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Created Diff never expires
23 removals
995 lines
21 additions
993 lines
This run of the CFX Release 19.2 Solver started at 11:14:10 on 11 Jul
This run of the CFX Release 19.2 Solver started at 16:01:45 on 15 Jul
2024 by user Emre on DESKTOP-6FIBNC0 (intel_xeon64.sse2_winnt) using
2024 by user Emre on DESKTOP-6FIBNC0 (intel_xeon64.sse2_winnt) using
the command:
the command:
"C:\Program Files\ANSYS Inc\v192\CFX\bin\perllib\cfx5solve.pl" -batch
"C:\Program Files\ANSYS Inc\v192\CFX\bin\perllib\cfx5solve.pl" -batch
-ccl runInput.ccl -fullname "Fluid Flow CFX_001"
-ccl runInput.ccl -fullname "Fluid Flow CFX_001"
Release 19.2
Release 19.2
Point Releases and Patches installed:
Point Releases and Patches installed:
ANSYS, Inc. Products Release 19.2
ANSYS, Inc. Products Release 19.2
SpaceClaim Release 19.2
SpaceClaim Release 19.2
AIM Release 19.2
AIM Release 19.2
Autodyn Release 19.2
Autodyn Release 19.2
LS-DYNA Release 19.2
LS-DYNA Release 19.2
CFX (includes CFD-Post) Release 19.2
CFX (includes CFD-Post) Release 19.2
Chemkin Release 19.2
Chemkin Release 19.2
EnSight Release 19.2
EnSight Release 19.2
FENSAP-ICE Release 19.2
FENSAP-ICE Release 19.2
Fluent (includes CFD-Post) Release 19.2
Fluent (includes CFD-Post) Release 19.2
Forte Release 19.2
Forte Release 19.2
Polyflow (includes CFD-Post) Release 19.2
Polyflow (includes CFD-Post) Release 19.2
TurboGrid Release 19.2
TurboGrid Release 19.2
ICEM CFD Release 19.2
ICEM CFD Release 19.2
Aqwa Release 19.2
Aqwa Release 19.2
Mechanical Products Release 19.2
Mechanical Products Release 19.2
Icepak (includes CFD-Post) Release 19.2
Icepak (includes CFD-Post) Release 19.2
ACIS Geometry Interface Release 19.2
ACIS Geometry Interface Release 19.2
AutoCAD Geometry Interface Release 19.2
AutoCAD Geometry Interface Release 19.2
Catia, Version 4 Geometry Interface Release 19.2
Catia, Version 4 Geometry Interface Release 19.2
Catia, Version 6 Geometry Interface Release 19.2
Catia, Version 6 Geometry Interface Release 19.2
Creo Elements/Direct Modeling Geometry Interface Release 19.2
Creo Elements/Direct Modeling Geometry Interface Release 19.2
Creo Parametric Geometry Interface Release 19.2
Creo Parametric Geometry Interface Release 19.2
Inventor Geometry Interface Release 19.2
Inventor Geometry Interface Release 19.2
JTOpen Geometry Interface Release 19.2
JTOpen Geometry Interface Release 19.2
NX Geometry Interface Release 19.2
NX Geometry Interface Release 19.2
Parasolid Geometry Interface Release 19.2
Parasolid Geometry Interface Release 19.2
Solid Edge Geometry Interface Release 19.2
Solid Edge Geometry Interface Release 19.2
SOLIDWORKS Geometry Interface Release 19.2
SOLIDWORKS Geometry Interface Release 19.2
ANSYS, Inc. License Manager Release 19.2
ANSYS, Inc. License Manager Release 19.2
Setting up CFX Solver run ...
Setting up CFX Solver run ...
+--------------------------------------------------------------------+
+--------------------------------------------------------------------+
| |
| |
| CFX Command Language for Run |
| CFX Command Language for Run |
| |
| |
+--------------------------------------------------------------------+
+--------------------------------------------------------------------+
LIBRARY:
LIBRARY:
CEL:
CEL:
EXPRESSIONS:
EXPRESSIONS:
Pidffmoni = massFlowAveAbs(Total Pressure in Stn Frame)@S3 \
Pidffmoni = massFlowAveAbs(Total Pressure in Stn Frame)@S3 \
Outlet-massFlowAveAbs(Total Pressure in Stn Frame)@R1 Inlet
Outlet-massFlowAveAbs(Total Pressure in Stn Frame)@R1 Inlet
END
END
END
END
MATERIAL: Air at 25 C
MATERIAL: Air Ideal Gas
Material Description = Air at 25 C and 1 atm (dry)
Material Description = Air Ideal Gas (constant Cp)
Material Group = Air Data, Constant Property Gases
Material Group = Air Data, Calorically Perfect Ideal Gases
Option = Pure Substance
Option = Pure Substance
Thermodynamic State = Gas
Thermodynamic State = Gas
PROPERTIES:
PROPERTIES:
Option = General Material
Option = General Material
EQUATION OF STATE:
EQUATION OF STATE:
Density = 1.185 [kg m^-3]
Molar Mass = 28.96 [kg kmol^-1]
Molar Mass = 28.96 [kg kmol^-1]
Option = Value
Option = Ideal Gas
END
END
SPECIFIC HEAT CAPACITY:
SPECIFIC HEAT CAPACITY:
Option = Value
Option = Value
Specific Heat Capacity = 1.0044E+03 [J kg^-1 K^-1]
Specific Heat Capacity = 1.0044E+03 [J kg^-1 K^-1]
Specific Heat Type = Constant Pressure
Specific Heat Type = Constant Pressure
END
END
REFERENCE STATE:
REFERENCE STATE:
Option = Specified Point
Option = Specified Point
Reference Pressure = 1 [atm]
Reference Pressure = 1 [atm]
Reference Specific Enthalpy = 0. [J/kg]
Reference Specific Enthalpy = 0. [J/kg]
Reference Specific Entropy = 0. [J/kg/K]
Reference Specific Entropy = 0. [J/kg/K]
Reference Temperature = 25 [C]
Reference Temperature = 25 [C]
END
END
DYNAMIC VISCOSITY:
DYNAMIC VISCOSITY:
Dynamic Viscosity = 1.831E-05 [kg m^-1 s^-1]
Dynamic Viscosity = 1.831E-05 [kg m^-1 s^-1]
Option = Value
Option = Value
END
END
THERMAL CONDUCTIVITY:
THERMAL CONDUCTIVITY:
Option = Value
Option = Value
Thermal Conductivity = 2.61E-02 [W m^-1 K^-1]
Thermal Conductivity = 2.61E-2 [W m^-1 K^-1]
END
END
ABSORPTION COEFFICIENT:
ABSORPTION COEFFICIENT:
Absorption Coefficient = 0.01 [m^-1]
Absorption Coefficient = 0.01 [m^-1]
Option = Value
Option = Value
END
END
SCATTERING COEFFICIENT:
SCATTERING COEFFICIENT:
Option = Value
Option = Value
Scattering Coefficient = 0.0 [m^-1]
Scattering Coefficient = 0.0 [m^-1]
END
END
REFRACTIVE INDEX:
REFRACTIVE INDEX:
Option = Value
Option = Value
Refractive Index = 1.0 [m m^-1]
Refractive Index = 1.0 [m m^-1]
END
THERMAL EXPANSIVITY:
Option = Value
Thermal Expansivity = 0.003356 [K^-1]
END
END
END
END
END
END
END
END
FLOW: Flow Analysis 1
FLOW: Flow Analysis 1
SOLUTION UNITS:
SOLUTION UNITS:
Angle Units = [rad]
Angle Units = [rad]
Length Units = [m]
Length Units = [m]
Mass Units = [kg]
Mass Units = [kg]
Solid Angle Units = [sr]
Solid Angle Units = [sr]
Temperature Units = [K]
Temperature Units = [K]
Time Units = [s]
Time Units = [s]
END
END
ANALYSIS TYPE:
ANALYSIS TYPE:
Option = Steady State
Option = Steady State
EXTERNAL SOLVER COUPLING:
EXTERNAL SOLVER COUPLING:
Option = None
Option = None
END
END
END
END
DOMAIN: R1
DOMAIN: R1
Coord Frame = Coord 0
Coord Frame = Coord 0
Domain Type = Fluid
Domain Type = Fluid
Location = Passage
Location = Passage
BOUNDARY: R1 Blade
BOUNDARY: R1 Blade
Boundary Type = WALL
Boundary Type = WALL
Frame Type = Rotating
Frame Type = Rotating
Location = BLADE
Location = BLADE
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Adiabatic
Option = Adiabatic
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = No Slip Wall
Option = No Slip Wall
END
END
WALL ROUGHNESS:
WALL ROUGHNESS:
Option = Smooth Wall
Option = Smooth Wall
END
END
END
END
END
END
BOUNDARY: R1 Hub
BOUNDARY: R1 Hub
Boundary Type = WALL
Boundary Type = WALL
Coord Frame = Coord 0
Coord Frame = Coord 0
Frame Type = Rotating
Frame Type = Rotating
Location = HUB
Location = HUB
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Adiabatic
Option = Adiabatic
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = No Slip Wall
Option = No Slip Wall
END
END
WALL ROUGHNESS:
WALL ROUGHNESS:
Option = Smooth Wall
Option = Smooth Wall
END
END
END
END
END
END
BOUNDARY: R1 Inlet
BOUNDARY: R1 Inlet
Boundary Type = INLET
Boundary Type = INLET
Frame Type = Stationary
Frame Type = Stationary
Location = INFLOW
Location = INFLOW
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
FLOW DIRECTION:
FLOW DIRECTION:
Option = Normal to Boundary Condition
Option = Normal to Boundary Condition
END
END
FLOW REGIME:
FLOW REGIME:
Option = Subsonic
Option = Subsonic
END
END
HEAT TRANSFER:
HEAT TRANSFER:
Option = Stationary Frame Total Temperature
Option = Stationary Frame Total Temperature
Stationary Frame Total Temperature = 288 [K]
Stationary Frame Total Temperature = 288 [K]
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = Stationary Frame Total Pressure
Option = Stationary Frame Total Pressure
Relative Pressure = 1 [atm]
Relative Pressure = 1 [atm]
END
END
TURBULENCE:
TURBULENCE:
Option = Medium Intensity and Eddy Viscosity Ratio
Option = Medium Intensity and Eddy Viscosity Ratio
END
END
END
END
END
END
BOUNDARY: R1 Shroud
BOUNDARY: R1 Shroud
Boundary Type = WALL
Boundary Type = WALL
Coord Frame = Coord 0
Coord Frame = Coord 0
Frame Type = Rotating
Frame Type = Rotating
Location = SHROUD
Location = SHROUD
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Adiabatic
Option = Adiabatic
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = No Slip Wall
Option = No Slip Wall
END
END
WALL ROUGHNESS:
WALL ROUGHNESS:
Option = Smooth Wall
Option = Smooth Wall
END
END
END
END
END
END
BOUNDARY: R1 to R1 Periodic 1 Side 1
BOUNDARY: R1 to R1 Periodic 1 Side 1
Boundary Type = INTERFACE
Boundary Type = INTERFACE
Location = PER1
Location = PER1
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
TURBULENCE:
TURBULENCE:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
END
END
END
END
BOUNDARY: R1 to R1 Periodic 1 Side 2
BOUNDARY: R1 to R1 Periodic 1 Side 2
Boundary Type = INTERFACE
Boundary Type = INTERFACE
Location = PER2
Location = PER2
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
TURBULENCE:
TURBULENCE:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
END
END
END
END
BOUNDARY: S1 to R1 Side 2
BOUNDARY: S1 to R1 Side 2
Boundary Type = INTERFACE
Boundary Type = INTERFACE
Location = OUTFLOW
Location = OUTFLOW
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
TURBULENCE:
TURBULENCE:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
END
END
END
END
DOMAIN MODELS:
DOMAIN MODELS:
BUOYANCY MODEL:
BUOYANCY MODEL:
Option = Non Buoyant
Option = Non Buoyant
END
END
DOMAIN MOTION:
DOMAIN MOTION:
Alternate Rotation Model = true
Alternate Rotation Model = true
Angular Velocity = 19451 [rev min^-1]
Angular Velocity = 19451 [rev min^-1]
Option = Rotating
Option = Rotating
AXIS DEFINITION:
AXIS DEFINITION:
Option = Coordinate Axis
Option = Coordinate Axis
Rotation Axis = Coord 0.3
Rotation Axis = Coord 0.3
END
END
END
END
MESH DEFORMATION:
MESH DEFORMATION:
Option = None
Option = None
END
END
REFERENCE PRESSURE:
REFERENCE PRESSURE:
Reference Pressure = 0 [atm]
Reference Pressure = 0 [atm]
END
END
END
END
FLUID DEFINITION: Fluid 1
FLUID DEFINITION: Air Ideal Gas
Material = Air at 25 C
Material = Air Ideal Gas
Option = Material Library
Option = Material Library
MORPHOLOGY:
MORPHOLOGY:
Option = Continuous Fluid
Option = Continuous Fluid
END
END
END
END
FLUID MODELS:
FLUID MODELS:
COMBUSTION MODEL:
COMBUSTION MODEL:
Option = None
Option = None
END
END
HEAT TRANSFER MODEL:
HEAT TRANSFER MODEL:
Include Viscous Work Term = True
Include Viscous Work Term = True
Option = Total Energy
Option = Total Energy
END
END
THERMAL RADIATION MODEL:
THERMAL RADIATION MODEL:
Option = None
Option = None
END
END
TURBULENCE MODEL:
TURBULENCE MODEL:
Option = SST
Option = SST
END
END
TURBULENT WALL FUNCTIONS:
TURBULENT WALL FUNCTIONS:
High Speed Model = Off
High Speed Model = Off
Option = Automatic
Option = Automatic
END
END
END
END
END
END
DOMAIN: R2
DOMAIN: R2
Coord Frame = Coord 0
Coord Frame = Coord 0
Domain Type = Fluid
Domain Type = Fluid
Location = Passage 3
Location = Passage 3
BOUNDARY: R2 Blade
BOUNDARY: R2 Blade
Boundary Type = WALL
Boundary Type = WALL
Frame Type = Rotating
Frame Type = Rotating
Location = BLADE 3
Location = BLADE 3
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Adiabatic
Option = Adiabatic
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = No Slip Wall
Option = No Slip Wall
END
END
WALL ROUGHNESS:
WALL ROUGHNESS:
Option = Smooth Wall
Option = Smooth Wall
END
END
END
END
END
END
BOUNDARY: R2 Hub
BOUNDARY: R2 Hub
Boundary Type = WALL
Boundary Type = WALL
Coord Frame = Coord 0
Coord Frame = Coord 0
Frame Type = Rotating
Frame Type = Rotating
Location = HUB 3
Location = HUB 3
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Adiabatic
Option = Adiabatic
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = No Slip Wall
Option = No Slip Wall
END
END
WALL ROUGHNESS:
WALL ROUGHNESS:
Option = Smooth Wall
Option = Smooth Wall
END
END
END
END
END
END
BOUNDARY: R2 Shroud
BOUNDARY: R2 Shroud
Boundary Type = WALL
Boundary Type = WALL
Coord Frame = Coord 0
Coord Frame = Coord 0
Frame Type = Rotating
Frame Type = Rotating
Location = SHROUD 3
Location = SHROUD 3
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Adiabatic
Option = Adiabatic
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = No Slip Wall
Option = No Slip Wall
END
END
WALL ROUGHNESS:
WALL ROUGHNESS:
Option = Smooth Wall
Option = Smooth Wall
END
END
END
END
END
END
BOUNDARY: R2 to R2 Periodic 1 Side 1
BOUNDARY: R2 to R2 Periodic 1 Side 1
Boundary Type = INTERFACE
Boundary Type = INTERFACE
Location = PER1 3
Location = PER1 3
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
TURBULENCE:
TURBULENCE:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
END
END
END
END
BOUNDARY: R2 to R2 Periodic 1 Side 2
BOUNDARY: R2 to R2 Periodic 1 Side 2
Boundary Type = INTERFACE
Boundary Type = INTERFACE
Location = PER2 3
Location = PER2 3
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
TURBULENCE:
TURBULENCE:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
END
END
END
END
BOUNDARY: R2 to S1 Side 1
BOUNDARY: R2 to S1 Side 1
Boundary Type = INTERFACE
Boundary Type = INTERFACE
Location = INFLOW 3
Location = INFLOW 3
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
TURBULENCE:
TURBULENCE:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
END
END
END
END
BOUNDARY: S2 to R2 Side 2
BOUNDARY: S2 to R2 Side 2
Boundary Type = INTERFACE
Boundary Type = INTERFACE
Location = OUTFLOW 3
Location = OUTFLOW 3
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
TURBULENCE:
TURBULENCE:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
END
END
END
END
DOMAIN MODELS:
DOMAIN MODELS:
BUOYANCY MODEL:
BUOYANCY MODEL:
Option = Non Buoyant
Option = Non Buoyant
END
END
DOMAIN MOTION:
DOMAIN MOTION:
Alternate Rotation Model = true
Alternate Rotation Model = true
Angular Velocity = 19451 [rev min^-1]
Angular Velocity = 19451 [rev min^-1]
Option = Rotating
Option = Rotating
AXIS DEFINITION:
AXIS DEFINITION:
Option = Coordinate Axis
Option = Coordinate Axis
Rotation Axis = Coord 0.3
Rotation Axis = Coord 0.3
END
END
END
END
MESH DEFORMATION:
MESH DEFORMATION:
Option = None
Option = None
END
END
REFERENCE PRESSURE:
REFERENCE PRESSURE:
Reference Pressure = 0 [atm]
Reference Pressure = 0 [atm]
END
END
END
END
FLUID DEFINITION: Fluid 1
FLUID DEFINITION: Air Ideal Gas
Material = Air at 25 C
Material = Air Ideal Gas
Option = Material Library
Option = Material Library
MORPHOLOGY:
MORPHOLOGY:
Option = Continuous Fluid
Option = Continuous Fluid
END
END
END
END
FLUID MODELS:
FLUID MODELS:
COMBUSTION MODEL:
COMBUSTION MODEL:
Option = None
Option = None
END
END
HEAT TRANSFER MODEL:
HEAT TRANSFER MODEL:
Include Viscous Work Term = True
Include Viscous Work Term = True
Option = Total Energy
Option = Total Energy
END
END
THERMAL RADIATION MODEL:
THERMAL RADIATION MODEL:
Option = None
Option = None
END
END
TURBULENCE MODEL:
TURBULENCE MODEL:
Option = SST
Option = SST
END
END
TURBULENT WALL FUNCTIONS:
TURBULENT WALL FUNCTIONS:
High Speed Model = Off
High Speed Model = Off
Option = Automatic
Option = Automatic
END
END
END
END
END
END
DOMAIN: R3
DOMAIN: R3
Coord Frame = Coord 0
Coord Frame = Coord 0
Domain Type = Fluid
Domain Type = Fluid
Location = Passage 5
Location = Passage 5
BOUNDARY: R3 Blade
BOUNDARY: R3 Blade
Boundary Type = WALL
Boundary Type = WALL
Frame Type = Rotating
Frame Type = Rotating
Location = BLADE 5
Location = BLADE 5
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Adiabatic
Option = Adiabatic
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = No Slip Wall
Option = No Slip Wall
END
END
WALL ROUGHNESS:
WALL ROUGHNESS:
Option = Smooth Wall
Option = Smooth Wall
END
END
END
END
END
END
BOUNDARY: R3 Hub
BOUNDARY: R3 Hub
Boundary Type = WALL
Boundary Type = WALL
Coord Frame = Coord 0
Coord Frame = Coord 0
Frame Type = Rotating
Frame Type = Rotating
Location = HUB 5
Location = HUB 5
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Adiabatic
Option = Adiabatic
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = No Slip Wall
Option = No Slip Wall
END
END
WALL ROUGHNESS:
WALL ROUGHNESS:
Option = Smooth Wall
Option = Smooth Wall
END
END
END
END
END
END
BOUNDARY: R3 Shroud
BOUNDARY: R3 Shroud
Boundary Type = WALL
Boundary Type = WALL
Coord Frame = Coord 0
Coord Frame = Coord 0
Frame Type = Rotating
Frame Type = Rotating
Location = SHROUD 5
Location = SHROUD 5
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Adiabatic
Option = Adiabatic
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = No Slip Wall
Option = No Slip Wall
END
END
WALL ROUGHNESS:
WALL ROUGHNESS:
Option = Smooth Wall
Option = Smooth Wall
END
END
END
END
END
END
BOUNDARY: R3 to R3 Periodic 1 Side 1
BOUNDARY: R3 to R3 Periodic 1 Side 1
Boundary Type = INTERFACE
Boundary Type = INTERFACE
Location = PER1 5
Location = PER1 5
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
TURBULENCE:
TURBULENCE:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
END
END
END
END
BOUNDARY: R3 to R3 Periodic 1 Side 2
BOUNDARY: R3 to R3 Periodic 1 Side 2
Boundary Type = INTERFACE
Boundary Type = INTERFACE
Location = PER2 5
Location = PER2 5
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
TURBULENCE:
TURBULENCE:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
END
END
END
END
BOUNDARY: R3 to S2 Side 1
BOUNDARY: R3 to S2 Side 1
Boundary Type = INTERFACE
Boundary Type = INTERFACE
Location = INFLOW 5
Location = INFLOW 5
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
TURBULENCE:
TURBULENCE:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
END
END
END
END
BOUNDARY: S3 to R3 Side 2
BOUNDARY: S3 to R3 Side 2
Boundary Type = INTERFACE
Boundary Type = INTERFACE
Location = OUTFLOW 5
Location = OUTFLOW 5
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
TURBULENCE:
TURBULENCE:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
END
END
END
END
DOMAIN MODELS:
DOMAIN MODELS:
BUOYANCY MODEL:
BUOYANCY MODEL:
Option = Non Buoyant
Option = Non Buoyant
END
END
DOMAIN MOTION:
DOMAIN MOTION:
Alternate Rotation Model = true
Alternate Rotation Model = true
Angular Velocity = 19451 [rev min^-1]
Angular Velocity = 19451 [rev min^-1]
Option = Rotating
Option = Rotating
AXIS DEFINITION:
AXIS DEFINITION:
Option = Coordinate Axis
Option = Coordinate Axis
Rotation Axis = Coord 0.3
Rotation Axis = Coord 0.3
END
END
END
END
MESH DEFORMATION:
MESH DEFORMATION:
Option = None
Option = None
END
END
REFERENCE PRESSURE:
REFERENCE PRESSURE:
Reference Pressure = 0 [atm]
Reference Pressure = 0 [atm]
END
END
END
END
FLUID DEFINITION: Fluid 1
FLUID DEFINITION: Air Ideal Gas
Material = Air at 25 C
Material = Air Ideal Gas
Option = Material Library
Option = Material Library
MORPHOLOGY:
MORPHOLOGY:
Option = Continuous Fluid
Option = Continuous Fluid
END
END
END
END
FLUID MODELS:
FLUID MODELS:
COMBUSTION MODEL:
COMBUSTION MODEL:
Option = None
Option = None
END
END
HEAT TRANSFER MODEL:
HEAT TRANSFER MODEL:
Include Viscous Work Term = True
Include Viscous Work Term = True
Option = Total Energy
Option = Total Energy
END
END
THERMAL RADIATION MODEL:
THERMAL RADIATION MODEL:
Option = None
Option = None
END
END
TURBULENCE MODEL:
TURBULENCE MODEL:
Option = SST
Option = SST
END
END
TURBULENT WALL FUNCTIONS:
TURBULENT WALL FUNCTIONS:
High Speed Model = Off
High Speed Model = Off
Option = Automatic
Option = Automatic
END
END
END
END
END
END
DOMAIN: S1
DOMAIN: S1
Coord Frame = Coord 0
Coord Frame = Coord 0
Domain Type = Fluid
Domain Type = Fluid
Location = Passage 2
Location = Passage 2
BOUNDARY: R2 to S1 Side 2
BOUNDARY: R2 to S1 Side 2
Boundary Type = INTERFACE
Boundary Type = INTERFACE
Location = OUTFLOW 2
Location = OUTFLOW 2
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
TURBULENCE:
TURBULENCE:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
END
END
END
END
BOUNDARY: S1 Blade
BOUNDARY: S1 Blade
Boundary Type = WALL
Boundary Type = WALL
Location = BLADE 2
Location = BLADE 2
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Adiabatic
Option = Adiabatic
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = No Slip Wall
Option = No Slip Wall
END
END
WALL ROUGHNESS:
WALL ROUGHNESS:
Option = Smooth Wall
Option = Smooth Wall
END
END
END
END
END
END
BOUNDARY: S1 Hub
BOUNDARY: S1 Hub
Boundary Type = WALL
Boundary Type = WALL
Location = HUB 2
Location = HUB 2
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Adiabatic
Option = Adiabatic
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = No Slip Wall
Option = No Slip Wall
END
END
WALL ROUGHNESS:
WALL ROUGHNESS:
Option = Smooth Wall
Option = Smooth Wall
END
END
END
END
END
END
BOUNDARY: S1 Shroud
BOUNDARY: S1 Shroud
Boundary Type = WALL
Boundary Type = WALL
Location = SHROUD 2
Location = SHROUD 2
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Adiabatic
Option = Adiabatic
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = No Slip Wall
Option = No Slip Wall
END
END
WALL ROUGHNESS:
WALL ROUGHNESS:
Option = Smooth Wall
Option = Smooth Wall
END
END
END
END
END
END
BOUNDARY: S1 to R1 Side 1
BOUNDARY: S1 to R1 Side 1
Boundary Type = INTERFACE
Boundary Type = INTERFACE
Location = INFLOW 2
Location = INFLOW 2
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
TURBULENCE:
TURBULENCE:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
END
END
END
END
BOUNDARY: S1 to S1 Periodic 1 Side 1
BOUNDARY: S1 to S1 Periodic 1 Side 1
Boundary Type = INTERFACE
Boundary Type = INTERFACE
Location = PER1 2
Location = PER1 2
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
TURBULENCE:
TURBULENCE:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
END
END
END
END
BOUNDARY: S1 to S1 Periodic 1 Side 2
BOUNDARY: S1 to S1 Periodic 1 Side 2
Boundary Type = INTERFACE
Boundary Type = INTERFACE
Location = PER2 2
Location = PER2 2
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
TURBULENCE:
TURBULENCE:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
END
END
END
END
DOMAIN MODELS:
DOMAIN MODELS:
BUOYANCY MODEL:
BUOYANCY MODEL:
Option = Non Buoyant
Option = Non Buoyant
END
END
DOMAIN MOTION:
DOMAIN MOTION:
Option = Stationary
Option = Stationary
END
END
MESH DEFORMATION:
MESH DEFORMATION:
Option = None
Option = None
END
END
REFERENCE PRESSURE:
REFERENCE PRESSURE:
Reference Pressure = 0 [atm]
Reference Pressure = 0 [atm]
END
END
END
END
FLUID DEFINITION: Fluid 1
FLUID DEFINITION: Air Ideal Gas
Material = Air at 25 C
Material = Air Ideal Gas
Option = Material Library
Option = Material Library
MORPHOLOGY:
MORPHOLOGY:
Option = Continuous Fluid
Option = Continuous Fluid
END
END
END
END
FLUID MODELS:
FLUID MODELS:
COMBUSTION MODEL:
COMBUSTION MODEL:
Option = None
Option = None
END
END
HEAT TRANSFER MODEL:
HEAT TRANSFER MODEL:
Include Viscous Work Term = True
Include Viscous Work Term = True
Option = Total Energy
Option = Total Energy
END
END
THERMAL RADIATION MODEL:
THERMAL RADIATION MODEL:
Option = None
Option = None
END
END
TURBULENCE MODEL:
TURBULENCE MODEL:
Option = SST
Option = SST
END
END
TURBULENT WALL FUNCTIONS:
TURBULENT WALL FUNCTIONS:
High Speed Model = Off
High Speed Model = Off
Option = Automatic
Option = Automatic
END
END
END
END
END
END
DOMAIN: S2
DOMAIN: S2
Coord Frame = Coord 0
Coord Frame = Coord 0
Domain Type = Fluid
Domain Type = Fluid
Location = Passage 4
Location = Passage 4
BOUNDARY: R3 to S2 Side 2
BOUNDARY: R3 to S2 Side 2
Boundary Type = INTERFACE
Boundary Type = INTERFACE
Location = OUTFLOW 4
Location = OUTFLOW 4
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
TURBULENCE:
TURBULENCE:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
END
END
END
END
BOUNDARY: S2 Blade
BOUNDARY: S2 Blade
Boundary Type = WALL
Boundary Type = WALL
Location = BLADE 4
Location = BLADE 4
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Adiabatic
Option = Adiabatic
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = No Slip Wall
Option = No Slip Wall
END
END
WALL ROUGHNESS:
WALL ROUGHNESS:
Option = Smooth Wall
Option = Smooth Wall
END
END
END
END
END
END
BOUNDARY: S2 Hub
BOUNDARY: S2 Hub
Boundary Type = WALL
Boundary Type = WALL
Location = HUB 4
Location = HUB 4
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Adiabatic
Option = Adiabatic
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = No Slip Wall
Option = No Slip Wall
END
END
WALL ROUGHNESS:
WALL ROUGHNESS:
Option = Smooth Wall
Option = Smooth Wall
END
END
END
END
END
END
BOUNDARY: S2 Shroud
BOUNDARY: S2 Shroud
Boundary Type = WALL
Boundary Type = WALL
Location = SHROUD 4
Location = SHROUD 4
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Adiabatic
Option = Adiabatic
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = No Slip Wall
Option = No Slip Wall
END
END
WALL ROUGHNESS:
WALL ROUGHNESS:
Option = Smooth Wall
Option = Smooth Wall
END
END
END
END
END
END
BOUNDARY: S2 to R2 Side 1
BOUNDARY: S2 to R2 Side 1
Boundary Type = INTERFACE
Boundary Type = INTERFACE
Location = INFLOW 4
Location = INFLOW 4
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
TURBULENCE:
TURBULENCE:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
END
END
END
END
BOUNDARY: S2 to S2 Periodic 1 Side 1
BOUNDARY: S2 to S2 Periodic 1 Side 1
Boundary Type = INTERFACE
Boundary Type = INTERFACE
Location = PER1 4
Location = PER1 4
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
TURBULENCE:
TURBULENCE:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
END
END
END
END
BOUNDARY: S2 to S2 Periodic 1 Side 2
BOUNDARY: S2 to S2 Periodic 1 Side 2
Boundary Type = INTERFACE
Boundary Type = INTERFACE
Location = PER2 4
Location = PER2 4
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
TURBULENCE:
TURBULENCE:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
END
END
END
END
DOMAIN MODELS:
DOMAIN MODELS:
BUOYANCY MODEL:
BUOYANCY MODEL:
Option = Non Buoyant
Option = Non Buoyant
END
END
DOMAIN MOTION:
DOMAIN MOTION:
Option = Stationary
Option = Stationary
END
END
MESH DEFORMATION:
MESH DEFORMATION:
Option = None
Option = None
END
END
REFERENCE PRESSURE:
REFERENCE PRESSURE:
Reference Pressure = 0 [atm]
Reference Pressure = 0 [atm]
END
END
END
END
FLUID DEFINITION: Fluid 1
FLUID DEFINITION: Air Ideal Gas
Material = Air at 25 C
Material = Air Ideal Gas
Option = Material Library
Option = Material Library
MORPHOLOGY:
MORPHOLOGY:
Option = Continuous Fluid
Option = Continuous Fluid
END
END
END
END
FLUID MODELS:
FLUID MODELS:
COMBUSTION MODEL:
COMBUSTION MODEL:
Option = None
Option = None
END
END
HEAT TRANSFER MODEL:
HEAT TRANSFER MODEL:
Include Viscous Work Term = True
Include Viscous Work Term = True
Option = Total Energy
Option = Total Energy
END
END
THERMAL RADIATION MODEL:
THERMAL RADIATION MODEL:
Option = None
Option = None
END
END
TURBULENCE MODEL:
TURBULENCE MODEL:
Option = SST
Option = SST
END
END
TURBULENT WALL FUNCTIONS:
TURBULENT WALL FUNCTIONS:
High Speed Model = Off
High Speed Model = Off
Option = Automatic
Option = Automatic
END
END
END
END
END
END
DOMAIN: S3
DOMAIN: S3
Coord Frame = Coord 0
Coord Frame = Coord 0
Domain Type = Fluid
Domain Type = Fluid
Location = Passage 6
Location = Passage 6
BOUNDARY: S3 Blade
BOUNDARY: S3 Blade
Boundary Type = WALL
Boundary Type = WALL
Location = BLADE 6
Location = BLADE 6
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Adiabatic
Option = Adiabatic
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = No Slip Wall
Option = No Slip Wall
END
END
WALL ROUGHNESS:
WALL ROUGHNESS:
Option = Smooth Wall
Option = Smooth Wall
END
END
END
END
END
END
BOUNDARY: S3 Hub
BOUNDARY: S3 Hub
Boundary Type = WALL
Boundary Type = WALL
Location = HUB 6
Location = HUB 6
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Adiabatic
Option = Adiabatic
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = No Slip Wall
Option = No Slip Wall
END
END
WALL ROUGHNESS:
WALL ROUGHNESS:
Option = Smooth Wall
Option = Smooth Wall
END
END
END
END
END
END
BOUNDARY: S3 Outlet
BOUNDARY: S3 Outlet
Boundary Type = OUTLET
Boundary Type = OUTLET
Location = OUTFLOW 6
Location = OUTFLOW 6
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
FLOW REGIME:
FLOW REGIME:
Option = Subsonic
Option = Subsonic
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Mass Flow Rate = 13 [kg s^-1]
Mass Flow Rate = 13 [kg s^-1]
Mass Flow Rate Area = Total for All Sectors
Mass Flow Rate Area = Total for All Sectors
Option = Mass Flow Rate
Option = Mass Flow Rate
END
END
END
END
END
END
BOUNDARY: S3 Shroud
BOUNDARY: S3 Shroud
Boundary Type = WALL
Boundary Type = WALL
Location = SHROUD 6
Location = SHROUD 6
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Adiabatic
Option = Adiabatic
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = No Slip Wall
Option = No Slip Wall
END
END
WALL ROUGHNESS:
WALL ROUGHNESS:
Option = Smooth Wall
Option = Smooth Wall
END
END
END
END
END
END
BOUNDARY: S3 to R3 Side 1
BOUNDARY: S3 to R3 Side 1
Boundary Type = INTERFACE
Boundary Type = INTERFACE
Location = INFLOW 6
Location = INFLOW 6
BOUNDARY CONDITIONS:
BOUNDARY CONDITIONS:
HEAT TRANSFER:
HEAT TRANSFER:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
MASS AND MOMENTUM:
MASS AND MOMENTUM:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
TURBULENCE:
TURBULENCE:
Option = Conservative Interface Flux
Option = Conservative Interface Flux
END
END
END
END
END
END
BOUNDARY: S3 to S3 Periodic 1 Side 1
BOUNDARY: S3 to S3 Periodic 1 Side 1
B
Boundary Type = INTERFACE
Location = PER1 6
BOUNDARY CONDITIONS:
HEAT