:1194
Please select only one compressibility correction (COMPRESSIBILITY-WILCOX or COMPRESSIBILITY-SARKAR).   option_structure.hpp:1205
Two versions (Negative and Edwards) selected for SA_OPTIONS. Please choose only one. SA_OPTIONS option_structure.hpp:1319
A non-standard version of SA-neg was requested (see https://turbmodels.larc.nasa.gov/spalart.html).   option_structure.hpp:1342
A non-standard version of SA-noft2-Edwards was requested (see https://turbmodels.larc.nasa.gov/spalart.html).   option_structure.hpp:1347
A non-standard version of SA-BCM was requested (see https://turbmodels.larc.nasa.gov/spalart.html).   option_structure.hpp:1352
Two correlations selected for LM_OPTIONS. Please choose only one. LM_OPTIONS option_structure.hpp:1471
Wrong number of arguments for DV_PARAM! DV_PARAM option_structure.inl:670
must begin with a marker name, but starts with the value “ … “. A marker whose name is purely numeric cannot be told apart from a value.   option_structure.inl:1172
Unequal number of values defined for   option_structure.inl:1182
More than one value provided for “string-value” pair, in   option_structure.inl:1189

Common/include/containers (7)

Message Options Code
out of bounds   CPyWrapperMatrixView.hpp:95
is read-only   CPyWrapperMatrixView.hpp:99
out of bounds   CPyWrapperMatrixView.hpp:136
is read-only   CPyWrapperMatrixView.hpp:140
has fewer rows than the number of vertices in the marker.   CPyWrapperMatrixView.hpp:162
out of bounds   CPyWrapperMatrixView.hpp:186
is read-only   CPyWrapperMatrixView.hpp:190

Common/include/geometry/meshreader (1)

Message Options Code
Error while reading the file   CSU2BinaryMeshReaderBase.hpp:105

Common/include/linear_algebra (7)

Message Options Code
The factorization has not been computed yet.   CPastixWrapper.hpp:203
Error solving linear system.   CPastixWrapper.hpp:215
Preconditioner needs to be built with valid references.   CPreconditioner.hpp:179
Preconditioner needs to be built with valid references.   CPreconditioner.hpp:227
Preconditioner needs to be built with valid references.   CPreconditioner.hpp:274
Preconditioner needs to be built with valid references.   CPreconditioner.hpp:320
Preconditioner needs to be built with valid references.   CPreconditioner.hpp:369

Common/include/toolboxes (2)

Message Options Code
Invalid quasi-Newton parameters   CQuasiNewtonInvLeastSquares.hpp:159
NdFlattener: Index out of range.   ndflattener.hpp:297

Common/src (5)

Message Options Code
Unsuccessful call to dgtsv_   wall_model.cpp:202
Not compiled with MKL or LAPACK support   wall_model.cpp:204
Unsuccessful call to dgtsv_   wall_model.cpp:282
Not compiled with MKL or LAPACK support   wall_model.cpp:284
Y+ greater than one: Increase the number of points or growth ratio.   wall_model.cpp:312

Common/src/adt (7)

Message Options Code
Element type not recognized.   CADTElemClass.cpp:546
3D elements not implemented yet   CADTElemClass.cpp:640
Newton did not converge   CADTElemClass.cpp:802
Point not inside the quadrilateral.   CADTElemClass.cpp:809
Newton did not converge   CADTElemClass.cpp:1015
Newton did not converge   CADTElemClass.cpp:1312
Newton did not converge   CADTElemClass.cpp:1706

Common/src/containers (13)

Message Options Code
There is no look-up-table file called   CFileReaderLUT.cpp:58
Version conflict between LUT reader and LUT library file.   CFileReaderLUT.cpp:81
Number of points provided before specifying level count.   CFileReaderLUT.cpp:99
Number of triangles provided before specifying level count.   CFileReaderLUT.cpp:109
Number of hull points provided before specifying level count.   CFileReaderLUT.cpp:119
Table levels are not provided in ascending order.   CFileReaderLUT.cpp:135
Duplicate table levels are present in LUT file   CFileReaderLUT.cpp:138
Number of read variables does not match number of … variables specified in lookup table … library header.   CFileReaderLUT.cpp:172
Number of read points on level … does not match number of points … specified in lookup table library header.   CFileReaderLUT.cpp:216
Number of read triangles on level … does not match number of triangles … specified in lookup table library header.   CFileReaderLUT.cpp:260
Number of read hull nodes on level … does not match number of hull nodes … specified in lookup table library header.   CFileReaderLUT.cpp:305
Flag … not found in file   CFileReaderLUT.cpp:339
Construction of trapezoidal map failed for level … of table   CLookUpTable.cpp:94

Common/src/fem (45)

Message Options Code
Invalid number of Gauss Jacobi integration points   fem_gauss_jacobi_quadrature.cpp:88
Entry not found in map   fem_geometry_structure.cpp:237
Inconsistency in total number of volume elements   fem_geometry_structure.cpp:784
Entry not found in mapGlobalElemIDToInd   fem_geometry_structure.cpp:887
Something went wrong in the renumbering   fem_geometry_structure.cpp:1166
Entry not found in mapGlobalElemIDToInd   fem_geometry_structure.cpp:1359
Entry not found in map   fem_geometry_structure.cpp:1432
Element ID and/or polynomial degree do not match … for this boundary element. This should not happen.   fem_geometry_structure.cpp:2439
Boundary face not found in localFaces. This should not happen.   fem_geometry_structure.cpp:2443
This should not happen   fem_geometry_structure.cpp:3126
This should not happen   fem_geometry_structure.cpp:3154
Corner vertices do not match. This should not happen.   fem_geometry_structure.cpp:3381
Corner vertices do not match. This should not happen.   fem_geometry_structure.cpp:3510
Corner vertices do not match. This should not happen.   fem_geometry_structure.cpp:3810
Corner vertices do not match. This should not happen.   fem_geometry_structure.cpp:4024
Corner vertices do not match. This should not happen.   fem_geometry_structure.cpp:4153
Corner vertices do not match. This should not happen.   fem_geometry_structure.cpp:4299
Top of the pyramid does not coincide with either corner point 1 or 2. … This should not happen   fem_geometry_structure.cpp:4347
Corner vertices do not match. This should not happen.   fem_geometry_structure.cpp:4409
Corner vertices do not match. This should not happen.   fem_geometry_structure.cpp:4629
Negative Jacobian found.   fem_geometry_structure.cpp:5098
Difference is too large to be caused by roundoff   fem_geometry_structure.cpp:5460
Difference is too large to be caused by roundoff   fem_geometry_structure.cpp:5562
Difference is too large to be caused by roundoff   fem_geometry_structure.cpp:5625
Wall function not present yet   fem_geometry_structure.cpp:5823
Exchange location not found in ADT   fem_geometry_structure.cpp:5879
Newton did not converge   fem_geometry_structure.cpp:6163
Polynomial order not supported   fem_integration_rules.cpp:226
Polynomial order not supported   fem_integration_rules.cpp:5580
Wrong size of the A matrix in InverseMatrix   fem_standard_element.cpp:82
Wrong size of the V matrix   fem_standard_element.cpp:144
Wrong size of the VDr matrix   fem_standard_element.cpp:161
Difference is too large to be caused by roundoff   fem_standard_element.cpp:229
Difference is too large to be caused by roundoff   fem_standard_element.cpp:243
Unexpected size of the matrices   fem_standard_element.cpp:883
Wrong size of the V matrix   fem_standard_element.cpp:983
Wrong size of the VDr and/or VDs matrices   fem_standard_element.cpp:1018
Wrong size of the V matrix   fem_standard_element.cpp:1072
Wrong size of the VDr and/or VDs matrices   fem_standard_element.cpp:1095
Wrong size of the V matrix   fem_standard_element.cpp:1119
Wrong size of the V matrix   fem_standard_element.cpp:1278
Wrong size of the V matrix   fem_standard_element.cpp:1420
Wrong size of the V matrix   fem_standard_element.cpp:1531
Corner vertices do not match. This should not happen.   fem_standard_element.cpp:3060
Corner vertices do not match. This should not happen.   fem_standard_element.cpp:3188

Common/src/geometry (69)

Message Options Code
Unrecognized data type for point-to-point MPI comms.   CGeometry.cpp:442
Unrecognized data type for point-to-point MPI comms.   CGeometry.cpp:489
Unrecognized data type for point-to-point MPI comms.   CGeometry.cpp:554
Unrecognized data type for point-to-point MPI comms.   CGeometry.cpp:601
Unrecognized quantity for point-to-point MPI comms.   CGeometry.cpp:635
Unrecognized quantity for point-to-point MPI comms.   CGeometry.cpp:725
Unrecognized quantity for point-to-point MPI comms.   CGeometry.cpp:818
Unrecognized data type for periodic MPI comms.   CGeometry.cpp:1573
Unrecognized data type for periodic MPI comms.   CGeometry.cpp:1620
Unrecognized data type for periodic MPI comms.   CGeometry.cpp:1643
Unable to match local-marker with cfg-marker for Surface Area.   CGeometry.cpp:2853
Unknown type of filter kernel   CGeometry.cpp:3712
Cannot compute the area/volume of a 1D element.   CGeometry.cpp:3920
Multigrid compaction: a fine point still references an emptied coarse CV.   CMultiGridGeometry.cpp:746
The index of the CV is greater than the size of the priority list.   CMultiGridQueue.cpp:47
The index of the CV is greater than the size of the priority list.   CMultiGridQueue.cpp:70
Unrecognized mesh format specified!   CPhysicalGeometry.cpp:94
Mismatch between NPOIN and number of points … listed in mesh file. … Please check the mesh file for correctness.   CPhysicalGeometry.cpp:476
Unrecognized element type.   CPhysicalGeometry.cpp:743
Unrecognized element type.   CPhysicalGeometry.cpp:1011
Unrecognized element type.   CPhysicalGeometry.cpp:1324
Unrecognized element type.   CPhysicalGeometry.cpp:1612
Unrecognized element type.   CPhysicalGeometry.cpp:1684
Unrecognized element type.   CPhysicalGeometry.cpp:1948
Unrecognized mesh format specified!   CPhysicalGeometry.cpp:3493
Element type not supported!   CPhysicalGeometry.cpp:3649
Element type not supported!   CPhysicalGeometry.cpp:3981
RCM ordering failed   CPhysicalGeometry.cpp:4529
RCM ordering failed   CPhysicalGeometry.cpp:4608
Panic!   CPhysicalGeometry.cpp:4963
At the moment only turbomachinery with the same amount of span-wise section can be simulated   CPhysicalGeometry.cpp:5056
Tang grid velocity NOT IMPLEMENTED YET for this configuration   CPhysicalGeometry.cpp:6156
Partitioning failed.   CPhysicalGeometry.cpp:7426
Surface sensitivity not found in file.   CPhysicalGeometry.cpp:7880
Unable to open SU2 restart file   CPhysicalGeometry.cpp:7970
Error reading restart file.   CPhysicalGeometry.cpp:7977
File … is not a binary SU2 restart file. … SU2 reads/writes binary restart files by default. … Note that backward compatibility for ASCII restart files is … possible with the READ_BINARY_RESTART option. READ_BINARY_RESTART CPhysicalGeometry.cpp:7984
Error reading restart file.   CPhysicalGeometry.cpp:8006
Error reading restart file.   CPhysicalGeometry.cpp:8027
Error reading restart file.   CPhysicalGeometry.cpp:8045
Error reading restart file.   CPhysicalGeometry.cpp:8053
Unable to open SU2 restart file   CPhysicalGeometry.cpp:8082
File … is not a binary SU2 restart file. … SU2 reads/writes binary restart files by default. … Note that backward compatibility for ASCII restart files is … possible with the READ_BINARY_RESTART option. READ_BINARY_RESTART CPhysicalGeometry.cpp:8099
Sensitivity x not found in file.   CPhysicalGeometry.cpp:8249
Sensitivity y not found in file.   CPhysicalGeometry.cpp:8252
Sensitivity z not found in file.   CPhysicalGeometry.cpp:8256
Unable to open SU2 restart file   CPhysicalGeometry.cpp:8316
Error reading restart file.   CPhysicalGeometry.cpp:8323
File … is a binary SU2 restart file, expected ASCII. … SU2 reads/writes binary restart files by default. … Note that backward compatibility for ASCII restart files is … possible with the READ_BINARY_RESTART option. READ_BINARY_RESTART CPhysicalGeometry.cpp:8330
Unable to open SU2 restart file   CPhysicalGeometry.cpp:8353
File … is a binary SU2 restart file, expected ASCII. … SU2 reads/writes binary restart files by default. … Note that backward compatibility for ASCII restart files is … possible with the READ_BINARY_RESTART option. READ_BINARY_RESTART CPhysicalGeometry.cpp:8368
There is no adjoint restart file   CPhysicalGeometry.cpp:8381
Sensitivity x not found in file.   CPhysicalGeometry.cpp:8399
Sensitivity y not found in file.   CPhysicalGeometry.cpp:8402
Sensitivity z not found in file.   CPhysicalGeometry.cpp:8406
There is no unordered ASCII sensitivity file   CPhysicalGeometry.cpp:8486
No external points given to ADT.   CPhysicalGeometry.cpp:8512
Not enough points in the input sensitivity file.   CPhysicalGeometry.cpp:8568
Handling of non-matching faces not implemented yet   CPhysicalGeometryFEM.cpp:773
Entry not found in mapExternalElemIDToTimeLevel   CPhysicalGeometryFEM.cpp:798
Negative Jacobian found   CPhysicalGeometryFEM.cpp:1318
Boundary face not found in faces of element   CPhysicalGeometryFEM.cpp:1718
message.str()   CPhysicalGeometryFEM.cpp:1910
Entry not found in mapExternalElemIDToTimeLevel   CPhysicalGeometryFEM.cpp:2423
Entry not found in mapExternalElemIDToTimeLevel   CPhysicalGeometryFEM.cpp:2500
Entry not found in mapExternalElemIDToTimeLevel   CPhysicalGeometryFEM.cpp:2557
Entry not found in mapExternalElemIDToTimeLevel   CPhysicalGeometryFEM.cpp:2618
No matching standard boundary element found   CPhysicalGeometryFEM.cpp:2935
Entry not found in mapExternalElemIDToTimeLevel   CPhysicalGeometryFEM.cpp:3013

Common/src/geometry/meshreader (36)

Message Options Code
SU2 built without CGNS support. … To use CGNS, build SU2 accordingly.   CCGNSMeshReaderBase.cpp:37
was not found or is not a properly formatted … CGNS file. Note that SU2 expects unstructured … CGNS files in ADF data format.   CCGNSMeshReaderBase.cpp:51
CGNS reader currently can only handle 1 database.   CCGNSMeshReaderBase.cpp:89
CGNS reader currently expects only 1 zone per CGNS file. … Multizone problems can be run with separate CGNS files for each zone.   CCGNSMeshReaderBase.cpp:126
Structured CGNS zone found while unstructured expected.   CCGNSMeshReaderBase.cpp:155
CGNS reader currently handles only 1 grid per zone.   CCGNSMeshReaderBase.cpp:172
Unknown coordinate name, … , in the CGNS file.   CCGNSMeshReaderBase.cpp:231
Vertex elements detected. Please remove.   CCGNSMeshReaderBase.cpp:385
Line elements detected in a 3D mesh. Please remove.   CCGNSMeshReaderBase.cpp:393
SU2 built without CGNS support. … To use CGNS, build SU2 accordingly.   CCGNSMeshReaderFEM.cpp:65
Invalid point requested. This should not happen.   CCGNSMeshReaderFEM.cpp:476
SU2 built without CGNS support. … To use CGNS, build SU2 accordingly.   CCGNSMeshReaderFVM.cpp:72
Error opening SU2 ASCII grid. … Check that the file exists.   CSU2ASCIIMeshReaderBase.cpp:45
Could not find the IZONE= keyword or the zone contents. … Check the SU2 ASCII file format.   CSU2ASCIIMeshReaderBase.cpp:72
Markers must be listed after points and elements in the SU2 mesh file.   CSU2ASCIIMeshReaderBase.cpp:177
Could not find the keyword “NDIME=”. … Check the SU2 ASCII file format.   CSU2ASCIIMeshReaderBase.cpp:197
Could not find the keyword “NPOIN=”. … Check the SU2 ASCII file format.   CSU2ASCIIMeshReaderBase.cpp:203
Could not find the keyword “NELEM=”. … Check the SU2 ASCII file format.   CSU2ASCIIMeshReaderBase.cpp:209
Could not find the keyword “NMARK=”. … Check the SU2 ASCII file format.   CSU2ASCIIMeshReaderBase.cpp:215
Mesh file contains deprecated SEND_RECEIVE marker! … Please remove any SEND_RECEIVE markers from the SU2 ASCII mesh.   CSU2ASCIIMeshReaderBase.cpp:419
Line boundary conditions are not possible for 3D calculations. … Please check the SU2 ASCII mesh file.   CSU2ASCIIMeshReaderBase.cpp:441
Mesh file contains deprecated periodic format!   CSU2ASCIIMeshReaderBase.cpp:489
Current implementation can only split a single actuator disk. … Remove disks or re-export your mesh with double surfaces (repeated points).   CSU2ASCIIMeshReaderFVM.cpp:105
The file … is not a valid SU2 binary file   CSU2BinaryMeshReaderBase.cpp:70
Error opening SU2 binary grid file … . Check that the file exists   CSU2BinaryMeshReaderBase.cpp:80
No support for actuator disks yet   CSU2BinaryMeshReaderBase.cpp:110
Wrong number of items in volume connectivity   CSU2BinaryMeshReaderBase.cpp:331
Mesh file contains deprecated SEND_RECEIVE marker! … Please remove any SEND_RECEIVE markers from the SU2 binary mesh.   CSU2BinaryMeshReaderBase.cpp:368
Wrong number of items in surface connectivity   CSU2BinaryMeshReaderBase.cpp:406
Line boundary conditions are not possible for 3D calculations. … Please check the SU2 binary file.   CSU2BinaryMeshReaderBase.cpp:409
Error opening SU2 binary grid file … . Check that the file exists   CSU2BinaryMeshReaderFEM.cpp:43
Not implemented yet   CSU2BinaryMeshReaderFEM.cpp:65
Not implemented yet   CSU2BinaryMeshReaderFEM.cpp:68
Not implemented yet   CSU2BinaryMeshReaderFEM.cpp:72
Error opening SU2 binary grid file … . Check that the file exists   CSU2BinaryMeshReaderFVM.cpp:52
Not implemented yet   CSU2BinaryMeshReaderFVM.cpp:66

Common/src/grid_movement (19)

Message Options Code
Higher order derivatives for BSplines are not implemented.   CBSplineBlending.cpp:144
There are no FFD boxes in the mesh file!!   CSurfaceMovement.cpp:174
There is not FFD box definition in the mesh file, … run DV_KIND=FFD_SETTING first !! DV_KIND CSurfaceMovement.cpp:209
There is no FFD box with tag “ … “ defined in the mesh file. … Check the definition of the design variables and/or the FFD settings !!   CSurfaceMovement.cpp:218
No markers are specified in DV_MARKER, so no deformation will occur. … List markers to be deformed in DV_MARKER. DV_MARKER CSurfaceMovement.cpp:228
There are no FFD Boxes in the mesh file!!   CSurfaceMovement.cpp:528
No surface positions file found and template writing not yet supported in parallel. To generate a   CSurfaceMovement.cpp:568
The FFD box ‘ … ‘ is not properly defined. The first 4 points must be listed counter … clockwise, such that applying the right-hand rule results in a vector into the box. … This is according to the VTK hexahedron ordering: … 7 +—-+ 6 … /| /| … 4 +—-+5| … |3+–|-+ 2 … |/ |/ … 0 +—-+ 1 … The CCW convention also applies in 2D, where only the bottom face is specified.   CSurfaceMovement.cpp:818
There is no surface positions file   CSurfaceMovement.cpp:3560
‘HicksHenneCamber’ can not be combined with other design variables.   CSurfaceMovement.cpp:3711
No input read!!   CSurfaceMovement.cpp:3936
There is no airfoil file   CSurfaceMovement.cpp:3940
No input read!!   CSurfaceMovement.cpp:3945
No input read!!   CSurfaceMovement.cpp:3951
No input read!!   CSurfaceMovement.cpp:3957
No input read!!   CSurfaceMovement.cpp:3963
ReadFFDInfo:: There is no geometry file called   CSurfaceMovement.cpp:4192
Deprecated FFD information found in mesh file. … FFD information generated with SU2 version <= 4.3 is incompatible with the current version. … Run SU2_DEF again with DV_KIND= FFD_SETTING. DV_KIND CSurfaceMovement.cpp:4328
There is no FFD box definition. Check the config file.   CSurfaceMovement.cpp:4801

Common/src/interface_interpolation (4)

Message Options Code
Unknown type of interpolation.   CInterpolatorFactory.cpp:84
The order of the zones does not allow conservative interpolation to be setup. … Swap zones … and … .   CMirror.cpp:38
MixingPlane interface option not implemented yet   CMixingPlane.cpp:147
Somehow there are no target interpolation points.   CRadialBasisFunction.cpp:411

Common/src/linear_algebra (32)

Message Options Code
Error during preparation of PaStiX data   CPastixWrapper.cpp:178
Error analyzing matrix:   CPastixWrapper.cpp:204
Unknown type of PaStiX factorization.   CPastixWrapper.cpp:305
Error factorizing matrix:   CPastixWrapper.cpp:312
GPU acceleration is not supported for AD scalar types.   CSysMatrix.cpp:56
GPU acceleration is not available in the AD and direct differentiation solvers.   CSysMatrix.cpp:59
ENABLE_CUDA is set to YES but SU2 was not compiled with CUDA support; … recompile with CUDA enabled in Meson to use GPU functions. ENABLE_CUDA CSysMatrix.cpp:61
CSysMatrix can only be initialized once.   CSysMatrix.cpp:194
CUDA CSysMatrix block-LDU SpMV requires square blocks.   CSysMatrix.cpp:300
CUDA preconditioners require square blocks.   CSysMatrix.cpp:419
Unrecognized quantity for point-to-point MPI comms.   CSysMatrix.cpp:568
Unrecognized quantity for point-to-point MPI comms.   CSysMatrix.cpp:652
Unrecognized quantity for point-to-point MPI comms.   CSysMatrix.cpp:763
nVar values incompatible.   CSysMatrix.cpp:970
nPoint and nBlk values incompatible.   CSysMatrix.cpp:973
Matrices do not have compatible sparsity.   CSysMatrix.cpp:1801
SU2 was not compiled with -DHAVE_PASTIX   CSysMatrix.cpp:1826
SU2 was not compiled with -DHAVE_PASTIX   CSysMatrix.cpp:1841
Number of linear solver iterations must be greater than 0.   CSysSolve.cpp:284
Number of linear solver iterations must be greater than 0.   CSysSolve.cpp:437
FGMRES subspace is too large (>1000).   CSysSolve.cpp:441
Number of linear solver restart iterations must be greater than 0.   CSysSolve.cpp:676
FGCRODR subspace is too large (> 200).   CSysSolve.cpp:679
Number of linear solver iterations must be greater than 0.   CSysSolve.cpp:1073
Number of linear solver iterations must be greater than 0.   CSysSolve.cpp:1264
Unknown type of linear solver.   CSysSolve.cpp:1565
The specified preconditioner is not yet implemented for the discrete adjoint method.   CSysSolve.cpp:1618
Unknown type of linear solver.   CSysSolve.cpp:1766
If this class were constructed in parallel its operations would be incorrect.   CSysVector.cpp:36
Only the master thread is allowed to initialize the vector.   CSysVector.cpp:40
GPU acceleration is not supported for AD scalar types.   CSysVector.cpp:93
Error in multiDot ENABLE_CUDA is set to YES Please compile with CUDA options … enabled in Meson to access GPU Functions ENABLE_CUDA CSysVector.cpp:96

Common/src/toolboxes (7)

Message Options Code
Matrix is singular   CSquareMatrixCM.cpp:72
Matrix inversion failed   CSquareMatrixCM.cpp:75
LLT factorization failed.   CSymmetricMatrix.cpp:82
LDLT factorization failed.   CSymmetricMatrix.cpp:141
Inversion with LDLT factorization failed.   CSymmetricMatrix.cpp:143
LLT factorization failed.   CSymmetricMatrix.cpp:154
Inversion with LLT factorization failed.   CSymmetricMatrix.cpp:156

Common/src/toolboxes/MMS (76)

Message Options Code
CIncTGVSolution not yet fully implemented/tested.   CIncTGVSolution.cpp:37
Unsteady mode must be selected for the incompressible Taylor Green Vortex   CIncTGVSolution.cpp:66
Incompressible flow equations must be selected for the incompressible Taylor Green Vortex   CIncTGVSolution.cpp:70
Navier Stokes equations must be selected for the incompressible Taylor Green Vortex   CIncTGVSolution.cpp:74
Constant density fluid model must be selected for the incompressible Taylor Green Vortex   CIncTGVSolution.cpp:78
Constant viscosity must be selected for the incompressible Taylor Green Vortex   CIncTGVSolution.cpp:82
Energy equation must be disabled (isothermal) for the incompressible Taylor Green Vortex   CIncTGVSolution.cpp:85
2D calculation required for the incompressible Taylor Green Vortex   CIncTGVSolution.cpp:88
Unsteady mode must be selected for the inviscid vortex   CInviscidVortexSolution.cpp:64
Compressible flow equations must be selected for the inviscid vortex   CInviscidVortexSolution.cpp:70
Euler equations must be selected for the inviscid vortex   CInviscidVortexSolution.cpp:73
Standard air or ideal gas must be selected for the inviscid vortex   CInviscidVortexSolution.cpp:76
Free-stream pressure must be 1.0 for the inviscid vortex   CInviscidVortexSolution.cpp:79
Free-stream density must be 1.0 for the inviscid vortex   CInviscidVortexSolution.cpp:82
Steady mode must be selected for the MMS incompressible Euler case   CMMSIncEulerSolution.cpp:62
Incompressible flow equations must be selected for the MMS incompressible Euler case   CMMSIncEulerSolution.cpp:66
Euler equations must be selected for the MMS incompressible Euler case   CMMSIncEulerSolution.cpp:70
Constant density fluid model must be selected for the MMS incompressible Euler case   CMMSIncEulerSolution.cpp:73
Energy equation must be disabled (isothermal) for the MMS incompressible Euler case   CMMSIncEulerSolution.cpp:77
Steady mode must be selected for the MMS incompressible NS case   CMMSIncNSSolution.cpp:63
Incompressible flow equations must be selected for the MMS incompressible NS case   CMMSIncNSSolution.cpp:67
Navier Stokes equations must be selected for the MMS incompressible NS case   CMMSIncNSSolution.cpp:71
Constant density fluid model must be selected for the MMS incompressible NS case   CMMSIncNSSolution.cpp:74
Constant viscosity must be selected for the MMS incompressible NS case   CMMSIncNSSolution.cpp:78
Energy equation must be disabled (isothermal) for the MMS incompressible NS case   CMMSIncNSSolution.cpp:81
Steady mode must be selected for the MMS NS Two Half Circles case   CMMSNSTwoHalfCirclesSolution.cpp:80
Compressible flow equations must be selected for the MMS NS Two Half Circles case   CMMSNSTwoHalfCirclesSolution.cpp:86
Navier Stokes equations must be selected for the MMS NS Two Half Circles case   CMMSNSTwoHalfCirclesSolution.cpp:90
Standard air or ideal gas must be selected for the MMS NS Two Half Circles case   CMMSNSTwoHalfCirclesSolution.cpp:93
Sutherland must be selected for viscosity for the MMS NS Two Half Circles case   CMMSNSTwoHalfCirclesSolution.cpp:96
Constant Prandtl number must be selected for the MMS NS Two Half Circles case   CMMSNSTwoHalfCirclesSolution.cpp:99
Grid must be 3D for the MMS NS Two Half Spheres case   CMMSNSTwoHalfSpheresSolution.cpp:80
Steady mode must be selected for the MMS NS Two Half Spheres case   CMMSNSTwoHalfSpheresSolution.cpp:83
Compressible flow equations must be selected for the MMS NS Two Half Spheres case   CMMSNSTwoHalfSpheresSolution.cpp:89
Navier Stokes equations must be selected for the MMS NS Two Half Spheres case   CMMSNSTwoHalfSpheresSolution.cpp:93
Standard air or ideal gas must be selected for the MMS NS Two Half Spheres case   CMMSNSTwoHalfSpheresSolution.cpp:96
Sutherland must be selected for viscosity for the MMS NS Two Half Spheres case   CMMSNSTwoHalfSpheresSolution.cpp:99
Constant Prandtl number must be selected for the MMS NS Two Half Spheres case   CMMSNSTwoHalfSpheresSolution.cpp:102
Steady mode must be selected for the MMS NS Unit Quad case   CMMSNSUnitQuadSolution.cpp:89
Compressible flow equations must be selected for the MMS NS Unit Quad case   CMMSNSUnitQuadSolution.cpp:95
Navier Stokes equations must be selected for the MMS NS Unit Quad case   CMMSNSUnitQuadSolution.cpp:98
Standard air or ideal gas must be selected for the MMS NS Unit Quad case   CMMSNSUnitQuadSolution.cpp:101
Constant viscosity must be selected for the MMS NS Unit Quad case   CMMSNSUnitQuadSolution.cpp:104
Constant Prandtl number must be selected for the MMS NS Unit Quad case   CMMSNSUnitQuadSolution.cpp:107
Steady mode must be selected for the MMS NS Unit Quad case with wall BCs.   CMMSNSUnitQuadSolutionWallBC.cpp:82
Compressible flow equations must be selected for the MMS NS Unit Quad case with wall BCs.   CMMSNSUnitQuadSolutionWallBC.cpp:88
Navier Stokes equations must be selected for the MMS NS Unit Quad case with wall BCs.   CMMSNSUnitQuadSolutionWallBC.cpp:92
Standard air or ideal gas must be selected for the MMS NS Unit Quad case with wall BCs.   CMMSNSUnitQuadSolutionWallBC.cpp:96
Sutherland must be selected for viscosity for the MMS NS Unit Quad case with wall BCs.   CMMSNSUnitQuadSolutionWallBC.cpp:100
Constant Prandtl number must be selected for the MMS NS Unit Quad case with wall BCs.   CMMSNSUnitQuadSolutionWallBC.cpp:104
Steady mode must be selected for the NS Unit Quad case   CNSUnitQuadSolution.cpp:55
Compressible flow equations must be selected for the NS Unit Quad case   CNSUnitQuadSolution.cpp:61
Navier Stokes equations must be selected for the NS Unit Quad case   CNSUnitQuadSolution.cpp:64
Ideal gas must be selected for the NS Unit Quad case   CNSUnitQuadSolution.cpp:67
Gamma must be 1.5 for the NS Unit Quad case   CNSUnitQuadSolution.cpp:69
Constant viscosity must be selected for the NS Unit Quad case   CNSUnitQuadSolution.cpp:72
Constant Prandtl number must be selected for the NS Unit Quad case   CNSUnitQuadSolution.cpp:75
Laminar Prandtl number must be larger than 1.e+20 for the NS Unit Quad case   CNSUnitQuadSolution.cpp:78
Steady mode must be selected for the Ringleb case   CRinglebSolution.cpp:52
Compressible flow equations must be selected for the Ringleb case   CRinglebSolution.cpp:58
Euler equations must be selected for the Ringleb case   CRinglebSolution.cpp:61
Standard air or ideal gas must be selected for the Ringleb case   CRinglebSolution.cpp:64
Newton algorithm did not converge   CRinglebSolution.cpp:135
Unsteady mode must be selected for the Taylor Green Vortex   CTGVSolution.cpp:60
Compressible flow equations must be selected for the Taylor Green Vortex   CTGVSolution.cpp:66
Navier Stokes equations must be selected for the Taylor Green Vortex   CTGVSolution.cpp:69
Standard air or ideal gas must be selected for the Taylor Green Vortex   CTGVSolution.cpp:72
Constant viscosity must be selected for the Taylor Green Vortex   CTGVSolution.cpp:75
Constant Prandtl number must be selected for the Taylor Green Vortex   CTGVSolution.cpp:78
User must implement this function   CUserDefinedSolution.cpp:45
User must implement this function   CUserDefinedSolution.cpp:52
User must implement this function   CUserDefinedSolution.cpp:57
User must implement this function   CUserDefinedSolution.cpp:62
User must implement this function   CUserDefinedSolution.cpp:66
Function must be overwritten by the derived class   CVerificationSolution.cpp:85
Function must be overwritten by the derived class   CVerificationSolution.cpp:95

SU2_CFD/include (7)

Message Options Code
Not implemented yet   sgs_model.inl:194
Not implemented yet   sgs_model.inl:233
Not implemented yet   sgs_model.inl:364
Not implemented yet   sgs_model.inl:403
Not implemented yet   sgs_model.inl:421
Not implemented yet   sgs_model.inl:494
Not implemented yet   sgs_model.inl:533

SU2_CFD/include/drivers (10)

Message Options Code
is not in MARKER_MONITORING. MARKER_MONITORING CDriverBase.hpp:139
is not in MARKER_ANALYZE. MARKER_ANALYZE CDriverBase.hpp:153
Initial coordinates are only available with DEFORM_MESH= YES DEFORM_MESH CDriverBase.hpp:226
Initial coordinates are only available with DEFORM_MESH= YES DEFORM_MESH CDriverBase.hpp:238
Marker index exceeds size.   CDriverBase.hpp:240
Marker index exceeds size.   CDriverBase.hpp:260
Zone index out of range   CDriverBase.hpp:585
Normal heat flux is only available for flow or heat solvers.   CDriverBase.hpp:606
Marker index exceeds size.   CDriverBase.hpp:774
The selected solver does not exist.   CDriverBase.hpp:777

SU2_CFD/include/fluid (4)

Message Options Code
Conductivity model not available for this fluid in CoolProp library.   CCoolPropConductivity.hpp:67
SU2 was not compiled with CoolProp (-Denable-coolprop=true). Note that CoolProp cannot be used with … directdiff or autodiff   CCoolPropConductivity.hpp:70
Viscosity model not available for this fluid in CoolProp library.   CCoolPropViscosity.hpp:122
SU2 was not compiled with CoolProp (-Denable-coolprop=true). Note that CoolProp cannot be used with … directdiff or autodiff   CCoolPropViscosity.hpp:125

SU2_CFD/include/gradients (2)

Message Options Code
Too many dimensions to compute gradients.   computeGradientsGreenGauss.hpp:204
Too many dimensions to compute gradients.   computeGradientsLeastSquares.hpp:362

SU2_CFD/include/limiters (2)

Message Options Code
Too many dimensions to compute limiters.   computeLimiters.hpp:56
Unknown limiter type.   computeLimiters.hpp:118

SU2_CFD/include/numerics/scalar (1)

Message Options Code
Static arrays are too small for the requested equation count.   scalar_edge_flux.hpp:371

SU2_CFD/include/numerics/turbulent/transition (2)

Message Options Code
Transition correlation is set to DEFAULT but no default value has ben set in the code.   trans_correlations.hpp:112
Transition correlation is set to DEFAULT but no default value has ben set in the code.   trans_correlations.hpp:185

SU2_CFD/include/output (4)

Message Options Code
Cannot find output field with name   COutput.hpp:496
Cannot find output field with name   COutput.hpp:531
Cannot find output field with name   COutput.hpp:715
Cannot find output field with name   COutput.hpp:753

SU2_CFD/include/output/filewriter (2)

Message Options Code
Unknown Type   CParaviewXMLFileWriter.hpp:157
Local renumbered iPoint ID … is larger than max number of nodes   CSurfaceFVMDataSorter.hpp:78

SU2_CFD/include/solvers (13)

Message Options Code
Not implemented for this solver.   CFVMFlowSolverBase.hpp:397
Out-of-bounds marker index used on inlet.   CFVMFlowSolverBase.hpp:2189
Out-of-bounds vertex index used on inlet.   CFVMFlowSolverBase.hpp:2191
Out-of-bounds marker index used on inlet.   CFVMFlowSolverBase.hpp:2206
Out-of-bounds vertex index used on inlet.   CFVMFlowSolverBase.hpp:2208
Out-of-bounds marker index used on inlet.   CFVMFlowSolverBase.hpp:2225
Out-of-bounds vertex index used on inlet.   CFVMFlowSolverBase.hpp:2227
The solution file … does not match with the mesh file. … This can be caused by empty lines at the end of the file.   CFVMFlowSolverBase.inl:967
Implement customized boundary conditions here.   CFVMFlowSolverBase.inl:1558
The equation count of this model has no instantiation.   CScalarSolver.hpp:401
Out-of-bounds marker index used on inlet.   CTurbSolver.hpp:121
Out-of-bounds vertex index used on inlet.   CTurbSolver.hpp:123
Out-of-bounds index used for inlet turbulence variable.   CTurbSolver.hpp:125

SU2_CFD/src (1)

Message Options Code
The required solver doesn’t support multizone simulations   SU2_CFD.cpp:112

SU2_CFD/src/drivers (51)

Message Options Code
There is no discrete adjoint functionality for one of the specified solvers yet.   CDiscAdjMultizoneDriver.cpp:114
The tape debug mode tag system is limited to a maximum zone number of 100.   CDiscAdjMultizoneDriver.cpp:273
InitializeGeometryDGFEM: Coarse grid levels not implemented yet.   CDriver.cpp:1043
Inlet profile specification via file (C++) has not been … implemented yet for this solver. … Please set SPECIFIED_INLET_PROFILE= NO and try again. SPECIFIED_INLET_PROFILE CDriver.cpp:1125
A restart capability has not been implemented yet for this solver. … Please set RESTART_SOL= NO and try again. RESTART_SOL CDriver.cpp:1195
No turbulence model selected.   CDriver.cpp:1258
Config file is missing the CONV_NUM_METHOD_TURB option. CONV_NUM_METHOD_TURB CDriver.cpp:1286
Invalid convective scheme for the turbulence equations.   CDriver.cpp:1291
Config file is missing the CONV_NUM_METHOD_TURB option. CONV_NUM_METHOD_TURB CDriver.cpp:1334
Invalid convective scheme for the transition equations.   CDriver.cpp:1339
Invalid convective scheme for the species transport equations. Use SCALAR_UPWIND.   CDriver.cpp:1379
Convective scheme not implemented (template_solver).   CDriver.cpp:1592
Config file is missing the CONV_NUM_METHOD_FLOW option. CONV_NUM_METHOD_FLOW CDriver.cpp:1617
Invalid upwind scheme or not implemented.   CDriver.cpp:1760
Invalid convective scheme for the Euler / Navier-Stokes equations.   CDriver.cpp:1797
Config file is missing the CONV_NUM_METHOD_FLOW option. CONV_NUM_METHOD_FLOW CDriver.cpp:1898
Invalid centered scheme or not implemented.   CDriver.cpp:1907
Invalid upwind scheme or not implemented.   CDriver.cpp:1959
Invalid convective scheme for the NEMO Euler / Navier-Stokes equations.   CDriver.cpp:1967
Riemann solver not implemented.   CDriver.cpp:2030
Species transport only available for standard compressible and incompressible flow.   CDriver.cpp:2067
Invalid convective scheme for the heat transfer equations.   CDriver.cpp:2080
Convective schemes not implemented for incompressible continuous adjoint.   CDriver.cpp:2107
Config file is missing the CONV_NUM_METHOD_ADJFLOW option. CONV_NUM_METHOD_ADJFLOW CDriver.cpp:2113
Centered scheme not implemented.   CDriver.cpp:2126
Upwind scheme not implemented.   CDriver.cpp:2153
Invalid convective scheme for the continuous adjoint Euler / Navier-Stokes equations.   CDriver.cpp:2160
Only the SA turbulence model can be used with the continuous adjoint solver.   CDriver.cpp:2222
Config file is missing the CONV_NUM_METHOD_ADJTURB option. CONV_NUM_METHOD_ADJTURB CDriver.cpp:2227
Convective scheme not implemented (adjoint turbulence).   CDriver.cpp:2234
Material model does not correspond to geometric conditions.   CDriver.cpp:2265
Material model does not correspond to geometric conditions.   CDriver.cpp:2272
Material model not implemented.   CDriver.cpp:2278
Material model not implemented.   CDriver.cpp:2285
Material model not implemented.   CDriver.cpp:2292
Mesh deformation was not correctly specified for the fluid/heat zone.   CDriver.cpp:2495
Could not determine the number of variables for transfer.   CDriver.cpp:2549
Invalid KindSolver for CDiscAdj-MultiZone/SingleZone-Driver.   CDriver.cpp:2855
Element index exceeds size.   CDriverBase.cpp:171
Element index exceeds size.   CDriverBase.cpp:178
Node index exceeds mesh size.   CDriverBase.cpp:197
Node index exceeds mesh size.   CDriverBase.cpp:204
Marker index exceeds size.   CDriverBase.cpp:339
Marker element index exceeds size.   CDriverBase.cpp:346
Marker element index exceeds size.   CDriverBase.cpp:353
Marker index exceeds size.   CDriverBase.cpp:366
Vertex index exceeds marker size.   CDriverBase.cpp:373
Vertex index exceeds marker size.   CDriverBase.cpp:381
Solver name was not defined.   CDriverBase.cpp:404
The FEA solver does not exist.   CDriverBase.cpp:413
The flow solver does not exist.   CDriverBase.cpp:434

SU2_CFD/src/fluid (14)

Message Options Code
SU2 was not compiled with CoolProp (-Denable-coolprop=true). Note that CoolProp cannot be used with directdiff … or autodiff   CCoolProp.cpp:123
SU2 was not compiled with MLPCpp enabled (-Denable-mlpcpp=true).   CDataDrivenFluid.cpp:53
SU2 was not compiled with MLPCpp enabled (-Denable-mlpcpp=true).   CFluidFlamelet.cpp:96
Preferential diffusion scalars not included in flamelet manifold.   CFluidFlamelet.cpp:232
Output vector size incompatible with manifold lookup operation.   CFluidFlamelet.cpp:322
Viscosity model not available.   CFluidModel.cpp:66
Conductivity model not available.   CFluidModel.cpp:119
Diffusivity model not available.   CFluidModel.cpp:148
Catalytic wall recombination not implemented for specified Mutation gas model.   CMutationTCLib.cpp:92
Array dPdU not allocated!   CNEMOGas.cpp:161
CONFIG ERROR: nSpecies mismatch between gas model & gas composition   CSU2TCLib.cpp:84
CONFIG ERROR: nSpecies mismatch between gas model & gas composition   CSU2TCLib.cpp:151
CONFIG ERROR: nSpecies mismatch between gas model & gas composition   CSU2TCLib.cpp:314
CONFIG ERROR: nSpecies mismatch between gas model & gas composition   CSU2TCLib.cpp:680

SU2_CFD/src/integration (1)

Message Options Code
Time integration scheme not implemented.   CFEM_DG_Integration.cpp:181

SU2_CFD/src/interfaces/cht (1)

Message Options Code
Polynomial Conductivity model not implemented for CHT interface.   CConjugateHeatInterface.cpp:110

SU2_CFD/src/iteration (4)

Message Options Code
Outlet pressure ramp only implemented for NRBC   CFluidIteration.cpp:355
The gust length needs to be positive   CFluidIteration.cpp:517
There is no vortex data file!!   CFluidIteration.cpp:624
No iteration found for specified solver.   CIterationFactory.cpp:123

SU2_CFD/src/numerics (1)

Message Options Code
Unrecognized upwind/central blending scheme!   CNumerics.cpp:1572

SU2_CFD/src/numerics/NEMO (1)

Message Options Code
nVar and nSpecies mismatch.   CNEMONumerics.cpp:330

SU2_CFD/src/numerics/NEMO/convection (2)

Message Options Code
AUSM+-Up2 requires a reference Mach number (“MACH_NUMBER”) greater than 0. MACH_NUMBER ausm_slau.cpp:494
AUSM+M requires a reference Mach number (“MACH_NUMBER”) greater than 0. MACH_NUMBER ausm_slau.cpp:567

SU2_CFD/src/numerics/elasticity (5)

Message Options Code
The electric field dimensions do not agree with the geometry.   CFEANonlinearElasticity.cpp:60
The electric field has not been defined.   CFEANonlinearElasticity.cpp:76
This material model cannot (yet) be used for plane stress.   nonlinear_models.cpp:140
This material model cannot (yet) be used for plane stress.   nonlinear_models.cpp:264
This material model cannot be used for 3D yet.   nonlinear_models.cpp:290

SU2_CFD/src/numerics/flow/convection (2)

Message Options Code
AUSM+Up requires a reference Mach number (“MACH_NUMBER”) greater than 0. MACH_NUMBER ausm_slau.cpp:400
AUSM+Up2 requires a reference Mach number (“MACH_NUMBER”) greater than 0. MACH_NUMBER ausm_slau.cpp:624

SU2_CFD/src/output (23)

Message Options Code
No coordinates found in the restart file!!   CBaselineOutput.cpp:79
No coordinates found in the restart file!!   CBaselineOutput.cpp:83
Number of requested fields and number of variables do not match.   CBaselineOutput.cpp:106
SetAnalyzeSurface is not implemented for FEM-DG solver.   CFlowCompFEMOutput.cpp:258
Custom outputs of type ‘Function’ cannot reference solver variables.   CFlowOutput.cpp:787
Inactive solver variable ( … ) used in function … … E.g. this may only be a variable of the compressible solver.   CFlowOutput.cpp:794
Invalid history output or solver variable ( … ) used in function … Valid solvers variables:   CFlowOutput.cpp:803
Wrong number of coordinates to specify probe   CFlowOutput.cpp:899
Cannot process PerSurface *_SURF history output:   CMultizoneOutput.cpp:169
Per Surface output group unknown:   CMultizoneOutput.cpp:180
Number of Cauchy Elems must be smaller than 1000   COutput.cpp:154
Number of Time Cauchy Elems must be smaller than 1000   COutput.cpp:157
Invalid history output ( … ) used in expression:   COutput.cpp:309
SU2 has diverged (NaN detected).   COutput.cpp:976
SU2 has diverged (NaN detected).   COutput.cpp:1085
The Full-MG startup has no criterion left to promote on and would stay on the   COutput.cpp:1366
Obsolete NEMO CONV_FIELD ‘ CONV_FIELD COutput.cpp:1559
Cannot find output field with name   COutput.cpp:1815
Cannot find output field with name   COutput.cpp:1849
Cannot find output field with name   COutput.cpp:1889
Invalid operation type ‘   COutput.cpp:2280
The current solver can only use ‘Function’ custom outputs.   COutput.cpp:2345
Invalid history output ( … ) used in function   COutput.cpp:2358

SU2_CFD/src/output/filewriter (25)

Message Options Code
Connectivity must be sorted.   CCGNSFileWriter.cpp:206
Unrecognized element type   CFEMDataSorter.cpp:124
Unrecognized element type   CFEMDataSorter.cpp:227
Unrecognized element type   CFVMDataSorter.cpp:164
Unrecognized element type   CFVMDataSorter.cpp:494
GEO_TYPE not found   CParallelDataSorter.cpp:368
Unable to open file   CParallelFileWriter.cpp:228
Unable to open file   CParallelFileWriter.cpp:260
Unable to open file   CParallelFileWriter.cpp:268
Connectivity must be sorted.   CParaviewBinaryFileWriter.cpp:54
Connectivity must be sorted.   CParaviewFileWriter.cpp:41
Connectivity must be sorted.   CParaviewXMLFileWriter.cpp:66
Writing array size failed   CParaviewXMLFileWriter.cpp:369
Writing data array failed   CParaviewXMLFileWriter.cpp:375
Unsupported element type for the STL writer.   CSTLFileWriter.cpp:291
STL File-Writer: Halo node not found.   CSTLFileWriter.cpp:329
Cannot find   CSU2MeshBinaryFileWriter.cpp:190
Cannot find   CSU2MeshFileWriter.cpp:126
Connectivity must be sorted before sorting output data   CSurfaceFEMDataSorter.cpp:72
Unrecognized element type   CSurfaceFEMDataSorter.cpp:369
Unrecognized element type   CSurfaceFEMDataSorter.cpp:468
Unrecognized element type   CSurfaceFVMDataSorter.cpp:1140
Unrecognized element type   CSurfaceFVMDataSorter.cpp:1470
Connectivity must be sorted.   CTecplotBinaryFileWriter.cpp:54
Connectivity must be sorted.   CTecplotFileWriter.cpp:41

SU2_CFD/src/solvers (148)

Message Options Code
This functional is not possible in 2D!!   CAdjEulerSolver.cpp:765
This functional is not possible in 2D!!   CAdjEulerSolver.cpp:777
This functional is not possible in 2D!!   CAdjEulerSolver.cpp:791
This functional is not possible in 2D!!   CAdjEulerSolver.cpp:850
This functional is not possible in 2D!!   CAdjEulerSolver.cpp:854
This functional is not possible in 2D!!   CAdjEulerSolver.cpp:862
Unsupported INLET_TYPE. INLET_TYPE CAdjEulerSolver.cpp:2978
The solution file … doesn’t match with the mesh file! … It could be empty lines at the end of the file.   CAdjEulerSolver.cpp:3906
There is no adjoint restart file   CAdjTurbSolver.cpp:109
The solution file … doesn’t match with the mesh file! … It could be empty lines at the end of the file.   CAdjTurbSolver.cpp:152
Unable to open SU2 restart file   CBaselineSolver.cpp:123
Error reading restart file.   CBaselineSolver.cpp:130
File … is not a binary SU2 restart file. … SU2 reads/writes binary restart files by default. … Note that backward compatibility for ASCII restart files is … possible with the READ_BINARY_RESTART option. READ_BINARY_RESTART CBaselineSolver.cpp:137
Unable to open SU2 restart file   CBaselineSolver.cpp:170
File … is not a binary SU2 restart file. … SU2 reads/writes binary restart files by default. … Note that backward compatibility for ASCII restart files is … possible with the READ_BINARY_RESTART option. READ_BINARY_RESTART CBaselineSolver.cpp:189
Unable to open SU2 restart file   CBaselineSolver.cpp:260
Error reading restart file.   CBaselineSolver.cpp:267
File … is a binary SU2 restart file, expected ASCII. … SU2 reads/writes binary restart files by default. … Note that backward compatibility for ASCII restart files is … possible with the READ_BINARY_RESTART option. READ_BINARY_RESTART CBaselineSolver.cpp:274
Unable to open SU2 restart file   CBaselineSolver.cpp:296
File … is a binary SU2 restart file, expected ASCII. … SU2 reads/writes binary restart files by default. … Note that backward compatibility for ASCII restart files is … possible with the READ_BINARY_RESTART option. READ_BINARY_RESTART CBaselineSolver.cpp:312
SU2 solution file … not found   CBaselineSolver.cpp:329
Unable to open SU2 restart file   CBaselineSolver_FEM.cpp:128
Error reading restart file.   CBaselineSolver_FEM.cpp:135
File … is not a binary SU2 restart file. … SU2 reads/writes binary restart files by default. … Note that backward compatibility for ASCII restart files is … possible with the READ_BINARY_RESTART option. READ_BINARY_RESTART CBaselineSolver_FEM.cpp:142
Unable to open SU2 restart file   CBaselineSolver_FEM.cpp:167
File … is not a binary SU2 restart file. … SU2 reads/writes binary restart files by default. … Note that backward compatibility for ASCII restart files is … possible with the READ_BINARY_RESTART option. READ_BINARY_RESTART CBaselineSolver_FEM.cpp:185
Unable to open SU2 restart file   CBaselineSolver_FEM.cpp:218
Error reading restart file.   CBaselineSolver_FEM.cpp:225
File … is a binary SU2 restart file, expected ASCII. … SU2 reads/writes binary restart files by default. … Note that backward compatibility for ASCII restart files is … possible with the READ_BINARY_RESTART option. READ_BINARY_RESTART CBaselineSolver_FEM.cpp:232
Unable to open SU2 restart file   CBaselineSolver_FEM.cpp:254
File … is a binary SU2 restart file, expected ASCII. … SU2 reads/writes binary restart files by default. … Note that backward compatibility for ASCII restart files is … possible with the READ_BINARY_RESTART option. READ_BINARY_RESTART CBaselineSolver_FEM.cpp:270
SU2 solution file … not found   CBaselineSolver_FEM.cpp:286
The solution file … doesn’t match with the mesh file! … It could be empty lines at the end of the file.   CBaselineSolver_FEM.cpp:376
Oops! The CDiscAdjSolver static array sizes are not large enough.   CDiscAdjSolver.cpp:82
Oops! The CEulerSolver static array sizes are not large enough.   CEulerSolver.cpp:364
Low-Mach correction is not supported with vectorization.   CEulerSolver.cpp:378
The numerical scheme + gas model in use do not … support vectorization.   CEulerSolver.cpp:386
Unknown fluid model.   CEulerSolver.cpp:914
Unable to open Actuator Disk Input File   CEulerSolver.cpp:4175
Unable to open Actuator Disk BEM Input File   CEulerSolver.cpp:4411
Invalid Riemann input!   CEulerSolver.cpp:5458
Invalid Riemann input!   CEulerSolver.cpp:5941
Invalid Giles input!   CEulerSolver.cpp:6980
Unsupported INLET_TYPE. INLET_TYPE CEulerSolver.cpp:7423
Invalid AVERAGE PROCESS input!   CEulerSolver.cpp:9564
Topology mode requires an element-based properties file.   CFEASolver.cpp:314
The properties file … doesn’t match with the mesh file! … It could be empty lines at the end of the file.   CFEASolver.cpp:388
There is no FEM prestretch reference file   CFEASolver.cpp:418
The solution file … doesn’t match with the mesh file! … It could be empty lines at the end of the file.   CFEASolver.cpp:465
There is no FEM reference geometry file!!   CFEASolver.cpp:491
The solution file … doesn’t match with the mesh file! … It could be empty lines at the end of the file.   CFEASolver.cpp:539
The solution file … doesn’t match with the mesh file! … It could be empty lines at the end of the file.   CFEASolver.cpp:3209
Unknown type of projection function   CFEASolver.cpp:3359
Rigid body motion only possible for CLASSICAL_RK4_EXPLICIT.   CFEM_DG_EulerSolver.cpp:3337
Only rigid body motion possible for DG-FEM solver at the moment.   CFEM_DG_EulerSolver.cpp:3510
Incompressible solver not implemented yet   CFEM_DG_EulerSolver.cpp:3830
BC not implemented.   CFEM_DG_EulerSolver.cpp:6346
SIZE_ARR_NORM is too small. Increase it or decrease ALIGNED_BYTES_MATMUL ALIGNED_BYTES_MATMUL CFEM_DG_EulerSolver.cpp:6509
SU2 has diverged. (NaN detected)   CFEM_DG_EulerSolver.cpp:7399
SU2 has diverged. (NaN detected)   CFEM_DG_EulerSolver.cpp:7436
Invalid Riemann input!   CFEM_DG_EulerSolver.cpp:8100
Implement customized boundary conditions here.   CFEM_DG_EulerSolver.cpp:8870
SIZE_ARR_NORM is too small. Increase it or decrease ALIGNED_BYTES_MATMUL ALIGNED_BYTES_MATMUL CFEM_DG_EulerSolver.cpp:8916
The solution file … doesn’t match with the mesh file! … It could be empty lines at the end of the file.   CFEM_DG_EulerSolver.cpp:9611
Unknown SGS model encountered   CFEM_DG_NSSolver.cpp:145
Incompressible solver not implemented yet   CFEM_DG_NSSolver.cpp:1281
Implement customized boundary conditions here.   CFEM_DG_NSSolver.cpp:6141
SIZE_ARR_NORM is too small. Increase it or decrease ALIGNED_BYTES_MATMUL ALIGNED_BYTES_MATMUL CFEM_DG_NSSolver.cpp:6453
The solution file … does not match with the mesh file! … This can be caused by empty lines at the end of the file.   CHeatSolver.cpp:258
Oops! The CIncEulerSolver static array sizes are not large enough.   CIncEulerSolver.cpp:251
Fluid model not implemented for incompressible solver.   CIncEulerSolver.cpp:361
Pressure Inlet is currently an unsupported INC_INLET_TYPE for pressure based solver. INC_INLET_TYPE CIncEulerSolver.cpp:2673
Unsupported INC_INLET_TYPE. INC_INLET_TYPE CIncEulerSolver.cpp:2734
Mass Flow Outlet is currently an unsupported INC_OUTLET_TYPE for pressure based solver. INC_OUTLET_TYPE CIncEulerSolver.cpp:2959
The requested outflow boundary condition has not yet been implemented for the pressure based poisson solver   CIncEulerSolver.cpp:3951
The requested boundary condition has not yet been implemented for the pressure based poisson solver   CIncEulerSolver.cpp:3995
Unknown type of boundary condition.   CIncNSSolver.cpp:459
Wall function treatment not implemented yet.   CIncNSSolver.cpp:469
Wall function treatment not implemented yet.   CIncNSSolver.cpp:633
Unknown CHT coupling method.   CIncNSSolver.cpp:706
It is not possible to compute grid velocity from boundary velocity for single zone problems. … MARKER_FLUID_LOAD should only be used for structural boundaries. MARKER_FLUID_LOAD CMeshSolver.cpp:573
Forced motions are not compatible with FSI simulations.   CMeshSolver.cpp:685
The solution file … doesn’t match with the mesh file! … It could be empty lines at the end of the file.   CMeshSolver.cpp:823
The solution file … doesn’t match with the mesh file! … It could be empty lines at the end of the file.   CMeshSolver.cpp:952
Oops! The CNEMOEulerSolver static array sizes are not large enough.   CNEMOEulerSolver.cpp:225
BC_INLET: Not operational in NEMO.   CNEMOEulerSolver.cpp:1627
Unsupported INLET_TYPE. INLET_TYPE CNEMOEulerSolver.cpp:1851
BC_HEATFLUX with catalytic wall: Not operational in NEMO.   CNEMONSSolver.cpp:356
NEED TO IMPLEMENT CATALYTIC BOUNDARIES IN HEATFLUX!!!   CNEMONSSolver.cpp:431
NEED TO TAKE A CLOSER LOOK AT THE JACOBIAN W/ IONIZATION IONIZATION CNEMONSSolver.cpp:544
Implicit not currently available for partially catalytic wall.   CNEMONSSolver.cpp:807
NEED TO TAKE A CLOSER LOOK AT THE JACOBIAN W/ IONIZATION IONIZATION CNEMONSSolver.cpp:864
Wall Functions not yet operational in NEMO.   CNEMONSSolver.cpp:1006
Wall function treatment not implemented yet   CNSSolver.cpp:464
Unknown CHT coupling method.   CNSSolver.cpp:624
Wall function treatment not implemented yet   CNSSolver.cpp:651
The definition of the momentum coefficient for an explicit solution is currently only an approximation and is not yet tested.   CPoissonSolver.cpp:211
HbyA is currently not supported for an explicit momentum solver.   CPoissonSolver.cpp:297
Requested type of outlet boundary condition not available   CPoissonSolver.cpp:477
Invalid boundary condition for flux correction   CPoissonSolver.cpp:484
The solution file … doesn’t match with the mesh file! … It could be empty lines at the end of the file.   CRadSolver.cpp:153
Unrecognized quantity for periodic communication.   CSolver.cpp:286
The NEMO solvers do not support rotational periodicity yet.   CSolver.cpp:379
Unrecognized quantity for periodic communication.   CSolver.cpp:1090
Unrecognized quantity for periodic communication.   CSolver.cpp:1432
Unrecognized quantity for point-to-point MPI comms.   CSolver.cpp:1540
Unrecognized quantity for point-to-point MPI comms.   CSolver.cpp:1708
Unrecognized quantity for point-to-point MPI comms.   CSolver.cpp:1875
SU2 has diverged (NaN detected).   CSolver.cpp:2178
SU2 has diverged (Residual > 10^20 detected).   CSolver.cpp:2184
There is no flow restart file   CSolver.cpp:2853
The solution file … doesn’t match with the mesh file! … It could be empty lines at the end of the file.   CSolver.cpp:2891
There is no flow restart file   CSolver.cpp:2918
The solution file … doesn’t match with the mesh file! … It could be empty lines at the end of the file.   CSolver.cpp:2959
Unable to open SU2 restart file   CSolver.cpp:3011
Error reading restart file.   CSolver.cpp:3018
File … is a binary SU2 restart file, expected ASCII. … SU2 reads/writes binary restart files by default. … Note that backward compatibility for ASCII restart files is … possible with the READ_BINARY_RESTART option. READ_BINARY_RESTART CSolver.cpp:3025
SU2 ASCII restart file … not found.   CSolver.cpp:3047
File … is a binary SU2 restart file, expected ASCII. … SU2 reads/writes binary restart files by default. … Note that backward compatibility for ASCII restart files is … possible with the READ_BINARY_RESTART option. READ_BINARY_RESTART CSolver.cpp:3064
SU2 ASCII restart file … not found.   CSolver.cpp:3081
Restart file does not seem to be a CSV file.   CSolver.cpp:3093
Unable to open SU2 restart file   CSolver.cpp:3162
Error reading restart file.   CSolver.cpp:3169
File … is not a binary SU2 restart file. … SU2 reads/writes binary restart files by default. … Note that backward compatibility for ASCII restart files is … possible with the READ_BINARY_RESTART option. READ_BINARY_RESTART CSolver.cpp:3176
Error reading restart file.   CSolver.cpp:3199
Error reading restart file.   CSolver.cpp:3218
Unable to open SU2 restart file   CSolver.cpp:3238
File … is not a binary SU2 restart file. … SU2 reads/writes binary restart files by default. … Note that backward compatibility for ASCII restart files is … possible with the READ_BINARY_RESTART option. READ_BINARY_RESTART CSolver.cpp:3255
Number of ranks must be multiple of 2.   CSolver.cpp:3403
Cannot interpolate the restart file for FEM problems.   CSolver.cpp:3406
Unsupported type of inlet.   CSolver.cpp:3878
Unsupported INLET_TYPE. INLET_TYPE CSolver.cpp:3900
Unsupported INC_INLET_TYPE. INC_INLET_TYPE CSolver.cpp:3913
Unknown type of interpolation function for inlets.   CSolver.cpp:4060
Prescribed inlet data does not match markers within tolerance.   CSolver.cpp:4201
The solution file … doesn’t match with the mesh file! … It could be empty lines at the end of the file.   CSolver.cpp:4514
SU2 was not compiled with libROM support.   CSolver.cpp:4605
FEM RANS not available   CSolverFactory.cpp:202
Adjoint FEM RANS not available   CSolverFactory.cpp:213
No proper allocation found for requested sub solver   CSolverFactory.cpp:348
Trying to create TurbSolver container but TURB_MODEL=NONE.   CSolverFactory.cpp:377
No continuous adjoint heat solver available.   CSolverFactory.cpp:444
Requested DG solver not found   CSolverFactory.cpp:487
Flow solver not found   CSolverFactory.cpp:520
Increase static array size MAXNVAR for CSpeciesVariable and proceed.   CSpeciesSolver.cpp:111
The solution file … doesn’t match with the mesh file! … It could be empty lines at the end of the file.   CSpeciesSolver.cpp:264
The solution file … does not match with the mesh file! … This can be caused by empty lines at the end of the file.   CTransLMSolver.cpp:557
The solution file … does not match with the mesh file! … This can be caused by empty lines at the end of the file.   CTurbSolver.cpp:158

SU2_CFD/src/variables (1)

Message Options Code
Variables cannot be constructed inside a parallel region.   CVariable.cpp:42

SU2_DEF/src/drivers (6)

Message Options Code
Unrecognized mesh_out format specified!   CDeformationDriver.cpp:512
An adjoint solver (discrete or continuous) was not specified in the configuration file.   CDiscAdjDeformationDriver.cpp:119
The projection using finite differences currently only supports a fixed direction of movement for FFD … points.   CDiscAdjDeformationDriver.cpp:410
The input grid doesn’t have the entire FFD information!   CDiscAdjDeformationDriver.cpp:446
Unsupported operation modus for the Sobolev Smoothing Solver.   CDiscAdjDeformationDriver.cpp:917
Unsupported operation modus for the Sobolev Smoothing Solver.   CDiscAdjDeformationDriver.cpp:979

SU2_GEO/src (2)

Message Options Code
The input grid doesn’t have the entire FFD information!   SU2_GEO.cpp:780
The finite difference steps is zero!!   SU2_GEO.cpp:1012


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