LIBRARY:
   CEL:
     EXPRESSIONS:
       massFlowRate = volumeFlowRate * waterDensity
       myRPM = 1500 [rev min^-1]
       pumpHead = (massFlowAve(Absolute Pressure)@Outlet-massFlowAve(Absolute \
         Pressure)@Inlet)/(areaAve(Density)@Outlet*g)
       volumeFlowRate = (550 / 3600) [m^3 s^-1]
       waterDensity = 1000 [kg m^-3]
       yPlus = areaAve(yplus)@Blade
     END
   END
   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: S1
     Coord Frame = Coord 0
     Domain Type = Fluid
     Location = B18,B18 2,B81,B666
     BOUNDARY: Blade
       Boundary Type = WALL
       Location = Blade
       BOUNDARY CONDITIONS:
         MASS AND MOMENTUM:
           Option = No Slip Wall
         END
         WALL ROUGHNESS:
           Option = Smooth Wall
         END
       END
     END
     BOUNDARY: Hub
       Boundary Type = WALL
       Location = Hub
       BOUNDARY CONDITIONS:
         MASS AND MOMENTUM:
           Option = No Slip Wall
         END
         WALL ROUGHNESS:
           Option = Smooth Wall
         END
       END
     END
     BOUNDARY: Interface GehauseExtension Side 1
       Boundary Type = INTERFACE
       Location = IF GE
       BOUNDARY CONDITIONS:
         MASS AND MOMENTUM:
           Option = Conservative Interface Flux
         END
         TURBULENCE:
           Option = Conservative Interface Flux
         END
       END
     END
     BOUNDARY: Interface GehauseExtension Side 2
       Boundary Type = INTERFACE
       Location = IF EG
       BOUNDARY CONDITIONS:
         MASS AND MOMENTUM:
           Option = Conservative Interface Flux
         END
         TURBULENCE:
           Option = Conservative Interface Flux
         END
       END
     END
     BOUNDARY: Interface LaufradGehause Side 1
       Boundary Type = INTERFACE
       Location = IF LG
       BOUNDARY CONDITIONS:
         MASS AND MOMENTUM:
           Option = Conservative Interface Flux
         END
         TURBULENCE:
           Option = Conservative Interface Flux
         END
       END
     END
     BOUNDARY: Interface LaufradGehause Side 2
       Boundary Type = INTERFACE
       Location = IF GL
       BOUNDARY CONDITIONS:
         MASS AND MOMENTUM:
           Option = Conservative Interface Flux
         END
         TURBULENCE:
           Option = Conservative Interface Flux
         END
       END
     END
     BOUNDARY: Interface ZulaufLaufrad Side 1
       Boundary Type = INTERFACE
       Location = IF ZL
       BOUNDARY CONDITIONS:
         MASS AND MOMENTUM:
           Option = Conservative Interface Flux
         END
         TURBULENCE:
           Option = Conservative Interface Flux
         END
       END
     END
     BOUNDARY: Interface ZulaufLaufrad Side 2
       Boundary Type = INTERFACE
       Location = IF LZ
       BOUNDARY CONDITIONS:
         MASS AND MOMENTUM:
           Option = Conservative Interface Flux
         END
         TURBULENCE:
           Option = Conservative Interface Flux
         END
       END
     END
     BOUNDARY: S1 Inlet
       Boundary Type = INLET
       Location = Inlet
       BOUNDARY CONDITIONS:
         FLOW DIRECTION:
           Option = Normal to Boundary Condition
         END
         FLOW REGIME:
           Option = Subsonic
         END
         MASS AND MOMENTUM:
           Mass Flow Rate = massFlowRate
           Mass Flow Rate Area = As Specified
           Option = Mass Flow Rate
         END
         TURBULENCE:
           Option = Medium Intensity and Eddy Viscosity Ratio
         END
       END
     END
     BOUNDARY: S1 Outlet
       Boundary Type = OUTLET
       Location = Outlet
       BOUNDARY CONDITIONS:
         FLOW REGIME:
           Option = Subsonic
         END
         MASS AND MOMENTUM:
           Option = Static Pressure
           Relative Pressure = 1 [atm]
         END
       END
     END
     BOUNDARY: S1 Wall
       Boundary Type = WALL
       Location = Wall
       BOUNDARY CONDITIONS:
         MASS AND MOMENTUM:
           Option = No Slip Wall
         END
         WALL ROUGHNESS:
           Option = Smooth Wall
         END
       END
     END
     BOUNDARY: S1 WallFree
       Boundary Type = WALL
       Location = WallFree,WallFree 2,WallFree 3
       BOUNDARY CONDITIONS:
         MASS AND MOMENTUM:
           Option = Free Slip Wall
         END
       END
     END
     BOUNDARY: Shroud
       Boundary Type = WALL
       Location = Shroud
       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: Water
       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: IF GE
     Boundary List1 = Interface GehauseExtension Side 1
     Boundary List2 = Interface GehauseExtension Side 2
     Interface Type = Fluid Fluid
     INTERFACE MODELS:
       Option = General Connection
       FRAME CHANGE:
         Option = None
       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: IF LG
     Boundary List1 = Interface LaufradGehause Side 1
     Boundary List2 = Interface LaufradGehause Side 2
     Interface Type = Fluid Fluid
     INTERFACE MODELS:
       Option = General Connection
       FRAME CHANGE:
         Option = None
       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: IF ZL
     Boundary List1 = Interface ZulaufLaufrad Side 1
     Boundary List2 = Interface ZulaufLaufrad Side 2
     Interface Type = Fluid Fluid
     INTERFACE MODELS:
       Option = General Connection
       FRAME CHANGE:
         Option = None
       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
   OUTPUT CONTROL:
     MONITOR OBJECTS:
       MONITOR BALANCES:
         Option = Full
       END
       MONITOR FORCES:
         Option = Full
       END
       MONITOR PARTICLES:
         Option = Full
       END
       MONITOR POINT: pumpHeadMon
         Coord Frame = Coord 0
         Expression Value = pumpHead
         Option = Expression
       END
       MONITOR POINT: yPlusMon
         Coord Frame = Coord 0
         Expression Value = areaAve(yplus)@REGION:Blade
         Option = Expression
       END
       MONITOR RESIDUALS:
         Option = Full
       END
       MONITOR TOTALS:
         Option = Full
       END
     END
     RESULTS:
       File Compression Level = Default
       Option = Standard
     END
   END
   SOLVER CONTROL:
     Turbulence Numerics = High Resolution
     ADVECTION SCHEME:
       Option = High Resolution
     END
     CONVERGENCE CONTROL:
       Local Timescale Factor = 5
       Maximum Number of Iterations = 100
       Minimum Number of Iterations = 100
       Timescale Control = Local Timescale Factor
     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 = 25.1
   Results Version = 25.1
 END
 SIMULATION CONTROL:
   EXECUTION CONTROL:
     EXECUTABLE SELECTION:
       Double Precision = No
       Large Problem = No
     END
     INTERPOLATOR STEP CONTROL:
       Runtime Priority = High
       MEMORY CONTROL:
         Memory Allocation Factor = 1
         Option = Model Based
       END
     END
     PARALLEL HOST LIBRARY:
       HOST DEFINITION: neropc
         Installation Root = C:\Program Files\ANSYS Inc\ANSYS Student\v%v\CFX
         Host Architecture String = winnt-amd64
       END
     END
     PARTITIONER STEP CONTROL:
       Multidomain Option = Automatic
       Option = Spatial Partitioning
       Runtime Priority = High
       MEMORY CONTROL:
         Memory Allocation Factor = 10
         Option = Model Based
       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
       SPATIAL PARTITIONING:
         Option = Automatic
       END
     END
     RUN DEFINITION:
       Run Mode = Full
       Solver Input File = CFX.def
       Solver Results File = C:/Users/Nero/Desktop/ANSYS \
         CFX/VK14/VK14_new_pending/dp1_CFX_Solution/CFX_004.res
     END
     SOLVER STEP CONTROL:
       Runtime Priority = High
       MEMORY CONTROL:
         Memory Allocation Factor = 1
         Option = Model Based
       END
       PARALLEL ENVIRONMENT:
         Maximum Number of Processes = 4
         Start Method = Intel MPI Local Parallel
         Parallel Host List = neropc*4
       END
     END
   END
 END
 
 überprüfe die bedingungen, es ist eine ansys cfx simulation