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An error has occurred in cfx5solve:The ANSYS CFX solver exited with return code1

- May 22, 2023 at 3:28 pm
  
  Stefano Chieti
  Subscriber
  
  Hello,
  I'm suffering with this solver error:
  "An error has occurred in cfx5solve: The ANSYS CFX solver exited with return code 1. No results file has been created"
  Same goes for parallel solution:
  " The ANSYS CFX partitioner exited with return code 1."
  
  This is an unexpected problem, because it follows from a project which was previously solved around an year ago.
  I wanted to launch it again with different inputs but there's no way it can get solved.
  I tought that maybe it could be a problem of directory path which changed in time. I tried to recreate from scratch the project in another .wbpj, literally anything was equal, but I still get these errors.
  In the following I share the .out file I obtain from the monitor, which doesn't report any relevant error:
  This run of the CFX GEOMETRY LICENSING PATCH 2021 R1 SP3 Solver started
  at 17:14:27 on 22 May 2023 -
  (intel_xeon64.sse2_winnt) using the command:
  
  "C:\Program Files\ANSYS Inc\v211\CFX\bin\perllib\cfx5solve.pl" -batch
  -ccl runInput.ccl -fullname CFX_001
  
  GEOMETRY LICENSING PATCH 2021 R1 SP3
  
  Point Releases and Patches installed:
  ANSYS, Inc. Products 2021 R1
  SpaceClaim 2021 R1
  Autodyn 2021 R1
  CFD-Post only 2021 R1
  CFX (includes CFD-Post) 2021 R1
  FENSAP-ICE 2021 R1
  Fluent (includes CFD-Post) 2021 R1
  Forte (includes EnSight) 2021 R1
  Polyflow (includes CFD-Post) 2021 R1
  TurboGrid 2021 R1
  Aqwa 2021 R1
  Customization Files for User Programmable Features 2021 R1
  Mechanical Products 2021 R1
  Icepak (includes CFD-Post) 2021 R1
  Remote Solve Manager Standalone Services 2021 R1
  Viewer 2021 R1
  ACIS Geometry Interface 2021 R1
  AutoCAD Geometry Interface 2021 R1
  Catia, Version 4 Geometry Interface 2021 R1
  Catia, Version 5 Geometry Interface 2021 R1
  Catia, Version 6 Geometry Interface 2021 R1
  Creo Elements/Direct Modeling Geometry Interface 2021 R1
  Creo Parametric Geometry Interface 2021 R1
  Inventor Geometry Interface 2021 R1
  JTOpen Geometry Interface 2021 R1
  NX Geometry Interface 2021 R1
  Parasolid Geometry Interface 2021 R1
  Solid Edge Geometry Interface 2021 R1
  SOLIDWORKS Geometry Interface 2021 R1
  ANSYS, Inc. License Manager 2021 R1
  Discovery 2021 R1.6
  Geometry Licensing Patch 2021 R1 SP3
  
  Setting up CFX Solver run ...
  
  +--------------------------------------------------------------------+
  | |
  | CFX Command Language for Run |
  | |
  +--------------------------------------------------------------------+
  
  LIBRARY:
  MATERIAL: Water
  Material Description = Water (liquid)
  Material Group = Water Data, Constant Property Liquids
  Option = Pure Substance
  Thermodynamic State = Liquid
  PROPERTIES:
  Option = General Material
  EQUATION OF STATE:
  Density = 997.0 [kg m^-3]
  Molar Mass = 18.02 [kg kmol^-1]
  Option = Value
  END
  SPECIFIC HEAT CAPACITY:
  Option = Value
  Specific Heat Capacity = 4181.7 [J kg^-1 K^-1]
  Specific Heat Type = Constant Pressure
  END
  REFERENCE STATE:
  Option = Specified Point
  Reference Pressure = 1 [atm]
  Reference Specific Enthalpy = 0.0 [J/kg]
  Reference Specific Entropy = 0.0 [J/kg/K]
  Reference Temperature = 25 [C]
  END
  DYNAMIC VISCOSITY:
  Dynamic Viscosity = 8.899E-4 [kg m^-1 s^-1]
  Option = Value
  END
  THERMAL CONDUCTIVITY:
  Option = Value
  Thermal Conductivity = 0.6069 [W m^-1 K^-1]
  END
  ABSORPTION COEFFICIENT:
  Absorption Coefficient = 1.0 [m^-1]
  Option = Value
  END
  SCATTERING COEFFICIENT:
  Option = Value
  Scattering Coefficient = 0.0 [m^-1]
  END
  REFRACTIVE INDEX:
  Option = Value
  Refractive Index = 1.0 [m m^-1]
  END
  THERMAL EXPANSIVITY:
  Option = Value
  Thermal Expansivity = 2.57E-04 [K^-1]
  END
  END
  END
  END
  FLOW: Flow Analysis 1
  SOLUTION UNITS:
  Angle Units = [rad]
  Length Units = [m]
  Mass Units = [kg]
  Solid Angle Units = [sr]
  Temperature Units = [K]
  Time Units = [s]
  END
  ANALYSIS TYPE:
  Option = Steady State
  EXTERNAL SOLVER COUPLING:
  Option = None
  END
  END
  DOMAIN: CONVERGENT
  Coord Frame = Coord 0
  Domain Type = Fluid
  Location = B1934
  BOUNDARY: CONVERGENT Default
  Boundary Type = WALL
  Location = F1935.1934
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  BOUNDARY: Interface CONVERGENT VOLUTE Side 1
  Boundary Type = INTERFACE
  Location = F1894.1934
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: OUTLET
  Boundary Type = OUTLET
  Location = F1936.1934
  BOUNDARY CONDITIONS:
  FLOW REGIME:
  Option = Subsonic
  END
  MASS AND MOMENTUM:
  Mass Flow Rate = 0.63 [kg s^-1]
  Mass Flow Rate Area = As Specified
  Option = Mass Flow Rate
  END
  END
  END
  DOMAIN MODELS:
  BUOYANCY MODEL:
  Option = Non Buoyant
  END
  DOMAIN MOTION:
  Option = Stationary
  END
  MESH DEFORMATION:
  Option = None
  END
  REFERENCE PRESSURE:
  Reference Pressure = 1 [atm]
  END
  END
  FLUID DEFINITION: Fluid 1
  Material = Water
  Option = Material Library
  MORPHOLOGY:
  Option = Continuous Fluid
  END
  END
  FLUID MODELS:
  COMBUSTION MODEL:
  Option = None
  END
  HEAT TRANSFER MODEL:
  Option = None
  END
  THERMAL RADIATION MODEL:
  Option = None
  END
  TURBULENCE MODEL:
  Option = SST
  END
  TURBULENT WALL FUNCTIONS:
  Option = Automatic
  END
  END
  END
  DOMAIN: DUCTS
  Coord Frame = Coord 0
  Domain Type = Fluid
  Location = B212,B213,B30,B31
  BOUNDARY: DUCTS Default
  Boundary Type = WALL
  Location = \
  F1916.30,F1917.30,F1920.31,F1921.31,F1924.212,F1925.212,F1928.213,F19\
  29.213,F25.212,F26.31,F27.213,F28.30,F355.212,F356.212,F357.212,F358.\
  212,F359.213,F360.213,F361.213,F362.213,F370.213,F371.213,F372.213,F3\
  73.213,F374.213,F375.213,F376.213,F377.213,F378.212,F379.212,F380.212\
  ,F381.212,F382.212,F383.212,F384.212,F385.212,F386.30,F387.30,F388.30\
  ,F389.30,F390.30,F391.30,F392.30,F393.30,F394.31,F395.31,F396.31,F397\
  .31,F398.31,F399.31,F400.31,F401.31,F402.31,F403.31,F404.31,F405.31,F\
  408.30,F409.30,F410.30,F411.30
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  BOUNDARY: Interface DUCTS ROTATINGCOOLINGDX Xdir Side 1
  Boundary Type = INTERFACE
  Location = \
  F205.212,F206.31,F207.213,F208.30,F21.30,F22.213,F23.31,F24.212
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface DUCTS ROTATINGCOOLINGDX Zdir Side 1
  Boundary Type = INTERFACE
  Location = F42.30,F43.213,F44.31,F45.212
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  DOMAIN MODELS:
  BUOYANCY MODEL:
  Option = Non Buoyant
  END
  DOMAIN MOTION:
  Option = Stationary
  END
  MESH DEFORMATION:
  Option = None
  END
  REFERENCE PRESSURE:
  Reference Pressure = 1 [atm]
  END
  END
  FLUID DEFINITION: Fluid 1
  Material = Water
  Option = Material Library
  MORPHOLOGY:
  Option = Continuous Fluid
  END
  END
  FLUID MODELS:
  COMBUSTION MODEL:
  Option = None
  END
  HEAT TRANSFER MODEL:
  Option = None
  END
  THERMAL RADIATION MODEL:
  Option = None
  END
  TURBULENCE MODEL:
  Option = SST
  END
  TURBULENT WALL FUNCTIONS:
  Option = Automatic
  END
  END
  END
  DOMAIN: EULERIAN
  Coord Frame = Coord 0
  Domain Type = Fluid
  Location = B32
  BOUNDARY: EULERIAN Default
  Boundary Type = WALL
  Location = F33.32
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  BOUNDARY: INLET
  Boundary Type = INLET
  Location = F34.32
  BOUNDARY CONDITIONS:
  FLOW DIRECTION:
  Option = Normal to Boundary Condition
  END
  FLOW REGIME:
  Option = Subsonic
  END
  MASS AND MOMENTUM:
  Option = Total Pressure
  Relative Pressure = 185 [kPa]
  END
  TURBULENCE:
  Option = Medium Intensity and Eddy Viscosity Ratio
  END
  END
  END
  BOUNDARY: Interface EULERIAN INTAKE Side 1
  Boundary Type = INTERFACE
  Location = F197.32
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  DOMAIN MODELS:
  BUOYANCY MODEL:
  Option = Non Buoyant
  END
  DOMAIN MOTION:
  Option = Stationary
  END
  MESH DEFORMATION:
  Option = None
  END
  REFERENCE PRESSURE:
  Reference Pressure = 1 [atm]
  END
  END
  FLUID DEFINITION: Fluid 1
  Material = Water
  Option = Material Library
  MORPHOLOGY:
  Option = Continuous Fluid
  END
  END
  FLUID MODELS:
  COMBUSTION MODEL:
  Option = None
  END
  HEAT TRANSFER MODEL:
  Option = None
  END
  THERMAL RADIATION MODEL:
  Option = None
  END
  TURBULENCE MODEL:
  Option = SST
  END
  TURBULENT WALL FUNCTIONS:
  Option = Automatic
  END
  END
  END
  DOMAIN: INTAKE
  Coord Frame = Coord 0
  Domain Type = Fluid
  Location = B78
  BOUNDARY: INTAKE Default
  Boundary Type = WALL
  Location = F1915.78,F523.78
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  BOUNDARY: Interface EULERIAN INTAKE Side 2
  Boundary Type = INTERFACE
  Location = F197.78
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface INTAKE INTAKEMAZE Side 1
  Boundary Type = INTERFACE
  Location = F83.78
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  DOMAIN MODELS:
  BUOYANCY MODEL:
  Option = Non Buoyant
  END
  DOMAIN MOTION:
  Option = Stationary
  END
  MESH DEFORMATION:
  Option = None
  END
  REFERENCE PRESSURE:
  Reference Pressure = 1 [atm]
  END
  END
  FLUID DEFINITION: Fluid 1
  Material = Water
  Option = Material Library
  MORPHOLOGY:
  Option = Continuous Fluid
  END
  END
  FLUID MODELS:
  COMBUSTION MODEL:
  Option = None
  END
  HEAT TRANSFER MODEL:
  Option = None
  END
  THERMAL RADIATION MODEL:
  Option = None
  END
  TURBULENCE MODEL:
  Option = SST
  END
  TURBULENT WALL FUNCTIONS:
  Option = Automatic
  END
  END
  END
  DOMAIN: INTAKE MAZE
  Coord Frame = Coord 0
  Domain Type = Fluid
  Location = B198
  BOUNDARY: INTAKE MAZE Default
  Boundary Type = WALL
  Location = \
  F515.198,F516.198,F517.198,F518.198,F519.198,F520.198,F521.198,F522.1\
  98,F967.198,F972.198,F974.198,F975.198,F977.198,F978.198,F979.198,F98\
  0.198,F981.198
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  BOUNDARY: Interface INTAKE INTAKEMAZE Side 2
  Boundary Type = INTERFACE
  Location = F83.198
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface INTAKEMAZE ROTATINGIMPELLER Side 1
  Boundary Type = INTERFACE
  Location = F223.198,F82.198
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  DOMAIN MODELS:
  BUOYANCY MODEL:
  Option = Non Buoyant
  END
  DOMAIN MOTION:
  Option = Stationary
  END
  MESH DEFORMATION:
  Option = None
  END
  REFERENCE PRESSURE:
  Reference Pressure = 1 [atm]
  END
  END
  FLUID DEFINITION: Fluid 1
  Material = Water
  Option = Material Library
  MORPHOLOGY:
  Option = Continuous Fluid
  END
  END
  FLUID MODELS:
  COMBUSTION MODEL:
  Option = None
  END
  HEAT TRANSFER MODEL:
  Option = None
  END
  THERMAL RADIATION MODEL:
  Option = None
  END
  TURBULENCE MODEL:
  Option = SST
  END
  TURBULENT WALL FUNCTIONS:
  Option = Automatic
  END
  END
  END
  DOMAIN: ROTATING BOLT
  Coord Frame = Coord 0
  Domain Type = Fluid
  Location = B264
  BOUNDARY: Interface ROTATINGBOLT ROTATINGIMPELLER Side 1
  Boundary Type = INTERFACE
  Location = F276.264,F277.264,F278.264,F279.264
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface ROTATINGBOLT ROTATINGSHAFT Side 1
  Boundary Type = INTERFACE
  Location = F249.264
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: ROTATING BOLT Default
  Boundary Type = WALL
  Frame Type = Rotating
  Location = \
  F1006.264,F1007.264,F1008.264,F1162.264,F1163.264,F247.264,F252.264,F\
  280.264,F305.264,F306.264,F307.264,F308.264,F942.264,F943.264,F957.26\
  4,F983.264
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  DOMAIN MODELS:
  BUOYANCY MODEL:
  Option = Non Buoyant
  END
  DOMAIN MOTION:
  Alternate Rotation Model = On
  Angular Velocity = -1256.64 [radian s^-1]
  Option = Rotating
  AXIS DEFINITION:
  Option = Coordinate Axis
  Rotation Axis = Coord 0.3
  END
  END
  MESH DEFORMATION:
  Option = None
  END
  REFERENCE PRESSURE:
  Reference Pressure = 1 [atm]
  END
  END
  FLUID DEFINITION: Fluid 1
  Material = Water
  Option = Material Library
  MORPHOLOGY:
  Option = Continuous Fluid
  END
  END
  FLUID MODELS:
  COMBUSTION MODEL:
  Option = None
  END
  HEAT TRANSFER MODEL:
  Option = None
  END
  THERMAL RADIATION MODEL:
  Option = None
  END
  TURBULENCE MODEL:
  Option = SST
  END
  TURBULENT WALL FUNCTIONS:
  Option = Automatic
  END
  END
  END
  DOMAIN: ROTATING COOLING CENTER
  Coord Frame = Coord 0
  Domain Type = Fluid
  Location = B310
  BOUNDARY: Interface ROTATINGCOOLINGCENTER ROTATINGCOOLINGDX Side 1
  Boundary Type = INTERFACE
  Location = F320.310
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface ROTATINGCOOLINGSX ROTATINGCOOLINGCENTER Side 2
  Boundary Type = INTERFACE
  Location = F340.310
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: ROTATING COOLING CENTER Default
  Boundary Type = WALL
  Frame Type = Rotating
  Location = F323.310
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  BOUNDARY: StaticWalls COOLING CENTER
  Boundary Type = WALL
  Frame Type = Rotating
  Location = F321.310
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  DOMAIN MODELS:
  BUOYANCY MODEL:
  Option = Non Buoyant
  END
  DOMAIN MOTION:
  Alternate Rotation Model = On
  Angular Velocity = -1256.64 [radian s^-1]
  Option = Rotating
  AXIS DEFINITION:
  Option = Coordinate Axis
  Rotation Axis = Coord 0.3
  END
  END
  MESH DEFORMATION:
  Option = None
  END
  REFERENCE PRESSURE:
  Reference Pressure = 1 [atm]
  END
  END
  FLUID DEFINITION: Fluid 1
  Material = Water
  Option = Material Library
  MORPHOLOGY:
  Option = Continuous Fluid
  END
  END
  FLUID MODELS:
  COMBUSTION MODEL:
  Option = None
  END
  HEAT TRANSFER MODEL:
  Option = None
  END
  THERMAL RADIATION MODEL:
  Option = None
  END
  TURBULENCE MODEL:
  Option = SST
  END
  TURBULENT WALL FUNCTIONS:
  Option = Automatic
  END
  END
  END
  DOMAIN: ROTATING COOLING DX
  Coord Frame = Coord 0
  Domain Type = Fluid
  Location = B327
  BOUNDARY: Interface DUCTS ROTATINGCOOLINGDX Xdir Side 2
  Boundary Type = INTERFACE
  Location = \
  F205.327,F206.327,F207.327,F208.327,F21.327,F22.327,F23.327,F24.327
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface DUCTS ROTATINGCOOLINGDX Zdir Side 2
  Boundary Type = INTERFACE
  Location = F42.327,F43.327,F44.327,F45.327
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface ROTATINGCOOLINGCENTER ROTATINGCOOLINGDX Side 2
  Boundary Type = INTERFACE
  Location = F320.327
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface ROTATINGCOOLINGDX ROTATINGSHAFT Side 1
  Boundary Type = INTERFACE
  Location = F265.327
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: ROTATING COOLING DX Default
  Boundary Type = WALL
  Frame Type = Rotating
  Location = \
  F10.327,F1000.327,F1001.327,F1002.327,F1003.327,F1004.327,F1009.327,F\
  1010.327,F1011.327,F1012.327,F1014.327,F1017.327,F1018.327,F1019.327,\
  F1020.327,F1021.327,F1022.327,F1023.327,F1024.327,F1025.327,F1026.327\
  ,F1027.327,F1028.327,F1040.327,F1041.327,F1042.327,F1043.327,F1044.32\
  7,F1045.327,F1046.327,F1047.327,F1048.327,F1049.327,F1050.327,F1051.3\
  27,F1052.327,F1053.327,F1054.327,F1055.327,F1056.327,F1057.327,F1058.\
  327,F1059.327,F1060.327,F1061.327,F1062.327,F1063.327,F1064.327,F1065\
  .327,F1066.327,F1067.327,F1068.327,F1069.327,F1070.327,F1071.327,F107\
  2.327,F1073.327,F1074.327,F1075.327,F1076.327,F1077.327,F1078.327,F10\
  79.327,F1080.327,F1081.327,F1082.327,F1083.327,F1084.327,F1085.327,F1\
  086.327,F1087.327,F1088.327,F1089.327,F1090.327,F1091.327,F1092.327,F\
  1093.327,F1094.327,F1095.327,F1096.327,F1097.327,F1098.327,F1099.327,\
  F11.327,F1100.327,F1101.327,F1102.327,F1103.327,F1104.327,F1105.327,F\
  1106.327,F1107.327,F1108.327,F1109.327,F1110.327,F1111.327,F1112.327,\
  F1113.327,F1114.327,F1115.327,F1116.327,F1117.327,F1118.327,F1119.327\
  ,F1120.327,F1121.327,F1122.327,F1123.327,F1124.327,F1125.327,F1126.32\
  7,F1127.327,F1128.327,F1129.327,F1130.327,F1131.327,F1132.327,F1133.3\
  27,F1134.327,F1135.327,F1136.327,F1137.327,F1138.327,F1139.327,F1140.\
  327,F1141.327,F1142.327,F1143.327,F1144.327,F1145.327,F1146.327,F1147\
  .327,F1148.327,F1149.327,F1150.327,F1151.327,F1152.327,F1153.327,F115\
  4.327,F1155.327,F1156.327,F1175.327,F1176.327,F1177.327,F1178.327,F11\
  79.327,F1180.327,F1181.327,F290.327,F324.327,F4.327,F40.327,F47.327,F\
  48.327,F49.327,F5.327,F50.327,F51.327,F52.327,F53.327,F54.327,F55.327\
  ,F56.327,F57.327,F58.327,F59.327,F6.327,F60.327,F61.327,F7.327,F8.327\
  ,F9.327,F937.327,F938.327,F939.327,F986.327,F997.327,F998.327,F999.327
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  BOUNDARY: StaticWalls COOLINGDX
  Boundary Type = WALL
  Frame Type = Rotating
  Location = \
  F219.327,F209.327,F1879.327,F266.327,F322.327,F346.327,F363.327,F365.\
  327,F1880.327,F364.327,F366.327,F367.327,F368.327,F369.327,F406.327,F\
  407.327,F41.327,F412.327,F413.327,F414.327,F415.327,F416.327,F417.327\
  ,F46.327,F345.327
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  DOMAIN MODELS:
  BUOYANCY MODEL:
  Option = Non Buoyant
  END
  DOMAIN MOTION:
  Alternate Rotation Model = On
  Angular Velocity = -1256.64 [radian s^-1]
  Option = Rotating
  AXIS DEFINITION:
  Option = Coordinate Axis
  Rotation Axis = Coord 0.3
  END
  END
  MESH DEFORMATION:
  Option = None
  END
  REFERENCE PRESSURE:
  Reference Pressure = 1 [atm]
  END
  END
  FLUID DEFINITION: Fluid 1
  Material = Water
  Option = Material Library
  MORPHOLOGY:
  Option = Continuous Fluid
  END
  END
  FLUID MODELS:
  COMBUSTION MODEL:
  Option = None
  END
  HEAT TRANSFER MODEL:
  Option = None
  END
  THERMAL RADIATION MODEL:
  Option = None
  END
  TURBULENCE MODEL:
  Option = SST
  END
  TURBULENT WALL FUNCTIONS:
  Option = Automatic
  END
  END
  END
  DOMAIN: ROTATING COOLING SX
  Coord Frame = Coord 0
  Domain Type = Fluid
  Location = B275
  BOUNDARY: Interface ROTATINGCOOLINGSX ROTATINGCOOLINGCENTER Side 1
  Boundary Type = INTERFACE
  Location = F340.275
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface ROTATINGSPILLAGE ROTATINGCOOLINGSX Side 2
  Boundary Type = INTERFACE
  Location = F248.275
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface SPILLAGEDX ROTATINGCOOLINGSX Side 2
  Boundary Type = INTERFACE
  Location = F220.275
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: ROTATING COOLING SX Default
  Boundary Type = WALL
  Frame Type = Rotating
  Location = \
  F1013.275,F1165.275,F1166.275,F1167.275,F1168.275,F1169.275,F1170.275\
  ,F1171.275,F1172.275,F1173.275,F1174.275,F251.275,F342.275,F39.275,F9\
  84.275,F987.275,F988.275,F989.275,F990.275,F991.275,F992.275,F993.275\
  ,F994.275,F995.275,F996.275
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  BOUNDARY: StaticWalls COOLING SX
  Boundary Type = WALL
  Frame Type = Rotating
  Location = F341.275,F289.275,F1891.275
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  DOMAIN MODELS:
  BUOYANCY MODEL:
  Option = Non Buoyant
  END
  DOMAIN MOTION:
  Alternate Rotation Model = On
  Angular Velocity = -1256.64 [radian s^-1]
  Option = Rotating
  AXIS DEFINITION:
  Option = Coordinate Axis
  Rotation Axis = Coord 0.3
  END
  END
  MESH DEFORMATION:
  Option = None
  END
  REFERENCE PRESSURE:
  Reference Pressure = 1 [atm]
  END
  END
  FLUID DEFINITION: Fluid 1
  Material = Water
  Option = Material Library
  MORPHOLOGY:
  Option = Continuous Fluid
  END
  END
  FLUID MODELS:
  COMBUSTION MODEL:
  Option = None
  END
  HEAT TRANSFER MODEL:
  Option = None
  END
  THERMAL RADIATION MODEL:
  Option = None
  END
  TURBULENCE MODEL:
  Option = SST
  END
  TURBULENT WALL FUNCTIONS:
  Option = Automatic
  END
  END
  END
  DOMAIN: ROTATING IMPELLER
  Coord Frame = Coord 0
  Domain Type = Fluid
  Location = B263
  BOUNDARY: Interface INTAKEMAZE ROTATINGIMPELLER Side 2
  Boundary Type = INTERFACE
  Location = F223.263,F82.263
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface ROTATINGBOLT ROTATINGIMPELLER Side 2
  Boundary Type = INTERFACE
  Location = F276.263,F277.263,F278.263,F279.263
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface ROTATINGIMPELLER ROTATINGSPILLAGE Side 1
  Boundary Type = INTERFACE
  Location = F287.263
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface ROTATINGIMPELLER VOLUTE Side 1
  Boundary Type = INTERFACE
  Location = F1876.263
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: ROTATING IMPELLER Default
  Boundary Type = WALL
  Frame Type = Rotating
  Location = \
  F100.263,F101.263,F102.263,F103.263,F104.263,F105.263,F106.263,F107.2\
  63,F108.263,F109.263,F110.263,F111.263,F112.263,F113.263,F114.263,F11\
  5.263,F1157.263,F1158.263,F1159.263,F116.263,F1160.263,F1161.263,F116\
  4.263,F117.263,F118.263,F119.263,F120.263,F121.263,F122.263,F123.263,\
  F124.263,F125.263,F87.263,F944.263,F945.263,F946.263,F947.263,F948.26\
  3,F949.263,F95.263,F950.263,F951.263,F952.263,F953.263,F954.263,F956.\
  263,F959.263,F96.263,F960.263,F961.263,F962.263,F963.263,F964.263,F96\
  5.263,F966.263,F97.263,F98.263,F99.263
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  BOUNDARY: StaticWalls IMPELLER
  Boundary Type = WALL
  Frame Type = Rotating
  Location = \
  F1901.263,F1902.263,F509.263,F508.263,F510.263,F511.263,F512.263,F513\
  .263,F514.263,F88.263,F1900.263,F221.263,F222.263,F217.263,F260.263,F\
  968.263,F969.263,F970.263,F971.263,F973.263,F976.263,F1893.263
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  DOMAIN MODELS:
  BUOYANCY MODEL:
  Option = Non Buoyant
  END
  DOMAIN MOTION:
  Alternate Rotation Model = On
  Angular Velocity = -1256.64 [radian s^-1]
  Option = Rotating
  AXIS DEFINITION:
  Option = Coordinate Axis
  Rotation Axis = Coord 0.3
  END
  END
  MESH DEFORMATION:
  Option = None
  END
  REFERENCE PRESSURE:
  Reference Pressure = 1 [atm]
  END
  END
  FLUID DEFINITION: Fluid 1
  Material = Water
  Option = Material Library
  MORPHOLOGY:
  Option = Continuous Fluid
  END
  END
  FLUID MODELS:
  COMBUSTION MODEL:
  Option = None
  END
  HEAT TRANSFER MODEL:
  Option = None
  END
  THERMAL RADIATION MODEL:
  Option = None
  END
  TURBULENCE MODEL:
  Option = SST
  END
  TURBULENT WALL FUNCTIONS:
  Option = Automatic
  END
  END
  END
  DOMAIN: ROTATING SHAFT
  Coord Frame = Coord 0
  Domain Type = Fluid
  Location = B258
  BOUNDARY: Interface ROTATINGBOLT ROTATINGSHAFT Side 2
  Boundary Type = INTERFACE
  Location = F249.258
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface ROTATINGCOOLINGDX ROTATINGSHAFT Side 2
  Boundary Type = INTERFACE
  Location = F265.258
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: ROTATING SHAFT Default
  Boundary Type = WALL
  Frame Type = Rotating
  Location = \
  F1005.258,F1029.258,F1030.258,F1031.258,F1032.258,F1033.258,F1034.258\
  ,F1035.258,F1036.258,F1037.258,F1038.258,F1039.258,F253.258
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  DOMAIN MODELS:
  BUOYANCY MODEL:
  Option = Non Buoyant
  END
  DOMAIN MOTION:
  Alternate Rotation Model = On
  Angular Velocity = -1256.64 [radian s^-1]
  Option = Rotating
  AXIS DEFINITION:
  Option = Coordinate Axis
  Rotation Axis = Coord 0.3
  END
  END
  MESH DEFORMATION:
  Option = None
  END
  REFERENCE PRESSURE:
  Reference Pressure = 1 [atm]
  END
  END
  FLUID DEFINITION: Fluid 1
  Material = Water
  Option = Material Library
  MORPHOLOGY:
  Option = Continuous Fluid
  END
  END
  FLUID MODELS:
  COMBUSTION MODEL:
  Option = None
  END
  HEAT TRANSFER MODEL:
  Option = None
  END
  THERMAL RADIATION MODEL:
  Option = None
  END
  TURBULENCE MODEL:
  Option = SST
  END
  TURBULENT WALL FUNCTIONS:
  Option = Automatic
  END
  END
  END
  DOMAIN: ROTATING SPILLAGE
  Coord Frame = Coord 0
  Domain Type = Fluid
  Location = B257
  BOUNDARY: Interface ROTATINGIMPELLER ROTATINGSPILLAGE Side 2
  Boundary Type = INTERFACE
  Location = F287.257
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface ROTATINGSPILLAGE ROTATINGCOOLINGSX Side 1
  Boundary Type = INTERFACE
  Location = F248.257
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface ROTATINGSPILLAGE SPILLAGESX Side 1
  Boundary Type = INTERFACE
  Location = F299.257,F300.257,F301.257,F302.257,F303.257
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface SPILLAGECENTER ROTATINGSPILLAGE Side 2
  Boundary Type = INTERFACE
  Location = F1881.257
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: ROTATING SPILLAGE Default
  Boundary Type = WALL
  Frame Type = Rotating
  Location = \
  F1015.257,F1016.257,F250.257,F286.257,F304.257,F91.257,F92.257,F93.25\
  7,F94.257,F940.257,F941.257,F958.257,F982.257,F985.257
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  BOUNDARY: StaticWalls SPILLAGE
  Boundary Type = WALL
  Frame Type = Rotating
  Location = \
  F1882.257,F309.257,F422.257,F423.257,F424.257,F425.257,F426.257,F427.\
  257,F428.257,F259.257,F429.257,F430.257,F431.257,F432.257,F433.257,F4\
  50.257,F483.257,F484.257,F485.257,F486.257,F487.257,F488.257,F90.257,\
  F218.257
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  DOMAIN MODELS:
  BUOYANCY MODEL:
  Option = Non Buoyant
  END
  DOMAIN MOTION:
  Alternate Rotation Model = On
  Angular Velocity = -1256.64 [radian s^-1]
  Option = Rotating
  AXIS DEFINITION:
  Option = Coordinate Axis
  Rotation Axis = Coord 0.3
  END
  END
  MESH DEFORMATION:
  Option = None
  END
  REFERENCE PRESSURE:
  Reference Pressure = 1 [atm]
  END
  END
  FLUID DEFINITION: Fluid 1
  Material = Water
  Option = Material Library
  MORPHOLOGY:
  Option = Continuous Fluid
  END
  END
  FLUID MODELS:
  COMBUSTION MODEL:
  Option = None
  END
  HEAT TRANSFER MODEL:
  Option = None
  END
  THERMAL RADIATION MODEL:
  Option = None
  END
  TURBULENCE MODEL:
  Option = SST
  END
  TURBULENT WALL FUNCTIONS:
  Option = Automatic
  END
  END
  END
  DOMAIN: SPILLAGE CENTER
  Coord Frame = Coord 0
  Domain Type = Fluid
  Location = B84
  BOUNDARY: Interface SPILLAGECENTER ROTATINGSPILLAGE Side 1
  Boundary Type = INTERFACE
  Location = F1881.84
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface SPILLAGECENTER SPILLAGEDX Side 1
  Boundary Type = INTERFACE
  Location = F328.84
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface SPILLAGECENTER SPILLAGESX Side 1
  Boundary Type = INTERFACE
  Location = F312.84
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface SPILLAGEVOLUTE SPILLAGECENTER Side 2
  Boundary Type = INTERFACE
  Location = F311.84
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: SPILLAGE CENTER Default
  Boundary Type = WALL
  Location = \
  F314.84,F316.84,F329.84,F332.84,F418.84,F434.84,F436.84,F437.84,F438.\
  84,F439.84,F86.84,F89.84
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  DOMAIN MODELS:
  BUOYANCY MODEL:
  Option = Non Buoyant
  END
  DOMAIN MOTION:
  Option = Stationary
  END
  MESH DEFORMATION:
  Option = None
  END
  REFERENCE PRESSURE:
  Reference Pressure = 1 [atm]
  END
  END
  FLUID DEFINITION: Fluid 1
  Material = Water
  Option = Material Library
  MORPHOLOGY:
  Option = Continuous Fluid
  END
  END
  FLUID MODELS:
  COMBUSTION MODEL:
  Option = None
  END
  HEAT TRANSFER MODEL:
  Option = None
  END
  THERMAL RADIATION MODEL:
  Option = None
  END
  TURBULENCE MODEL:
  Option = SST
  END
  TURBULENT WALL FUNCTIONS:
  Option = Automatic
  END
  END
  END
  DOMAIN: SPILLAGE DX
  Coord Frame = Coord 0
  Domain Type = Fluid
  Location = B339
  BOUNDARY: Interface SPILLAGECENTER SPILLAGEDX Side 2
  Boundary Type = INTERFACE
  Location = F328.339
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface SPILLAGEDX ROTATINGCOOLINGSX Side 1
  Boundary Type = INTERFACE
  Location = F220.339
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: SPILLAGE DX Default
  Boundary Type = WALL
  Location = F1890.339,F330.339,F331.339,F419.339,F420.339,F421.339
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  DOMAIN MODELS:
  BUOYANCY MODEL:
  Option = Non Buoyant
  END
  DOMAIN MOTION:
  Option = Stationary
  END
  MESH DEFORMATION:
  Option = None
  END
  REFERENCE PRESSURE:
  Reference Pressure = 1 [atm]
  END
  END
  FLUID DEFINITION: Fluid 1
  Material = Water
  Option = Material Library
  MORPHOLOGY:
  Option = Continuous Fluid
  END
  END
  FLUID MODELS:
  COMBUSTION MODEL:
  Option = None
  END
  HEAT TRANSFER MODEL:
  Option = None
  END
  THERMAL RADIATION MODEL:
  Option = None
  END
  TURBULENCE MODEL:
  Option = SST
  END
  TURBULENT WALL FUNCTIONS:
  Option = Automatic
  END
  END
  END
  DOMAIN: SPILLAGE SX
  Coord Frame = Coord 0
  Domain Type = Fluid
  Location = B38
  BOUNDARY: Interface ROTATINGSPILLAGE SPILLAGESX Side 2
  Boundary Type = INTERFACE
  Location = F299.38,F300.38,F301.38,F302.38,F303.38
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface SPILLAGECENTER SPILLAGESX Side 2
  Boundary Type = INTERFACE
  Location = F312.38
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: SPILLAGE SX Default
  Boundary Type = WALL
  Location = \
  F315.38,F347.38,F348.38,F349.38,F350.38,F351.38,F352.38,F353.38,F354.\
  38,F435.38,F440.38,F441.38,F442.38,F443.38,F444.38,F445.38,F446.38,F4\
  47.38,F448.38,F449.38,F451.38,F452.38,F453.38,F454.38,F455.38,F456.38\
  ,F457.38,F458.38,F459.38,F460.38,F461.38,F462.38,F463.38,F464.38,F465\
  .38,F466.38,F467.38,F468.38,F469.38,F470.38,F471.38,F472.38,F473.38,F\
  474.38,F475.38,F476.38,F477.38,F478.38,F479.38,F480.38,F481.38,F482.38
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  DOMAIN MODELS:
  BUOYANCY MODEL:
  Option = Non Buoyant
  END
  DOMAIN MOTION:
  Option = Stationary
  END
  MESH DEFORMATION:
  Option = None
  END
  REFERENCE PRESSURE:
  Reference Pressure = 1 [atm]
  END
  END
  FLUID DEFINITION: Fluid 1
  Material = Water
  Option = Material Library
  MORPHOLOGY:
  Option = Continuous Fluid
  END
  END
  FLUID MODELS:
  COMBUSTION MODEL:
  Option = None
  END
  HEAT TRANSFER MODEL:
  Option = None
  END
  THERMAL RADIATION MODEL:
  Option = None
  END
  TURBULENCE MODEL:
  Option = SST
  END
  TURBULENT WALL FUNCTIONS:
  Option = Automatic
  END
  END
  END
  DOMAIN: SPILLAGE VOLUTE
  Coord Frame = Coord 0
  Domain Type = Fluid
  Location = B319
  BOUNDARY: Interface SPILLAGEVOLUTE SPILLAGECENTER Side 1
  Boundary Type = INTERFACE
  Location = F311.319
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface VOLUTE SPILLAGEVOLUTE Side 2
  Boundary Type = INTERFACE
  Location = F1888.319
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: SPILLAGE VOLUTE Default
  Boundary Type = WALL
  Location = F313.319
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  DOMAIN MODELS:
  BUOYANCY MODEL:
  Option = Non Buoyant
  END
  DOMAIN MOTION:
  Option = Stationary
  END
  MESH DEFORMATION:
  Option = None
  END
  REFERENCE PRESSURE:
  Reference Pressure = 1 [atm]
  END
  END
  FLUID DEFINITION: Fluid 1
  Material = Water
  Option = Material Library
  MORPHOLOGY:
  Option = Continuous Fluid
  END
  END
  FLUID MODELS:
  COMBUSTION MODEL:
  Option = None
  END
  HEAT TRANSFER MODEL:
  Option = None
  END
  THERMAL RADIATION MODEL:
  Option = None
  END
  TURBULENCE MODEL:
  Option = SST
  END
  TURBULENT WALL FUNCTIONS:
  Option = Automatic
  END
  END
  END
  DOMAIN: VOLUTE
  Coord Frame = Coord 0
  Domain Type = Fluid
  Location = B1875
  BOUNDARY: Interface CONVERGENT VOLUTE Side 2
  Boundary Type = INTERFACE
  Location = F1894.1875
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface ROTATINGIMPELLER VOLUTE Side 2
  Boundary Type = INTERFACE
  Location = F1876.1875
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface VOLUTE SPILLAGEVOLUTE Side 1
  Boundary Type = INTERFACE
  Location = F1888.1875
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: VOLUTE Default
  Boundary Type = WALL
  Location = \
  F1887.1875,F1895.1875,F1896.1875,F1897.1875,F1898.1875,F1899.1875,F48\
  9.1875,F490.1875,F491.1875,F492.1875,F493.1875,F494.1875,F495.1875,F4\
  96.1875,F497.1875,F498.1875,F499.1875,F500.1875,F501.1875,F502.1875,F\
  503.1875,F504.1875,F505.1875,F506.1875,F507.1875
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  DOMAIN MODELS:
  BUOYANCY MODEL:
  Option = Non Buoyant
  END
  DOMAIN MOTION:
  Option = Stationary
  END
  MESH DEFORMATION:
  Option = None
  END
  REFERENCE PRESSURE:
  Reference Pressure = 1 [atm]
  END
  END
  FLUID DEFINITION: Fluid 1
  Material = Water
  Option = Material Library
  MORPHOLOGY:
  Option = Continuous Fluid
  END
  END
  FLUID MODELS:
  COMBUSTION MODEL:
  Option = None
  END
  HEAT TRANSFER MODEL:
  Option = None
  END
  THERMAL RADIATION MODEL:
  Option = None
  END
  TURBULENCE MODEL:
  Option = SST
  END
  TURBULENT WALL FUNCTIONS:
  Option = Automatic
  END
  END
  END
  DOMAIN INTERFACE: Interface CONVERGENT VOLUTE
  Boundary List1 = Interface CONVERGENT VOLUTE Side 1
  Boundary List2 = Interface CONVERGENT VOLUTE Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = None
  AXIS DEFINITION:
  Option = Coordinate Axis
  Rotation Axis = Coord 0.3
  END
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface DUCTS ROTATINGCOOLINGDX Xdir
  Boundary List1 = Interface DUCTS ROTATINGCOOLINGDX Xdir Side 1
  Boundary List2 = Interface DUCTS ROTATINGCOOLINGDX Xdir Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = Automatic
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface DUCTS ROTATINGCOOLINGDX Zdir
  Boundary List1 = Interface DUCTS ROTATINGCOOLINGDX Zdir Side 1
  Boundary List2 = Interface DUCTS ROTATINGCOOLINGDX Zdir Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = Automatic
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface EULERIAN INTAKE
  Boundary List1 = Interface EULERIAN INTAKE Side 1
  Boundary List2 = Interface EULERIAN INTAKE Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = None
  AXIS DEFINITION:
  Option = Coordinate Axis
  Rotation Axis = Coord 0.3
  END
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface INTAKE INTAKEMAZE
  Boundary List1 = Interface INTAKE INTAKEMAZE Side 1
  Boundary List2 = Interface INTAKE INTAKEMAZE Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = None
  AXIS DEFINITION:
  Option = Coordinate Axis
  Rotation Axis = Coord 0.3
  END
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface INTAKEMAZE ROTATINGIMPELLER
  Boundary List1 = Interface INTAKEMAZE ROTATINGIMPELLER Side 1
  Boundary List2 = Interface INTAKEMAZE ROTATINGIMPELLER Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = Automatic
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface ROTATINGBOLT ROTATINGIMPELLER
  Boundary List1 = Interface ROTATINGBOLT ROTATINGIMPELLER Side 1
  Boundary List2 = Interface ROTATINGBOLT ROTATINGIMPELLER Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = Automatic
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface ROTATINGBOLT ROTATINGSHAFT
  Boundary List1 = Interface ROTATINGBOLT ROTATINGSHAFT Side 1
  Boundary List2 = Interface ROTATINGBOLT ROTATINGSHAFT Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = Automatic
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface ROTATINGCOOLINGCENTER ROTATINGCOOLINGDX
  Boundary List1 = Interface ROTATINGCOOLINGCENTER ROTATINGCOOLINGDX Side 1
  Boundary List2 = Interface ROTATINGCOOLINGCENTER ROTATINGCOOLINGDX Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = Automatic
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface ROTATINGCOOLINGDX ROTATINGSHAFT
  Boundary List1 = Interface ROTATINGCOOLINGDX ROTATINGSHAFT Side 1
  Boundary List2 = Interface ROTATINGCOOLINGDX ROTATINGSHAFT Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = None
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface ROTATINGCOOLINGSX ROTATINGCOOLINGCENTER
  Boundary List1 = Interface ROTATINGCOOLINGSX ROTATINGCOOLINGCENTER Side 1
  Boundary List2 = Interface ROTATINGCOOLINGSX ROTATINGCOOLINGCENTER Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = Automatic
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface ROTATINGIMPELLER ROTATINGSPILLAGE
  Boundary List1 = Interface ROTATINGIMPELLER ROTATINGSPILLAGE Side 1
  Boundary List2 = Interface ROTATINGIMPELLER ROTATINGSPILLAGE Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = Automatic
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface ROTATINGIMPELLER VOLUTE
  Boundary List1 = Interface ROTATINGIMPELLER VOLUTE Side 1
  Boundary List2 = Interface ROTATINGIMPELLER VOLUTE Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = Automatic
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface ROTATINGSPILLAGE ROTATINGCOOLINGSX
  Boundary List1 = Interface ROTATINGSPILLAGE ROTATINGCOOLINGSX Side 1
  Boundary List2 = Interface ROTATINGSPILLAGE ROTATINGCOOLINGSX Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = Automatic
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface ROTATINGSPILLAGE SPILLAGESX
  Boundary List1 = Interface ROTATINGSPILLAGE SPILLAGESX Side 1
  Boundary List2 = Interface ROTATINGSPILLAGE SPILLAGESX Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = Automatic
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface SPILLAGECENTER ROTATINGSPILLAGE
  Boundary List1 = Interface SPILLAGECENTER ROTATINGSPILLAGE Side 1
  Boundary List2 = Interface SPILLAGECENTER ROTATINGSPILLAGE Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = Automatic
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface SPILLAGECENTER SPILLAGEDX
  Boundary List1 = Interface SPILLAGECENTER SPILLAGEDX Side 1
  Boundary List2 = Interface SPILLAGECENTER SPILLAGEDX Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = None
  AXIS DEFINITION:
  Option = Coordinate Axis
  Rotation Axis = Coord 0.3
  END
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface SPILLAGECENTER SPILLAGESX
  Boundary List1 = Interface SPILLAGECENTER SPILLAGESX Side 1
  Boundary List2 = Interface SPILLAGECENTER SPILLAGESX Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = None
  AXIS DEFINITION:
  Option = Coordinate Axis
  Rotation Axis = Coord 0.3
  END
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface SPILLAGEDX ROTATINGCOOLINGSX
  Boundary List1 = Interface SPILLAGEDX ROTATINGCOOLINGSX Side 1
  Boundary List2 = Interface SPILLAGEDX ROTATINGCOOLINGSX Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = Automatic
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface SPILLAGEVOLUTE SPILLAGECENTER
  Boundary List1 = Interface SPILLAGEVOLUTE SPILLAGECENTER Side 1
  Boundary List2 = Interface SPILLAGEVOLUTE SPILLAGECENTER Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = None
  AXIS DEFINITION:
  Option = Coordinate Axis
  Rotation Axis = Coord 0.3
  END
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface VOLUTE SPILLAGEVOLUTE
  Boundary List1 = Interface VOLUTE SPILLAGEVOLUTE Side 1
  Boundary List2 = Interface VOLUTE SPILLAGEVOLUTE Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = None
  AXIS DEFINITION:
  Option = Coordinate Axis
  Rotation Axis = Coord 0.3
  END
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  OUTPUT CONTROL:
  RESULTS:
  File Compression Level = Default
  Option = Standard
  END
  END
  SOLVER CONTROL:
  Turbulence Numerics = First Order
  ADVECTION SCHEME:
  Option = High Resolution
  END
  CONVERGENCE CONTROL:
  Length Scale Option = Conservative
  Maximum Number of Iterations = 500
  Minimum Number of Iterations = 1
  Timescale Control = Auto Timescale
  Timescale Factor = 10
  END
  CONVERGENCE CRITERIA:
  Residual Target = 0.001
  Residual Type = RMS
  END
  DYNAMIC MODEL CONTROL:
  Global Dynamic Model Control = On
  END
  INTERRUPT CONTROL:
  Option = Any Interrupt
  CONVERGENCE CONDITIONS:
  Option = Default Conditions
  END
  END
  END
  END
  COMMAND FILE:
  Version = 21.1
  Results Version = 21.1
  END
  SIMULATION CONTROL:
  EXECUTION CONTROL:
  EXECUTABLE SELECTION:
  Double Precision = Yes
  Large Problem = No
  END
  INTERPOLATOR STEP CONTROL:
  Runtime Priority = Standard
  MEMORY CONTROL:
  Memory Allocation Factor = 1.0
  END
  END
  PARALLEL HOST LIBRARY:
  HOST DEFINITION: -----
  Host Architecture String = winnt-amd64
  Installation Root = C:\Program Files\ANSYS Inc\v%v\CFX
  END
  END
  PARTITIONER STEP CONTROL:
  Multidomain Option = Automatic
  Runtime Priority = Standard
  MEMORY CONTROL:
  Memory Allocation Factor = 1.0
  END
  PARTITION SMOOTHING:
  Maximum Partition Smoothing Sweeps = 100
  Option = Smooth
  END
  PARTITIONING TYPE:
  MeTiS Type = k-way
  Option = MeTiS
  Partition Size Rule = Automatic
  Partition Weight Factors = 0.50000, 0.50000
  END
  END
  RUN DEFINITION:
  Run Mode = Full
  Solver Input File = CFX.def
  Solver Results File = \
  C:/Users/-CFD_pe\
  nding/dp0_CFX_1_Solution_1/CFX_001.res
  END
  SOLVER STEP CONTROL:
  Runtime Priority = Standard
  MEMORY CONTROL:
  Memory Allocation Factor = 1.0
  END
  PARALLEL ENVIRONMENT:
  Number of Processes = 2
  Start Method = Intel MPI Local Parallel
  Parallel Host List = ---*2
  END
  END
  END
  END
  
  +--------------------------------------------------------------------+
  | |
  | Partitioning |
  | |
  +--------------------------------------------------------------------+
  
  +--------------------------------------------------------------------+
  | |
  | ANSYS(R) CFX(R) Partitioner |
  | |
  +--------------------------------------------------------------------+
  | An error has occurred in cfx5solve: |
  | |
  | The ANSYS CFX partitioner exited with return code 1. |
  +--------------------------------------------------------------------+
  
  +--------------------------------------------------------------------+
  | For CFX runs launched from Workbench, the final locations of |
  | directories and files generated may differ from those shown. |
  +--------------------------------------------------------------------+
  
  This run of the ANSYS CFX Solver has finished.
  
  Do you have any idea?
  Thank you,
  Stefano
- May 23, 2023 at 11:28 am
  
  C N
  Ansys Employee
  
  Hello Stefano,
  Mostly this error of return code 1 happens when the boundary condition, an initial condition or some other function is not set properly. Either you did not set any pressure condition or the condition you set is not valid.If the isolated regions do not have the pressure level set either by the boundary conditions or using a reference pressure equation, you may encounter severe robustness problems.Also check your directory location.
  
  This situation may have arisen because a domain interface was not properly defined during problem setup. Please carefully check the setup.
  
  The solver will stop now and write a results file. The isolated regions can be visualised in CFX Post by making plots of the variable "Isolated Volumes".
  
  If you are sure that the pressure level is set in each isolated fluid region then you can force the solver to turn off this check by setting the expert parameter "check isolated regions = f".
  Thanks,
  Chaitanya Natraj
- May 23, 2023 at 1:12 pm
  
  Stefano Chieti
  Subscriber
  
  Hello Chaitanya,
  thank you for your prompt reply! I can easely agree with any of your setup statements, I know that can be far from good or "correct".
  The real fact is that I had a project in FluidFlow (CFX), with the same exact setup, which was solved withou errors and gave me results. My very first attempt was to change some setup input values. Then I found errors. My second attempt was then to simply re-run the same exact setup in that project, which eventually led to errors where previously where not!
  My last attempt has been to reproduce from scratch in another project, with the same first solved setup, but still getting errors.
  The fact which triggers me is that the initial, solved, project is not able to be solved anymore without changing anything, exept for the directory location on my workstation (the workstation and release of ANSYS is the same). This is why I also thought about some licensing or directory path problem.
  I attach the initial project .outfile if can be usefull. I double-checked it and it's exaclty the same as the one atteched in the starting thread.
  %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
  This run of the CFX 2021 R1 Solver started at 10:08:45 on 08 Feb 2022
  by user Stefano.CHIETI on ------- (intel_xeon64.sse2_winnt) using the
  command:
  
  "C:\Program Files\ANSYS Inc\v211\CFX\bin\perllib\cfx5solve.pl" -batch
  -ccl runInput.ccl -fullname CFX_003
  
  2021 R1
  
  Point Releases and Patches installed:
  ANSYS, Inc. Products 2021 R1
  SpaceClaim 2021 R1
  Autodyn 2021 R1
  CFD-Post only 2021 R1
  CFX (includes CFD-Post) 2021 R1
  FENSAP-ICE 2021 R1
  Fluent (includes CFD-Post) 2021 R1
  Forte (includes EnSight) 2021 R1
  Polyflow (includes CFD-Post) 2021 R1
  TurboGrid 2021 R1
  Aqwa 2021 R1
  Customization Files for User Programmable Features 2021 R1
  Mechanical Products 2021 R1
  Icepak (includes CFD-Post) 2021 R1
  Remote Solve Manager Standalone Services 2021 R1
  Viewer 2021 R1
  ACIS Geometry Interface 2021 R1
  AutoCAD Geometry Interface 2021 R1
  Catia, Version 4 Geometry Interface 2021 R1
  Catia, Version 5 Geometry Interface 2021 R1
  Catia, Version 6 Geometry Interface 2021 R1
  Creo Elements/Direct Modeling Geometry Interface 2021 R1
  Creo Parametric Geometry Interface 2021 R1
  Inventor Geometry Interface 2021 R1
  JTOpen Geometry Interface 2021 R1
  NX Geometry Interface 2021 R1
  Parasolid Geometry Interface 2021 R1
  Solid Edge Geometry Interface 2021 R1
  SOLIDWORKS Geometry Interface 2021 R1
  ANSYS, Inc. License Manager 2021 R1
  
  Setting up CFX Solver run ...
  
  +--------------------------------------------------------------------+
  | |
  | CFX Command Language for Run |
  | |
  +--------------------------------------------------------------------+
  
  LIBRARY:
  MATERIAL: Water
  Material Description = Water (liquid)
  Material Group = Water Data, Constant Property Liquids
  Option = Pure Substance
  Thermodynamic State = Liquid
  PROPERTIES:
  Option = General Material
  EQUATION OF STATE:
  Density = 997.0 [kg m^-3]
  Molar Mass = 18.02 [kg kmol^-1]
  Option = Value
  END
  SPECIFIC HEAT CAPACITY:
  Option = Value
  Specific Heat Capacity = 4181.7 [J kg^-1 K^-1]
  Specific Heat Type = Constant Pressure
  END
  REFERENCE STATE:
  Option = Specified Point
  Reference Pressure = 1 [atm]
  Reference Specific Enthalpy = 0.0 [J/kg]
  Reference Specific Entropy = 0.0 [J/kg/K]
  Reference Temperature = 25 [C]
  END
  DYNAMIC VISCOSITY:
  Dynamic Viscosity = 8.899E-4 [kg m^-1 s^-1]
  Option = Value
  END
  THERMAL CONDUCTIVITY:
  Option = Value
  Thermal Conductivity = 0.6069 [W m^-1 K^-1]
  END
  ABSORPTION COEFFICIENT:
  Absorption Coefficient = 1.0 [m^-1]
  Option = Value
  END
  SCATTERING COEFFICIENT:
  Option = Value
  Scattering Coefficient = 0.0 [m^-1]
  END
  REFRACTIVE INDEX:
  Option = Value
  Refractive Index = 1.0 [m m^-1]
  END
  THERMAL EXPANSIVITY:
  Option = Value
  Thermal Expansivity = 2.57E-04 [K^-1]
  END
  END
  END
  END
  FLOW: Flow Analysis 1
  SOLUTION UNITS:
  Angle Units = [rad]
  Length Units = [m]
  Mass Units = [kg]
  Solid Angle Units = [sr]
  Temperature Units = [K]
  Time Units = [s]
  END
  ANALYSIS TYPE:
  Option = Steady State
  EXTERNAL SOLVER COUPLING:
  Option = None
  END
  END
  DOMAIN: CONVERGENT
  Coord Frame = Coord 0
  Domain Type = Fluid
  Location = B2646
  BOUNDARY: CONVERGENT Default
  Boundary Type = WALL
  Location = F2647.2646
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  BOUNDARY: Interface Convergent Volute Side 1
  Boundary Type = INTERFACE
  Location = F1861.2646
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: OUTLET
  Boundary Type = OUTLET
  Location = F2648.2646
  BOUNDARY CONDITIONS:
  FLOW REGIME:
  Option = Subsonic
  END
  MASS AND MOMENTUM:
  Mass Flow Rate = 0.63 [kg s^-1]
  Mass Flow Rate Area = As Specified
  Option = Mass Flow Rate
  END
  END
  END
  DOMAIN MODELS:
  BUOYANCY MODEL:
  Option = Non Buoyant
  END
  DOMAIN MOTION:
  Option = Stationary
  END
  MESH DEFORMATION:
  Option = None
  END
  REFERENCE PRESSURE:
  Reference Pressure = 1 [atm]
  END
  END
  FLUID DEFINITION: Fluid 1
  Material = Water
  Option = Material Library
  MORPHOLOGY:
  Option = Continuous Fluid
  END
  END
  FLUID MODELS:
  COMBUSTION MODEL:
  Option = None
  END
  HEAT TRANSFER MODEL:
  Option = None
  END
  THERMAL RADIATION MODEL:
  Option = None
  END
  TURBULENCE MODEL:
  Option = SST
  END
  TURBULENT WALL FUNCTIONS:
  Option = Automatic
  END
  END
  END
  DOMAIN: DUCTS
  Coord Frame = Coord 0
  Domain Type = Fluid
  Location = B188,B189,B26,B27
  BOUNDARY: DUCTS Default
  Boundary Type = WALL
  Location = \
  F21.188,F22.27,F23.189,F24.26,F254.188,F255.188,F256.188,F258.188,F25\
  9.189,F260.189,F261.189,F263.189,F271.189,F272.189,F273.189,F274.189,\
  F275.189,F276.189,F277.189,F278.189,F279.188,F280.188,F281.188,F282.1\
  88,F2828.26,F2829.26,F283.188,F2832.27,F2833.27,F2836.188,F2837.188,F\
  284.188,F2840.189,F2841.189,F285.188,F286.188,F287.26,F288.26,F289.26\
  ,F290.26,F291.26,F292.26,F293.26,F294.26,F295.27,F296.27,F297.27,F298\
  .27,F299.27,F300.27,F301.27,F302.27,F303.27,F304.27,F306.27,F307.27,F\
  310.26,F311.26,F312.26,F314.26
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  BOUNDARY: Interface Ducts RotatingCoolingDX Xdir Side 1
  Boundary Type = INTERFACE
  Location = \
  F2657.26,F2658.189,F2659.27,F2660.188,F2666.188,F2667.27,F2668.189,F2\
  669.26
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface Ducts RotatingCoolingDX Zdir Side 1
  Boundary Type = INTERFACE
  Location = F2662.26,F2663.189,F2664.27,F2665.188
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  DOMAIN MODELS:
  BUOYANCY MODEL:
  Option = Non Buoyant
  END
  DOMAIN MOTION:
  Option = Stationary
  END
  MESH DEFORMATION:
  Option = None
  END
  REFERENCE PRESSURE:
  Reference Pressure = 1 [atm]
  END
  END
  FLUID DEFINITION: Fluid 1
  Material = Water
  Option = Material Library
  MORPHOLOGY:
  Option = Continuous Fluid
  END
  END
  FLUID MODELS:
  COMBUSTION MODEL:
  Option = None
  END
  HEAT TRANSFER MODEL:
  Option = None
  END
  THERMAL RADIATION MODEL:
  Option = None
  END
  TURBULENCE MODEL:
  Option = SST
  END
  TURBULENT WALL FUNCTIONS:
  Option = Automatic
  END
  END
  END
  DOMAIN: EULERIAN
  Coord Frame = Coord 0
  Domain Type = Fluid
  Location = B2640
  BOUNDARY: EULERIAN Default
  Boundary Type = WALL
  Location = F2641.2640
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  BOUNDARY: INLET
  Boundary Type = INLET
  Location = F2642.2640
  BOUNDARY CONDITIONS:
  FLOW DIRECTION:
  Option = Normal to Boundary Condition
  END
  FLOW REGIME:
  Option = Subsonic
  END
  MASS AND MOMENTUM:
  Option = Total Pressure
  Relative Pressure = 185 [kPa]
  END
  TURBULENCE:
  Option = Medium Intensity and Eddy Viscosity Ratio
  END
  END
  END
  BOUNDARY: Interface Eulerian Intake Side 1
  Boundary Type = INTERFACE
  Location = F2759.2640
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  DOMAIN MODELS:
  BUOYANCY MODEL:
  Option = Non Buoyant
  END
  DOMAIN MOTION:
  Option = Stationary
  END
  MESH DEFORMATION:
  Option = None
  END
  REFERENCE PRESSURE:
  Reference Pressure = 1 [atm]
  END
  END
  FLUID DEFINITION: Fluid 1
  Material = Water
  Option = Material Library
  MORPHOLOGY:
  Option = Continuous Fluid
  END
  END
  FLUID MODELS:
  COMBUSTION MODEL:
  Option = None
  END
  HEAT TRANSFER MODEL:
  Option = None
  END
  THERMAL RADIATION MODEL:
  Option = None
  END
  TURBULENCE MODEL:
  Option = SST
  END
  TURBULENT WALL FUNCTIONS:
  Option = Automatic
  END
  END
  END
  DOMAIN: INTAKE
  Coord Frame = Coord 0
  Domain Type = Fluid
  Location = B67
  BOUNDARY: INTAKE Default
  Boundary Type = WALL
  Location = F2868.67,F436.67
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  BOUNDARY: Interface Eulerian Intake Side 2
  Boundary Type = INTERFACE
  Location = F2759.67
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface Intake IntakeMaze Side 1
  Boundary Type = INTERFACE
  Location = F2875.67
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  DOMAIN MODELS:
  BUOYANCY MODEL:
  Option = Non Buoyant
  END
  DOMAIN MOTION:
  Option = Stationary
  END
  MESH DEFORMATION:
  Option = None
  END
  REFERENCE PRESSURE:
  Reference Pressure = 1 [atm]
  END
  END
  FLUID DEFINITION: Fluid 1
  Material = Water
  Option = Material Library
  MORPHOLOGY:
  Option = Continuous Fluid
  END
  END
  FLUID MODELS:
  COMBUSTION MODEL:
  Option = None
  END
  HEAT TRANSFER MODEL:
  Option = None
  END
  THERMAL RADIATION MODEL:
  Option = None
  END
  TURBULENCE MODEL:
  Option = SST
  END
  TURBULENT WALL FUNCTIONS:
  Option = Automatic
  END
  END
  END
  DOMAIN: INTAKE MAZE
  Coord Frame = Coord 0
  Domain Type = Fluid
  Location = B2761
  BOUNDARY: INTAKE MAZE Default
  Boundary Type = WALL
  Location = \
  F427.2761,F428.2761,F429.2761,F430.2761,F431.2761,F432.2761,F433.2761\
  ,F434.2761,F899.2761,F904.2761,F906.2761,F907.2761,F909.2761,F910.276\
  1,F911.2761,F912.2761,F913.2761
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  BOUNDARY: Interface Intake IntakeMaze Side 2
  Boundary Type = INTERFACE
  Location = F2875.2761
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface IntakeMaze RotatingImpeller Side 1
  Boundary Type = INTERFACE
  Location = F211.2761,F2874.2761
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  DOMAIN MODELS:
  BUOYANCY MODEL:
  Option = Non Buoyant
  END
  DOMAIN MOTION:
  Option = Stationary
  END
  MESH DEFORMATION:
  Option = None
  END
  REFERENCE PRESSURE:
  Reference Pressure = 1 [atm]
  END
  END
  FLUID DEFINITION: Fluid 1
  Material = Water
  Option = Material Library
  MORPHOLOGY:
  Option = Continuous Fluid
  END
  END
  FLUID MODELS:
  COMBUSTION MODEL:
  Option = None
  END
  HEAT TRANSFER MODEL:
  Option = None
  END
  THERMAL RADIATION MODEL:
  Option = None
  END
  TURBULENCE MODEL:
  Option = SST
  END
  TURBULENT WALL FUNCTIONS:
  Option = Automatic
  END
  END
  END
  DOMAIN: ROTATING BOLT
  Coord Frame = Coord 0
  Domain Type = Fluid
  Location = B2687
  BOUNDARY: Interface RotatingBolt RotatingImpeller Side 1
  Boundary Type = INTERFACE
  Location = F2699.2687,F2700.2687,F2701.2687,F2702.2687
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface RotatingBolt RotatingShaft Side 1
  Boundary Type = INTERFACE
  Location = F2672.2687
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: ROTATING BOLT Default
  Boundary Type = WALL
  Frame Type = Rotating
  Location = \
  F1096.2687,F1097.2687,F236.2687,F237.2687,F238.2687,F239.2687,F2670.2\
  687,F2675.2687,F2703.2687,F872.2687,F873.2687,F888.2687,F915.2687,F93\
  8.2687,F939.2687,F940.2687
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  DOMAIN MODELS:
  BUOYANCY MODEL:
  Option = Non Buoyant
  END
  DOMAIN MOTION:
  Alternate Rotation Model = true
  Angular Velocity = -1256.64 [radian s^-1]
  Option = Rotating
  AXIS DEFINITION:
  Option = Coordinate Axis
  Rotation Axis = Coord 0.3
  END
  END
  MESH DEFORMATION:
  Option = None
  END
  REFERENCE PRESSURE:
  Reference Pressure = 1 [atm]
  END
  END
  FLUID DEFINITION: Fluid 1
  Material = Water
  Option = Material Library
  MORPHOLOGY:
  Option = Continuous Fluid
  END
  END
  FLUID MODELS:
  COMBUSTION MODEL:
  Option = None
  END
  HEAT TRANSFER MODEL:
  Option = None
  END
  THERMAL RADIATION MODEL:
  Option = None
  END
  TURBULENCE MODEL:
  Option = SST
  END
  TURBULENT WALL FUNCTIONS:
  Option = Automatic
  END
  END
  END
  DOMAIN: ROTATING COOLING CENTER
  Coord Frame = Coord 0
  Domain Type = Fluid
  Location = B2762
  BOUNDARY: Interface RotatingCoolingCENTER RotatingCoolingDX Side 1
  Boundary Type = INTERFACE
  Location = F2778.2762
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface RotatingCoolingSX RotatingCoolingCENTER Side 2
  Boundary Type = INTERFACE
  Location = F2804.2762
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: ROTATING COOLING CENTER Default
  Boundary Type = WALL
  Frame Type = Rotating
  Location = F2781.2762
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  BOUNDARY: StaticWalls CoolingCENTER
  Boundary Type = WALL
  Frame Type = Rotating
  Location = F2779.2762
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  DOMAIN MODELS:
  BUOYANCY MODEL:
  Option = Non Buoyant
  END
  DOMAIN MOTION:
  Alternate Rotation Model = true
  Angular Velocity = -1256.64 [radian s^-1]
  Option = Rotating
  AXIS DEFINITION:
  Option = Coordinate Axis
  Rotation Axis = Coord 0.3
  END
  END
  MESH DEFORMATION:
  Option = None
  END
  REFERENCE PRESSURE:
  Reference Pressure = 1 [atm]
  END
  END
  FLUID DEFINITION: Fluid 1
  Material = Water
  Option = Material Library
  MORPHOLOGY:
  Option = Continuous Fluid
  END
  END
  FLUID MODELS:
  COMBUSTION MODEL:
  Option = None
  END
  HEAT TRANSFER MODEL:
  Option = None
  END
  THERMAL RADIATION MODEL:
  Option = None
  END
  TURBULENCE MODEL:
  Option = SST
  END
  TURBULENT WALL FUNCTIONS:
  Option = Automatic
  END
  END
  END
  DOMAIN: ROTATING COOLING DX
  Coord Frame = Coord 0
  Domain Type = Fluid
  Location = B2787
  BOUNDARY: Interface Ducts RotatingCoolingDX Xdir Side 2
  Boundary Type = INTERFACE
  Location = \
  F2657.2787,F2658.2787,F2659.2787,F2660.2787,F2666.2787,F2667.2787,F26\
  68.2787,F2669.2787
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface Ducts RotatingCoolingDX Zdir Side 2
  Boundary Type = INTERFACE
  Location = F2662.2787,F2663.2787,F2664.2787,F2665.2787
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface RotatingCoolingCENTER RotatingCoolingDX Side 2
  Boundary Type = INTERFACE
  Location = F2778.2787
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface RotatingCoolingDX RotatingShaft Side 1
  Boundary Type = INTERFACE
  Location = F2688.2787
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: ROTATING COOLING DX Default
  Boundary Type = WALL
  Frame Type = Rotating
  Location = \
  F10.2787,F1000.2787,F1001.2787,F1002.2787,F1003.2787,F1004.2787,F1005\
  .2787,F1006.2787,F1007.2787,F1008.2787,F1009.2787,F1010.2787,F1011.27\
  87,F1012.2787,F1013.2787,F1014.2787,F1015.2787,F1016.2787,F1017.2787,\
  F1018.2787,F1019.2787,F1020.2787,F1021.2787,F1022.2787,F1023.2787,F10\
  24.2787,F1025.2787,F1026.2787,F1027.2787,F1028.2787,F1029.2787,F1030.\
  2787,F1031.2787,F1032.2787,F1033.2787,F1034.2787,F1035.2787,F1036.278\
  7,F1037.2787,F1038.2787,F1039.2787,F1040.2787,F1041.2787,F1042.2787,F\
  1043.2787,F1044.2787,F1045.2787,F1046.2787,F1047.2787,F1048.2787,F104\
  9.2787,F1050.2787,F1051.2787,F1052.2787,F1053.2787,F1054.2787,F1055.2\
  787,F1056.2787,F1057.2787,F1058.2787,F1059.2787,F1060.2787,F1061.2787\
  ,F1062.2787,F1063.2787,F1064.2787,F1065.2787,F1066.2787,F1067.2787,F1\
  068.2787,F1069.2787,F1070.2787,F1071.2787,F1072.2787,F1073.2787,F1074\
  .2787,F1075.2787,F1076.2787,F1077.2787,F1078.2787,F1079.2787,F1080.27\
  87,F1081.2787,F1082.2787,F1083.2787,F1084.2787,F1085.2787,F1086.2787,\
  F1087.2787,F1088.2787,F1089.2787,F1090.2787,F11.2787,F1111.2787,F1112\
  .2787,F1113.2787,F1114.2787,F1115.2787,F1116.2787,F1117.2787,F2713.27\
  87,F2782.2787,F32.2787,F36.2787,F37.2787,F38.2787,F39.2787,F4.2787,F4\
  0.2787,F41.2787,F42.2787,F43.2787,F44.2787,F45.2787,F46.2787,F47.2787\
  ,F48.2787,F49.2787,F5.2787,F50.2787,F6.2787,F7.2787,F8.2787,F867.2787\
  ,F868.2787,F869.2787,F9.2787,F918.2787,F929.2787,F930.2787,F931.2787,\
  F932.2787,F933.2787,F934.2787,F935.2787,F936.2787,F941.2787,F942.2787\
  ,F943.2787,F944.2787,F948.2787,F951.2787,F952.2787,F953.2787,F954.278\
  7,F955.2787,F956.2787,F957.2787,F958.2787,F959.2787,F960.2787,F961.27\
  87,F962.2787,F974.2787,F975.2787,F976.2787,F977.2787,F978.2787,F979.2\
  787,F980.2787,F981.2787,F982.2787,F983.2787,F984.2787,F985.2787,F986.\
  2787,F987.2787,F988.2787,F989.2787,F990.2787,F991.2787,F992.2787,F993\
  .2787,F994.2787,F995.2787,F996.2787,F997.2787,F998.2787,F999.2787
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  BOUNDARY: StaticWalls CoolingDX
  Boundary Type = WALL
  Frame Type = Rotating
  Location = \
  F1841.2787,F1842.2787,F185.2787,F204.2787,F243.2787,F245.2787,F264.27\
  87,F266.2787,F265.2787,F267.2787,F268.2787,F2689.2787,F269.2787,F270.\
  2787,F308.2787,F309.2787,F315.2787,F320.2787,F321.2787,F322.2787,F323\
  .2787,F324.2787,F33.2787,F2780.2787,F35.2787
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  DOMAIN MODELS:
  BUOYANCY MODEL:
  Option = Non Buoyant
  END
  DOMAIN MOTION:
  Alternate Rotation Model = true
  Angular Velocity = -1256.64 [radian s^-1]
  Option = Rotating
  AXIS DEFINITION:
  Option = Coordinate Axis
  Rotation Axis = Coord 0.3
  END
  END
  MESH DEFORMATION:
  Option = None
  END
  REFERENCE PRESSURE:
  Reference Pressure = 1 [atm]
  END
  END
  FLUID DEFINITION: Fluid 1
  Material = Water
  Option = Material Library
  MORPHOLOGY:
  Option = Continuous Fluid
  END
  END
  FLUID MODELS:
  COMBUSTION MODEL:
  Option = None
  END
  HEAT TRANSFER MODEL:
  Option = None
  END
  THERMAL RADIATION MODEL:
  Option = None
  END
  TURBULENCE MODEL:
  Option = SST
  END
  TURBULENT WALL FUNCTIONS:
  Option = Automatic
  END
  END
  END
  DOMAIN: ROTATING COOLING SX
  Coord Frame = Coord 0
  Domain Type = Fluid
  Location = B2698
  BOUNDARY: Interface RotatingCoolingSX RotatingCoolingCENTER Side 1
  Boundary Type = INTERFACE
  Location = F2804.2698
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface RotatingSpillage RotatingCoolingSX Side 2
  Boundary Type = INTERFACE
  Location = F2671.2698
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface SpillageDX RotatingCoolingSX Side 2
  Boundary Type = INTERFACE
  Location = F207.2698
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: ROTATING COOLING SX Default
  Boundary Type = WALL
  Frame Type = Rotating
  Location = \
  F1100.2698,F1101.2698,F1102.2698,F1103.2698,F1104.2698,F1105.2698,F11\
  06.2698,F1107.2698,F1108.2698,F1109.2698,F2674.2698,F2806.2698,F31.26\
  98,F916.2698,F919.2698,F920.2698,F921.2698,F922.2698,F923.2698,F924.2\
  698,F925.2698,F926.2698,F927.2698,F928.2698,F946.2698
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  BOUNDARY: StaticWalls CoolingSX
  Boundary Type = WALL
  Frame Type = Rotating
  Location = F1856.2698,F2712.2698,F2805.2698
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  DOMAIN MODELS:
  BUOYANCY MODEL:
  Option = Non Buoyant
  END
  DOMAIN MOTION:
  Alternate Rotation Model = true
  Angular Velocity = -1256.64 [radian s^-1]
  Option = Rotating
  AXIS DEFINITION:
  Option = Coordinate Axis
  Rotation Axis = Coord 0.3
  END
  END
  MESH DEFORMATION:
  Option = None
  END
  REFERENCE PRESSURE:
  Reference Pressure = 1 [atm]
  END
  END
  FLUID DEFINITION: Fluid 1
  Material = Water
  Option = Material Library
  MORPHOLOGY:
  Option = Continuous Fluid
  END
  END
  FLUID MODELS:
  COMBUSTION MODEL:
  Option = None
  END
  HEAT TRANSFER MODEL:
  Option = None
  END
  THERMAL RADIATION MODEL:
  Option = None
  END
  TURBULENCE MODEL:
  Option = SST
  END
  TURBULENT WALL FUNCTIONS:
  Option = Automatic
  END
  END
  END
  DOMAIN: ROTATING IMPELLER
  Coord Frame = Coord 0
  Domain Type = Fluid
  Location = B2686
  BOUNDARY: Interface IntakeMaze RotatingImpeller Side 2
  Boundary Type = INTERFACE
  Location = F211.2686,F2874.2686
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface RotatingBolt RotatingImpeller Side 2
  Boundary Type = INTERFACE
  Location = F2699.2686,F2700.2686,F2701.2686,F2702.2686
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface RotatingImpeller RotatingSpillage Side 1
  Boundary Type = INTERFACE
  Location = F2710.2686
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface RotatingImpeller Volute Side 1
  Boundary Type = INTERFACE
  Location = F2727.2686
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: ROTATING IMPELLER Default
  Boundary Type = WALL
  Frame Type = Rotating
  Location = \
  F100.2686,F101.2686,F102.2686,F103.2686,F104.2686,F105.2686,F106.2686\
  ,F107.2686,F1091.2686,F1092.2686,F1093.2686,F1094.2686,F1095.2686,F10\
  99.2686,F69.2686,F77.2686,F78.2686,F79.2686,F80.2686,F81.2686,F82.268\
  6,F83.2686,F84.2686,F85.2686,F86.2686,F87.2686,F875.2686,F876.2686,F8\
  77.2686,F878.2686,F879.2686,F88.2686,F880.2686,F881.2686,F882.2686,F8\
  83.2686,F884.2686,F885.2686,F887.2686,F89.2686,F891.2686,F892.2686,F8\
  93.2686,F894.2686,F895.2686,F896.2686,F897.2686,F898.2686,F90.2686,F9\
  1.2686,F92.2686,F93.2686,F94.2686,F95.2686,F96.2686,F97.2686,F98.2686\
  ,F99.2686
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  BOUNDARY: StaticWalls IMPELLER
  Boundary Type = WALL
  Frame Type = Rotating
  Location = \
  F1869.2686,F420.2686,F421.2686,F422.2686,F423.2686,F424.2686,F425.268\
  6,F426.2686,F70.2686,F900.2686,F901.2686,F902.2686,F903.2686,F905.268\
  6,F908.2686,F1860.2686,F1867.2686,F1868.2686,F193.2686,F209.2686,F210\
  .2686,F2683.2686
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  DOMAIN MODELS:
  BUOYANCY MODEL:
  Option = Non Buoyant
  END
  DOMAIN MOTION:
  Alternate Rotation Model = true
  Angular Velocity = -1256.64 [radian s^-1]
  Option = Rotating
  AXIS DEFINITION:
  Option = Coordinate Axis
  Rotation Axis = Coord 0.3
  END
  END
  MESH DEFORMATION:
  Option = None
  END
  REFERENCE PRESSURE:
  Reference Pressure = 1 [atm]
  END
  END
  FLUID DEFINITION: Fluid 1
  Material = Water
  Option = Material Library
  MORPHOLOGY:
  Option = Continuous Fluid
  END
  END
  FLUID MODELS:
  COMBUSTION MODEL:
  Option = None
  END
  HEAT TRANSFER MODEL:
  Option = None
  END
  THERMAL RADIATION MODEL:
  Option = None
  END
  TURBULENCE MODEL:
  Option = SST
  END
  TURBULENT WALL FUNCTIONS:
  Option = Automatic
  END
  END
  END
  DOMAIN: ROTATING SHAFT
  Coord Frame = Coord 0
  Domain Type = Fluid
  Location = B2681
  BOUNDARY: Interface RotatingBolt RotatingShaft Side 2
  Boundary Type = INTERFACE
  Location = F2672.2681
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface RotatingCoolingDX RotatingShaft Side 2
  Boundary Type = INTERFACE
  Location = F2688.2681
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: ROTATING SHAFT Default
  Boundary Type = WALL
  Frame Type = Rotating
  Location = \
  F2676.2681,F937.2681,F963.2681,F964.2681,F965.2681,F966.2681,F967.268\
  1,F968.2681,F969.2681,F970.2681,F971.2681,F972.2681,F973.2681
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  DOMAIN MODELS:
  BUOYANCY MODEL:
  Option = Non Buoyant
  END
  DOMAIN MOTION:
  Alternate Rotation Model = true
  Angular Velocity = -1256.64 [radian s^-1]
  Option = Rotating
  AXIS DEFINITION:
  Option = Coordinate Axis
  Rotation Axis = Coord 0.3
  END
  END
  MESH DEFORMATION:
  Option = None
  END
  REFERENCE PRESSURE:
  Reference Pressure = 1 [atm]
  END
  END
  FLUID DEFINITION: Fluid 1
  Material = Water
  Option = Material Library
  MORPHOLOGY:
  Option = Continuous Fluid
  END
  END
  FLUID MODELS:
  COMBUSTION MODEL:
  Option = None
  END
  HEAT TRANSFER MODEL:
  Option = None
  END
  THERMAL RADIATION MODEL:
  Option = None
  END
  TURBULENCE MODEL:
  Option = SST
  END
  TURBULENT WALL FUNCTIONS:
  Option = Automatic
  END
  END
  END
  DOMAIN: ROTATING SPILLAGE
  Coord Frame = Coord 0
  Domain Type = Fluid
  Location = B2680
  BOUNDARY: Interface RotatingImpeller RotatingSpillage Side 2
  Boundary Type = INTERFACE
  Location = F2710.2680
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface RotatingSpillage RotatingCoolingSX Side 1
  Boundary Type = INTERFACE
  Location = F2671.2680
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface RotatingSpillage SpillageSX Side 1
  Boundary Type = INTERFACE
  Location = F2722.2680,F2723.2680,F2724.2680,F2725.2680,F2726.2680
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface SpillageCENTER RotatingSpillage Side 2
  Boundary Type = INTERFACE
  Location = F1847.2680
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: ROTATING SPILLAGE Default
  Boundary Type = WALL
  Frame Type = Rotating
  Location = \
  F235.2680,F2673.2680,F2709.2680,F73.2680,F74.2680,F75.2680,F76.2680,F\
  870.2680,F871.2680,F890.2680,F914.2680,F917.2680,F949.2680,F950.2680
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  BOUNDARY: StaticWalls Spillage
  Boundary Type = WALL
  Frame Type = Rotating
  Location = \
  F1848.2680,F241.2680,F2682.2680,F331.2680,F332.2680,F333.2680,F334.26\
  80,F335.2680,F336.2680,F337.2680,F338.2680,F339.2680,F340.2680,F341.2\
  680,F342.2680,F362.2680,F395.2680,F396.2680,F397.2680,F398.2680,F399.\
  2680,F400.2680,F72.2680,F201.2680
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  DOMAIN MODELS:
  BUOYANCY MODEL:
  Option = Non Buoyant
  END
  DOMAIN MOTION:
  Alternate Rotation Model = true
  Angular Velocity = -1256.64 [radian s^-1]
  Option = Rotating
  AXIS DEFINITION:
  Option = Coordinate Axis
  Rotation Axis = Coord 0.3
  END
  END
  MESH DEFORMATION:
  Option = None
  END
  REFERENCE PRESSURE:
  Reference Pressure = 1 [atm]
  END
  END
  FLUID DEFINITION: Fluid 1
  Material = Water
  Option = Material Library
  MORPHOLOGY:
  Option = Continuous Fluid
  END
  END
  FLUID MODELS:
  COMBUSTION MODEL:
  Option = None
  END
  HEAT TRANSFER MODEL:
  Option = None
  END
  THERMAL RADIATION MODEL:
  Option = None
  END
  TURBULENCE MODEL:
  Option = SST
  END
  TURBULENT WALL FUNCTIONS:
  Option = Automatic
  END
  END
  END
  DOMAIN: SPILLAGE CENTER
  Coord Frame = Coord 0
  Domain Type = Fluid
  Location = B2862
  BOUNDARY: Interface SpillageCENTER RotatingSpillage Side 1
  Boundary Type = INTERFACE
  Location = F1847.2862
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface SpillageCENTER SpillageDX Side 1
  Boundary Type = INTERFACE
  Location = F2788.2862
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface SpillageCENTER SpillageSX Side 1
  Boundary Type = INTERFACE
  Location = F2764.2862
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface SpillageVolute SpillageCENTER Side 2
  Boundary Type = INTERFACE
  Location = F2763.2862
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: SPILLAGE CENTER Default
  Boundary Type = WALL
  Location = \
  F2768.2862,F2770.2862,F2790.2862,F2793.2862,F2864.2862,F326.2862,F343\
  .2862,F347.2862,F349.2862,F350.2862,F351.2862,F71.2862
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  DOMAIN MODELS:
  BUOYANCY MODEL:
  Option = Non Buoyant
  END
  DOMAIN MOTION:
  Option = Stationary
  END
  MESH DEFORMATION:
  Option = None
  END
  REFERENCE PRESSURE:
  Reference Pressure = 1 [atm]
  END
  END
  FLUID DEFINITION: Fluid 1
  Material = Water
  Option = Material Library
  MORPHOLOGY:
  Option = Continuous Fluid
  END
  END
  FLUID MODELS:
  COMBUSTION MODEL:
  Option = None
  END
  HEAT TRANSFER MODEL:
  Option = None
  END
  THERMAL RADIATION MODEL:
  Option = None
  END
  TURBULENCE MODEL:
  Option = SST
  END
  TURBULENT WALL FUNCTIONS:
  Option = Automatic
  END
  END
  END
  DOMAIN: SPILLAGE DX
  Coord Frame = Coord 0
  Domain Type = Fluid
  Location = B2802
  BOUNDARY: Interface SpillageCENTER SpillageDX Side 2
  Boundary Type = INTERFACE
  Location = F2788.2802
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface SpillageDX RotatingCoolingSX Side 1
  Boundary Type = INTERFACE
  Location = F207.2802
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: SPILLAGE DX Default
  Boundary Type = WALL
  Location = \
  F1855.2802,F2791.2802,F2792.2802,F328.2802,F329.2802,F330.2802
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  DOMAIN MODELS:
  BUOYANCY MODEL:
  Option = Non Buoyant
  END
  DOMAIN MOTION:
  Option = Stationary
  END
  MESH DEFORMATION:
  Option = None
  END
  REFERENCE PRESSURE:
  Reference Pressure = 1 [atm]
  END
  END
  FLUID DEFINITION: Fluid 1
  Material = Water
  Option = Material Library
  MORPHOLOGY:
  Option = Continuous Fluid
  END
  END
  FLUID MODELS:
  COMBUSTION MODEL:
  Option = None
  END
  HEAT TRANSFER MODEL:
  Option = None
  END
  THERMAL RADIATION MODEL:
  Option = None
  END
  TURBULENCE MODEL:
  Option = SST
  END
  TURBULENT WALL FUNCTIONS:
  Option = Automatic
  END
  END
  END
  DOMAIN: SPILLAGE SX
  Coord Frame = Coord 0
  Domain Type = Fluid
  Location = B30
  BOUNDARY: Interface RotatingSpillage SpillageSX Side 2
  Boundary Type = INTERFACE
  Location = F2722.30,F2723.30,F2724.30,F2725.30,F2726.30
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface SpillageCENTER SpillageSX Side 2
  Boundary Type = INTERFACE
  Location = F2764.30
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: SPILLAGE SX Default
  Boundary Type = WALL
  Location = \
  F246.30,F247.30,F248.30,F249.30,F250.30,F251.30,F252.30,F253.30,F2769\
  .30,F344.30,F352.30,F353.30,F354.30,F355.30,F356.30,F357.30,F358.30,F\
  359.30,F360.30,F361.30,F363.30,F364.30,F365.30,F366.30,F367.30,F368.3\
  0,F369.30,F370.30,F371.30,F372.30,F373.30,F374.30,F375.30,F376.30,F37\
  7.30,F378.30,F379.30,F380.30,F381.30,F382.30,F383.30,F384.30,F385.30,\
  F386.30,F387.30,F388.30,F389.30,F390.30,F391.30,F392.30,F393.30,F394.\
  30
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  DOMAIN MODELS:
  BUOYANCY MODEL:
  Option = Non Buoyant
  END
  DOMAIN MOTION:
  Option = Stationary
  END
  MESH DEFORMATION:
  Option = None
  END
  REFERENCE PRESSURE:
  Reference Pressure = 1 [atm]
  END
  END
  FLUID DEFINITION: Fluid 1
  Material = Water
  Option = Material Library
  MORPHOLOGY:
  Option = Continuous Fluid
  END
  END
  FLUID MODELS:
  COMBUSTION MODEL:
  Option = None
  END
  HEAT TRANSFER MODEL:
  Option = None
  END
  THERMAL RADIATION MODEL:
  Option = None
  END
  TURBULENCE MODEL:
  Option = SST
  END
  TURBULENT WALL FUNCTIONS:
  Option = Automatic
  END
  END
  END
  DOMAIN: SPILLAGE VOLUTE
  Coord Frame = Coord 0
  Domain Type = Fluid
  Location = B2775
  BOUNDARY: Interface SpillageVolute SpillageCENTER Side 1
  Boundary Type = INTERFACE
  Location = F2763.2775
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface Volute SpillageVolute Side 2
  Boundary Type = INTERFACE
  Location = F2811.2775
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: SPILLAGE VOLUTE Default
  Boundary Type = WALL
  Location = F2767.2775
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  DOMAIN MODELS:
  BUOYANCY MODEL:
  Option = Non Buoyant
  END
  DOMAIN MOTION:
  Option = Stationary
  END
  MESH DEFORMATION:
  Option = None
  END
  REFERENCE PRESSURE:
  Reference Pressure = 1 [atm]
  END
  END
  FLUID DEFINITION: Fluid 1
  Material = Water
  Option = Material Library
  MORPHOLOGY:
  Option = Continuous Fluid
  END
  END
  FLUID MODELS:
  COMBUSTION MODEL:
  Option = None
  END
  HEAT TRANSFER MODEL:
  Option = None
  END
  THERMAL RADIATION MODEL:
  Option = None
  END
  TURBULENCE MODEL:
  Option = SST
  END
  TURBULENT WALL FUNCTIONS:
  Option = Automatic
  END
  END
  END
  DOMAIN: VOLUTE
  Coord Frame = Coord 0
  Domain Type = Fluid
  Location = B1834
  BOUNDARY: Interface Convergent Volute Side 2
  Boundary Type = INTERFACE
  Location = F1861.1834
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface RotatingImpeller Volute Side 2
  Boundary Type = INTERFACE
  Location = F2727.1834
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: Interface Volute SpillageVolute Side 1
  Boundary Type = INTERFACE
  Location = F2811.1834
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  END
  TURBULENCE:
  Option = Conservative Interface Flux
  END
  END
  END
  BOUNDARY: VOLUTE Default
  Boundary Type = WALL
  Location = \
  F1853.1834,F1862.1834,F1863.1834,F1864.1834,F1865.1834,F1866.1834,F40\
  1.1834,F402.1834,F403.1834,F404.1834,F405.1834,F406.1834,F407.1834,F4\
  08.1834,F409.1834,F410.1834,F411.1834,F412.1834,F413.1834,F414.1834,F\
  415.1834,F416.1834,F417.1834,F418.1834,F419.1834
  BOUNDARY CONDITIONS:
  MASS AND MOMENTUM:
  Option = No Slip Wall
  END
  WALL ROUGHNESS:
  Option = Smooth Wall
  END
  END
  END
  DOMAIN MODELS:
  BUOYANCY MODEL:
  Option = Non Buoyant
  END
  DOMAIN MOTION:
  Option = Stationary
  END
  MESH DEFORMATION:
  Option = None
  END
  REFERENCE PRESSURE:
  Reference Pressure = 1 [atm]
  END
  END
  FLUID DEFINITION: Fluid 1
  Material = Water
  Option = Material Library
  MORPHOLOGY:
  Option = Continuous Fluid
  END
  END
  FLUID MODELS:
  COMBUSTION MODEL:
  Option = None
  END
  HEAT TRANSFER MODEL:
  Option = None
  END
  THERMAL RADIATION MODEL:
  Option = None
  END
  TURBULENCE MODEL:
  Option = SST
  END
  TURBULENT WALL FUNCTIONS:
  Option = Automatic
  END
  END
  END
  DOMAIN INTERFACE: Interface Convergent Volute
  Boundary List1 = Interface Convergent Volute Side 1
  Boundary List2 = Interface Convergent Volute Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = None
  AXIS DEFINITION:
  Option = Coordinate Axis
  Rotation Axis = Coord 0.3
  END
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface Ducts RotatingCoolingDX Xdir
  Boundary List1 = Interface Ducts RotatingCoolingDX Xdir Side 1
  Boundary List2 = Interface Ducts RotatingCoolingDX Xdir Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = Automatic
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface Ducts RotatingCoolingDX Zdir
  Boundary List1 = Interface Ducts RotatingCoolingDX Zdir Side 1
  Boundary List2 = Interface Ducts RotatingCoolingDX Zdir Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = Automatic
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface Eulerian Intake
  Boundary List1 = Interface Eulerian Intake Side 1
  Boundary List2 = Interface Eulerian Intake Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = None
  AXIS DEFINITION:
  Option = Coordinate Axis
  Rotation Axis = Coord 0.3
  END
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface Intake IntakeMaze
  Boundary List1 = Interface Intake IntakeMaze Side 1
  Boundary List2 = Interface Intake IntakeMaze Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = None
  AXIS DEFINITION:
  Option = Coordinate Axis
  Rotation Axis = Coord 0.3
  END
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface IntakeMaze RotatingImpeller
  Boundary List1 = Interface IntakeMaze RotatingImpeller Side 1
  Boundary List2 = Interface IntakeMaze RotatingImpeller Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = Automatic
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface RotatingBolt RotatingImpeller
  Boundary List1 = Interface RotatingBolt RotatingImpeller Side 1
  Boundary List2 = Interface RotatingBolt RotatingImpeller Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = Automatic
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface RotatingBolt RotatingShaft
  Boundary List1 = Interface RotatingBolt RotatingShaft Side 1
  Boundary List2 = Interface RotatingBolt RotatingShaft Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = Automatic
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface RotatingCoolingCENTER RotatingCoolingDX
  Boundary List1 = Interface RotatingCoolingCENTER RotatingCoolingDX Side 1
  Boundary List2 = Interface RotatingCoolingCENTER RotatingCoolingDX Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = Automatic
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface RotatingCoolingDX RotatingShaft
  Boundary List1 = Interface RotatingCoolingDX RotatingShaft Side 1
  Boundary List2 = Interface RotatingCoolingDX RotatingShaft Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = None
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface RotatingCoolingSX RotatingCoolingCENTER
  Boundary List1 = Interface RotatingCoolingSX RotatingCoolingCENTER Side 1
  Boundary List2 = Interface RotatingCoolingSX RotatingCoolingCENTER Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = Automatic
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface RotatingImpeller RotatingSpillage
  Boundary List1 = Interface RotatingImpeller RotatingSpillage Side 1
  Boundary List2 = Interface RotatingImpeller RotatingSpillage Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = Automatic
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface RotatingImpeller Volute
  Boundary List1 = Interface RotatingImpeller Volute Side 1
  Boundary List2 = Interface RotatingImpeller Volute Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = Automatic
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface RotatingSpillage RotatingCoolingSX
  Boundary List1 = Interface RotatingSpillage RotatingCoolingSX Side 1
  Boundary List2 = Interface RotatingSpillage RotatingCoolingSX Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = Automatic
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface RotatingSpillage SpillageSX
  Boundary List1 = Interface RotatingSpillage SpillageSX Side 1
  Boundary List2 = Interface RotatingSpillage SpillageSX Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = Automatic
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface SpillageCENTER RotatingSpillage
  Boundary List1 = Interface SpillageCENTER RotatingSpillage Side 1
  Boundary List2 = Interface SpillageCENTER RotatingSpillage Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = Automatic
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface SpillageCENTER SpillageDX
  Boundary List1 = Interface SpillageCENTER SpillageDX Side 1
  Boundary List2 = Interface SpillageCENTER SpillageDX Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = None
  AXIS DEFINITION:
  Option = Coordinate Axis
  Rotation Axis = Coord 0.3
  END
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface SpillageCENTER SpillageSX
  Boundary List1 = Interface SpillageCENTER SpillageSX Side 1
  Boundary List2 = Interface SpillageCENTER SpillageSX Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = None
  AXIS DEFINITION:
  Option = Coordinate Axis
  Rotation Axis = Coord 0.3
  END
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface SpillageDX RotatingCoolingSX
  Boundary List1 = Interface SpillageDX RotatingCoolingSX Side 1
  Boundary List2 = Interface SpillageDX RotatingCoolingSX Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = Automatic
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface SpillageVolute SpillageCENTER
  Boundary List1 = Interface SpillageVolute SpillageCENTER Side 1
  Boundary List2 = Interface SpillageVolute SpillageCENTER Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = None
  AXIS DEFINITION:
  Option = Coordinate Axis
  Rotation Axis = Coord 0.3
  END
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  DOMAIN INTERFACE: Interface Volute SpillageVolute
  Boundary List1 = Interface Volute SpillageVolute Side 1
  Boundary List2 = Interface Volute SpillageVolute Side 2
  Interface Type = Fluid Fluid
  INTERFACE MODELS:
  Option = General Connection
  FRAME CHANGE:
  Option = Frozen Rotor
  END
  MASS AND MOMENTUM:
  Option = Conservative Interface Flux
  MOMENTUM INTERFACE MODEL:
  Option = None
  END
  END
  PITCH CHANGE:
  Option = None
  AXIS DEFINITION:
  Option = Coordinate Axis
  Rotation Axis = Coord 0.3
  END
  END
  END
  MESH CONNECTION:
  Option = GGI
  END
  END
  OUTPUT CONTROL:
  RESULTS:
  File Compression Level = Default
  Option = Standard
  END
  END
  SOLVER CONTROL:
  Turbulence Numerics = First Order
  ADVECTION SCHEME:
  Option = High Resolution
  END
  CONVERGENCE CONTROL:
  Length Scale Option = Conservative
  Maximum Number of Iterations = 500
  Minimum Number of Iterations = 1
  Timescale Control = Auto Timescale
  Timescale Factor = 10
  END
  CONVERGENCE CRITERIA:
  Residual Target = 1e-3
  Residual Type = RMS
  END
  DYNAMIC MODEL CONTROL:
  Global Dynamic Model Control = Yes
  END
  INTERRUPT CONTROL:
  Option = Any Interrupt
  CONVERGENCE CONDITIONS:
  Option = Default Conditions
  END
  END
  END
  END
  COMMAND FILE:
  Version = 21.1
  Results Version = 21.1
  END
  SIMULATION CONTROL:
  EXECUTION CONTROL:
  EXECUTABLE SELECTION:
  Double Precision = Yes
  Large Problem = No
  END
  INTERPOLATOR STEP CONTROL:
  Runtime Priority = Standard
  MEMORY CONTROL:
  Memory Allocation Factor = 1.0
  END
  END
  PARALLEL HOST LIBRARY:
  HOST DEFINITION: -------
  Host Architecture String = winnt-amd64
  Installation Root = C:\Program Files\ANSYS Inc\v%v\CFX
  END
  END
  PARTITIONER STEP CONTROL:
  Multidomain Option = Automatic
  Runtime Priority = Standard
  MEMORY CONTROL:
  Memory Allocation Factor = 1.0
  END
  PARTITION SMOOTHING:
  Maximum Partition Smoothing Sweeps = 100
  Option = Smooth
  END
  PARTITIONING TYPE:
  MeTiS Type = k-way
  Option = MeTiS
  Partition Size Rule = Automatic
  Partition Weight Factors = 0.25000, 0.25000, 0.25000, 0.25000
  END
  END
  RUN DEFINITION:
  Run Mode = Full
  Solver Input File = CFX.def
  Solver Results File = \
  C:/Users/-------/dp0_CFX_35\
  _Solution_35/CFX_003.res
  END
  SOLVER STEP CONTROL:
  Runtime Priority = Standard
  MEMORY CONTROL:
  Memory Allocation Factor = 1.0
  END
  PARALLEL ENVIRONMENT:
  Number of Processes = 4
  Start Method = Intel MPI Local Parallel
  Parallel Host List = ------*4
  END
  END
  END
  END
  
  +--------------------------------------------------------------------+
  | |
  | Partitioning |
  | |
  +--------------------------------------------------------------------+
  
  +--------------------------------------------------------------------+
  | |
  | ANSYS(R) CFX(R) Partitioner |
  | |
  | 2021 R1 |
  | Build 21.1 2020-11-09T17:12:37.550718 |
  | Mon Nov 9 19:04:23 GMTST 2020 |
  | |
  | Executable Attributes |
  | |
  | double-64bit-int32-archfort-optimised-std-lcomp |
  | |
  | (C) 1996-2021 ANSYS, Inc. |
  | |
  | All rights reserved. Unauthorized use, distribution or duplication |
  | is prohibited. This product is subject to U.S. laws governing |
  | export and re-export. For full Legal Notice, see documentation. |
  +--------------------------------------------------------------------+
  
  +--------------------------------------------------------------------+
  | Job Information at Start of Run |
  +--------------------------------------------------------------------+
  Run mode: partitioning run
  Host computer: ---- (PID:------)
  Job started: Tue Feb 8 10:08:49 2022
  +--------------------------------------------------------------------+
  | License Information |
  +--------------------------------------------------------------------+
- May 23, 2023 at 3:27 pm
  
  NickFL
  Subscriber
  
  It looks to be a partitioner error meaning that the job isn't even making to the solver. For the run from May 2023 you have only 2 partitions and that from Feb 2022 had 4. Also in there seems to be a results file. I am not a Workbench guy, does Workbench save the partitioning information so you don't have to repartition? And that maybe the original partitioning had a higher memory allocation due to the large number of interfaces. But usually if it runs into a memory error, the error message looks a little different. My first recommendation is try the local 4 like you had in Feb 2022. Get that working again. And make sure there are no special characters or spaces in your filename & path.
- May 23, 2023 at 3:36 pm
  
  Stefano Chieti
  Subscriber
  
  I posted the solver run with 2 partitions but I also tried with 4 partitions as the initial one. Either with partitions or serial, the result is the same.
  The old analysis was solved, I tried to solve it again on these days with the same setup and same solver controls, but it didn't work.
  - May 23, 2023 at 3:42 pm
    
    NickFL
    Subscriber
    
    Well something has changed and using Workbench it hides so much from you that debugging is often more difficult.
    The next thing is, open CFX in stand-alone mode. Continue running the C:/Users/-------/dp0_CFX_35\Solution_35/CFX_003.res file. Does this run?
    - May 23, 2023 at 4:40 pm
      
      Stefano Chieti
      Subscriber
      
      I tried what you suggested, the import of .res file in a CFX stand-alone was ok. When I select the "continue calculation" option I obtain the same return code. I tried in a brand new project and in the same initial project.
    - May 23, 2023 at 5:00 pm
      
      NickFL
      Subscriber
      
      So in stand-alone the res file was able to be run? That tells us that the solver license, installation and everything is working fine. Ant that there is nothing wrong with the setup. I do not recall if res files saves the partitions or whether it repartitions every time. What happens if you give it a different number of partitions when you run the res file.
      What does "continue calculation" mean? Is this a Workbench thing? It could mean your Workbench project is corrupted. This is why I typically run my studies in stand-alone. I wouldn't be able to help you recover the Workbench project.
    - May 23, 2023 at 5:23 pm
      
      Stefano Chieti
      Subscriber
      
      In stand-alone the .res file was imported in the solution block correctly. I.e. I could see the results in the CFX-Post.
      When triyng to run the .res file again, I obtain the error code object of the thread. Doesn't change with number of partitions or serial calculations.
      This is my original Workbench - Block AK is the where the .res solved correclty came from.
      This is the brand new project where I re-create the original one:
    - May 23, 2023 at 5:31 pm
      
      NickFL
      Subscriber
      
      Sorry I don’t do Workbench.
      And when I speak of stand-alone, I mean close Workbench and from the Windows Start Menu find CFX. This will start the CFX Launcher. Change the working directory to something appropriate, like where your files are. Then open the CFX Solver manager. Then in the Define Run window specify the working res file for the Solver Input File.
      In CFX the file can be run from a def or a res as they both have everything they need for the solve.
    - May 24, 2023 at 4:36 pm
      
      Stefano Chieti
      Subscriber
      
      I did exaclty what you suggested, so I opened a stand-alone CFX from Windows and retrieved the run information in Define Run window.
      I tried to run both the .def and the .res of the original project, the .def and the .res of the recreated project. I ever obtanied the same return code after the initialization of the partitioning (same applies for serial).
      The only difference is that the original .res file displayed the RMS curves on the monitor, but still exited at the partitioner.
    - May 24, 2023 at 4:39 pm
      
      NickFL
      Subscriber
      
      Have you tried simply solving flow through a pipe and seeing if you can get through the partitioning step?
    - May 24, 2023 at 4:51 pm
      
      Stefano Chieti
      Subscriber
      
      I'm going to have a quick test on it. I will keep you up to date!
    - May 25, 2023 at 10:02 am
      
      Stefano Chieti
      Subscriber
      
      I tried with a simple pipe flow, still got the same error.
      
      This run of the CFX GEOMETRY LICENSING PATCH 2021 R1 SP3 Solver started
      at 12:00:23 on 25 May 2023 by user Stefano.CHIETI on ----------
      (intel_xeon64.sse2_winnt) using the command:
      
      "C:\Program Files\ANSYS Inc\v211\CFX\bin\perllib\cfx5solve.pl" -batch
      -ccl runInput.ccl -fullname "CFD 2022_003"
      
      GEOMETRY LICENSING PATCH 2021 R1 SP3
      
      Point Releases and Patches installed:
      ANSYS, Inc. Products 2021 R1
      SpaceClaim 2021 R1
      Autodyn 2021 R1
      CFD-Post only 2021 R1
      CFX (includes CFD-Post) 2021 R1
      FENSAP-ICE 2021 R1
      Fluent (includes CFD-Post) 2021 R1
      Forte (includes EnSight) 2021 R1
      Polyflow (includes CFD-Post) 2021 R1
      TurboGrid 2021 R1
      Aqwa 2021 R1
      Customization Files for User Programmable Features 2021 R1
      Mechanical Products 2021 R1
      Icepak (includes CFD-Post) 2021 R1
      Remote Solve Manager Standalone Services 2021 R1
      Viewer 2021 R1
      ACIS Geometry Interface 2021 R1
      AutoCAD Geometry Interface 2021 R1
      Catia, Version 4 Geometry Interface 2021 R1
      Catia, Version 5 Geometry Interface 2021 R1
      Catia, Version 6 Geometry Interface 2021 R1
      Creo Elements/Direct Modeling Geometry Interface 2021 R1
      Creo Parametric Geometry Interface 2021 R1
      Inventor Geometry Interface 2021 R1
      JTOpen Geometry Interface 2021 R1
      NX Geometry Interface 2021 R1
      Parasolid Geometry Interface 2021 R1
      Solid Edge Geometry Interface 2021 R1
      SOLIDWORKS Geometry Interface 2021 R1
      ANSYS, Inc. License Manager 2021 R1
      Discovery 2021 R1.6
      Geometry Licensing Patch 2021 R1 SP3
      
      Setting up CFX Solver run ...
      
      +--------------------------------------------------------------------+
      | |
      | CFX Command Language for Run |
      | |
      +--------------------------------------------------------------------+
      
      LIBRARY:
      MATERIAL: Water
      Material Description = Water (liquid)
      Material Group = Water Data, Constant Property Liquids
      Option = Pure Substance
      Thermodynamic State = Liquid
      PROPERTIES:
      Option = General Material
      EQUATION OF STATE:
      Density = 997.0 [kg m^-3]
      Molar Mass = 18.02 [kg kmol^-1]
      Option = Value
      END
      SPECIFIC HEAT CAPACITY:
      Option = Value
      Specific Heat Capacity = 4181.7 [J kg^-1 K^-1]
      Specific Heat Type = Constant Pressure
      END
      REFERENCE STATE:
      Option = Specified Point
      Reference Pressure = 1 [atm]
      Reference Specific Enthalpy = 0.0 [J/kg]
      Reference Specific Entropy = 0.0 [J/kg/K]
      Reference Temperature = 25 [C]
      END
      DYNAMIC VISCOSITY:
      Dynamic Viscosity = 8.899E-4 [kg m^-1 s^-1]
      Option = Value
      END
      THERMAL CONDUCTIVITY:
      Option = Value
      Thermal Conductivity = 0.6069 [W m^-1 K^-1]
      END
      ABSORPTION COEFFICIENT:
      Absorption Coefficient = 1.0 [m^-1]
      Option = Value
      END
      SCATTERING COEFFICIENT:
      Option = Value
      Scattering Coefficient = 0.0 [m^-1]
      END
      REFRACTIVE INDEX:
      Option = Value
      Refractive Index = 1.0 [m m^-1]
      END
      THERMAL EXPANSIVITY:
      Option = Value
      Thermal Expansivity = 2.57E-04 [K^-1]
      END
      END
      END
      END
      FLOW: Flow Analysis 1
      SOLUTION UNITS:
      Angle Units = [rad]
      Length Units = [m]
      Mass Units = [kg]
      Solid Angle Units = [sr]
      Temperature Units = [K]
      Time Units = [s]
      END
      ANALYSIS TYPE:
      Option = Steady State
      EXTERNAL SOLVER COUPLING:
      Option = None
      END
      END
      DOMAIN: Default Domain
      Coord Frame = Coord 0
      Domain Type = Fluid
      Location = B32
      BOUNDARY: inlet
      Boundary Type = INLET
      Location = F197.32
      BOUNDARY CONDITIONS:
      FLOW REGIME:
      Option = Subsonic
      END
      MASS AND MOMENTUM:
      Normal Speed = 0.005 [m s^-1]
      Option = Normal Speed
      END
      TURBULENCE:
      Option = Medium Intensity and Eddy Viscosity Ratio
      END
      END
      END
      BOUNDARY: outlet
      Boundary Type = OUTLET
      Location = F34.32
      BOUNDARY CONDITIONS:
      FLOW REGIME:
      Option = Subsonic
      END
      MASS AND MOMENTUM:
      Option = Average Static Pressure
      Pressure Profile Blend = 0.05
      Relative Pressure = 0 [Pa]
      END
      PRESSURE AVERAGING:
      Option = Average Over Whole Outlet
      END
      END
      END
      BOUNDARY: wall
      Boundary Type = WALL
      Location = F33.32
      BOUNDARY CONDITIONS:
      MASS AND MOMENTUM:
      Option = No Slip Wall
      END
      WALL ROUGHNESS:
      Option = Smooth Wall
      END
      END
      END
      DOMAIN MODELS:
      BUOYANCY MODEL:
      Option = Non Buoyant
      END
      DOMAIN MOTION:
      Option = Stationary
      END
      MESH DEFORMATION:
      Option = None
      END
      REFERENCE PRESSURE:
      Reference Pressure = 1 [atm]
      END
      END
      FLUID DEFINITION: Fluid 1
      Material = Water
      Option = Material Library
      MORPHOLOGY:
      Option = Continuous Fluid
      END
      END
      FLUID MODELS:
      COMBUSTION MODEL:
      Option = None
      END
      HEAT TRANSFER MODEL:
      Fluid Temperature = 25 [C]
      Option = Isothermal
      END
      THERMAL RADIATION MODEL:
      Option = None
      END
      TURBULENCE MODEL:
      Option = k epsilon
      END
      TURBULENT WALL FUNCTIONS:
      Option = Scalable
      END
      END
      END
      OUTPUT CONTROL:
      RESULTS:
      File Compression Level = Default
      Option = Standard
      END
      END
      SOLVER CONTROL:
      Turbulence Numerics = First Order
      ADVECTION SCHEME:
      Option = High Resolution
      END
      CONVERGENCE CONTROL:
      Length Scale Option = Conservative
      Maximum Number of Iterations = 100
      Minimum Number of Iterations = 1
      Timescale Control = Auto Timescale
      Timescale Factor = 1.0
      END
      CONVERGENCE CRITERIA:
      Residual Target = 1.E-4
      Residual Type = RMS
      END
      DYNAMIC MODEL CONTROL:
      Global Dynamic Model Control = On
      END
      INTERRUPT CONTROL:
      Option = Any Interrupt
      CONVERGENCE CONDITIONS:
      Option = Default Conditions
      END
      END
      END
      END
      COMMAND FILE:
      Version = 21.1
      Results Version = 21.1
      END
      SIMULATION CONTROL:
      EXECUTION CONTROL:
      EXECUTABLE SELECTION:
      Double Precision = No
      Large Problem = No
      END
      INTERPOLATOR STEP CONTROL:
      Runtime Priority = Standard
      MEMORY CONTROL:
      Memory Allocation Factor = 1.0
      END
      END
      PARALLEL HOST LIBRARY:
      HOST DEFINITION: ---------
      Host Architecture String = winnt-amd64
      Installation Root = C:\Program Files\ANSYS Inc\v%v\CFX
      END
      END
      PARTITIONER STEP CONTROL:
      Multidomain Option = Automatic
      Runtime Priority = Standard
      MEMORY CONTROL:
      Memory Allocation Factor = 1.0
      END
      PARTITION SMOOTHING:
      Maximum Partition Smoothing Sweeps = 100
      Option = Smooth
      END
      PARTITIONING TYPE:
      MeTiS Type = k-way
      Option = MeTiS
      Partition Size Rule = Automatic
      END
      END
      RUN DEFINITION:
      Run Mode = Full
      Solver Input File = CFD 2022.def
      Solver Results File = \
      C:/Users/Stefano.CHIETI/Desktop/----------/-CFD_pending/dp0_CFX_Solution/CFD 2022_003.res
      END
      SOLVER STEP CONTROL:
      Runtime Priority = Standard
      MEMORY CONTROL:
      Memory Allocation Factor = 1.0
      END
      PARALLEL ENVIRONMENT:
      Number of Processes = 1
      Start Method = Serial
      END
      END
      END
      END
      
      +--------------------------------------------------------------------+
      | |
      | Solver |
      | |
      +--------------------------------------------------------------------+
      
      +--------------------------------------------------------------------+
      | |
      | ANSYS(R) CFX(R) Solver |
      | |
      +--------------------------------------------------------------------+
      | An error has occurred in cfx5solve: |
      | |
      | The ANSYS CFX solver exited with return code 1. No results file |
      | has been created. |
      +--------------------------------------------------------------------+
      End of solution stage.
      +--------------------------------------------------------------------+
      | For CFX runs launched from Workbench, the final locations of |
      | directories and files generated may differ from those shown. |
      +--------------------------------------------------------------------+
      
      This run of the ANSYS CFX Solver has finished.
    - May 25, 2023 at 10:15 am
      NickFL
      Subscriber
      
      Ok, I think you are at the limit of how I can help. My suggest course would be:
      
      Uninstall. Restart the computer. Reinstall & make sure your antivirus software is turned off (yep, sometimes that is necessary). And if you are going to reinstall, you may as well upgrade.
      Contact your IT team at school or work. They might know a way to identify what is blocking it from running.
    - May 25, 2023 at 10:19 am
      
      Stefano Chieti
      Subscriber
      
      The firewall theme was my very first concern.
      Hope that will really be the problem.
      Anyway, a really big thank to you for the support. I'll let you know if and when I'll hopefully find a resolution!
    - May 29, 2023 at 10:57 am
      
      Stefano Chieti
      Subscriber
      
      Hello, I finally managed to solve the error.
      After many attempts, I uninstalled and reinstalled the software as per Ansys Customer Support suggest.
      Probably it was a License Manager release problem that could not update since 2021.
      
      Thank you all again for the support!

Viewing 4 reply threads

The topic ‘An error has occurred in cfx5solve:The ANSYS CFX solver exited with return code1’ is closed to new replies.

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