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May 22, 2023 at 3:28 pm
Stefano Chieti
SubscriberHello,
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 EmployeeHello 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 pmSubscriber
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 |
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+--------------------------------------------------------------------+
+--------------------------------------------------------------------+
| Job Information at Start of Run |
+--------------------------------------------------------------------+Run mode: partitioning run
Host computer: ---- (PID:------)
Job started: Tue Feb 8 10:08:49 2022
+--------------------------------------------------------------------+
| License Information |
+--------------------------------------------------------------------+
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May 23, 2023 at 3:27 pm
NickFL
SubscriberIt 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 pmSubscriber
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.
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May 23, 2023 at 3:42 pmSubscriber
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?
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May 23, 2023 at 4:40 pmSubscriber
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.
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May 23, 2023 at 5:00 pmSubscriber
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.
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May 23, 2023 at 5:23 pmSubscriber
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:
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May 23, 2023 at 5:31 pmSubscriber
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.
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May 24, 2023 at 4:36 pmSubscriber
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.
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May 24, 2023 at 4:39 pmSubscriber
Have you tried simply solving flow through a pipe and seeing if you can get through the partitioning step?
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May 24, 2023 at 4:51 pmSubscriber
I'm going to have a quick test on it. I will keep you up to date!
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May 25, 2023 at 10:02 amSubscriber
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 amSubscriber
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.
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May 25, 2023 at 10:19 amSubscriber
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!
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May 29, 2023 at 10:57 amSubscriber
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!
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- 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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