ошибка при начале расчета в CFX

Здравствуйте! вылетает ошибка при запуске расчета в CFX, делаю дипломную работу по моделированию лазерного излучения, надеюсь на вашу помощь! Заранее спасибо! 

Нашел похожую тему на данном форуме, там у автора была проблема с тем что стояла запятая вместо точки, проверил все значения - у меня везде точки.

вот лог файл:

 This run of the CFX Release 18.2 Solver started at 12:50:25 on 09 Apr
 2018 by user Vlad Lebed on DESKTOP-KNV36K5 (intel_xeon64.sse2_winnt)
 using the command:
 
  "C:\Program Files\ANSYS Inc\v182\CFX\bin\perllib\cfx5solve.pl" -batch
    -ccl runInput.ccl -fullname 2703_002
 
 Release 18.2
 
  Point Releases and Patches installed:
  ANSYS, Inc. Products Release 18.2
  ANSYS Mechanical Products Release 18.2
  ANSYS Autodyn Release 18.2
  ANSYS LS-DYNA Release 18.2
  ANSYS AIM Release 18.2
  ANSYS CFX (includes ANSYS CFD-Post) Release 18.2
  ANSYS Fluent (includes ANSYS CFD-Post) Release 18.2
  ANSYS TurboGrid Release 18.2
  ANSYS FENSAP-ICE Release 18.2
  ANSYS Polyflow (includes ANSYS CFD-Post) Release 18.2
  ANSYS Forte Release 18.2
  ANSYS Chemkin Release 18.2
  ANSYS ICEM CFD Release 18.2
  ANSYS Aqwa Release 18.2
  ANSYS Icepak (includes ANSYS CFD-Post) Release 18.2
  AutoCAD Release 18.2
  ACIS Release 18.2
  Catia, Version 4 Release 18.2
  Catia, Version 6 Release 18.2
  Creo Elements/Direct Modeling Release 18.2
  Inventor Release 18.2
  JTOpen Release 18.2
  NX Release 18.2
  Parasolid Release 18.2
  Creo Parametric Release 18.2
  Solid Edge Release 18.2
  SolidWorks Release 18.2
  ANSYS, Inc. License Manager Release 18.2
 
 Setting up CFX Solver run ...
 

 +--------------------------------------------------------------------+
 |                                                                    |
 |                    CFX Command Language for Run                    |
 |                                                                    |
 +--------------------------------------------------------------------+

 LIBRARY:
   CEL:
     EXPRESSIONS:
       AL2A = al2o3a(T)
       AL2C = al2o3c(T)
       Al2 = al2o3des(T)
       I = I0*(1-Rotr)*e^((kx/1[m-1])*(-y/1[m]))
       I0 = heat
       Rotr = 0.1
       X14c = X14C(T)
       X17 = X14X17H2a(T)
       area = (rad/1[m])^2-(x/1[m])^2-(z/1[m])^2
       b = 100[nm]
       gaus = exp(-(((z/0.01[m])^2)+(x/0.01[m])^2)*sigma)
       heat = power/(pi*rad^2)
       imp = step(step(t0/1[s]-t/1[s])-0.25)
       kx = l2-(l2-l1)*step(step(b/1[m]-y/1[m])-0.25)
       l1 = 0.8 [m-1]
       l2 = 0.03 [m-1]
       power = 200 [W]
       rad = 1[mm]
       sigma = 200
       sourse = gaus*step(area)*I*imp
       t0 = 250E-6[s]
       x0 = 0[m]
       z0 = 0[mm]
     END
     FUNCTION: X14C
       Argument Units = [C]
       Option = Interpolation
       Result Units = [J kg^-1 C^-1]
       INTERPOLATION DATA:
         Data Pairs = 20,462
         Extend Max = On
         Extend Min = On
         Option = One Dimensional
       END
     END
     FUNCTION: X14X17H2a
       Argument Units = [C]
       Option = Interpolation
       Result Units = [C^-1]
       INTERPOLATION DATA:
         Data Pairs = \
           20,9E-06,100,9.8E-06,200,1.06E-05,300,1.08E-05,400,1.1E-05,500,1.11\
           E-05,600,1.18E-05,700,1.1E-05,800,1.07E-05,900,1.14E-05,1000,1.15E-\
           05
         Extend Max = On
         Extend Min = On
         Option = One Dimensional
       END
     END
     FUNCTION: al2o3a
       Argument Units = [K]
       Option = Interpolation
       Result Units = [K^-1]
       INTERPOLATION DATA:
         Data Pairs = \
           100,9.09E-06,300,7.82E-06,350,7.9E-06,400,8E-06,500,8.18E-06,600,8.\
           36E-06,700,8.55E-06,800,8.73E-06,1000,9.09E-06,1200,9.44E-06,1400,9\
           .8E-06,1600,10.15E-06,1800,10.5E-06,2000,10.85E-06,2200,11.2E-06
         Extend Max = On
         Extend Min = On
         Option = One Dimensional
       END
     END
     FUNCTION: al2o3c
       Argument Units = [K]
       Option = Interpolation
       Result Units = [J kg^-1 K^-1]
       INTERPOLATION DATA:
         Data Pairs = \
           300,775,350,886,400,959,500,1050,600,1105,700,1143,800,1173,1000,12\
           23,1200,1268,1400,1310,1600,1349,1800,1388,2000,1425,2200,1463
         Extend Max = On
         Extend Min = On
         Option = One Dimensional
       END
     END
     FUNCTION: al2o3des
       Argument Units = [K]
       Option = Interpolation
       Result Units = [kg m^-3]
       INTERPOLATION DATA:
         Data Pairs = \
           300,3970,350,3965,400,3961,500,3951,600,3941,700,3931,800,3921,1000\
           ,3900,1200,3879,1400,3856,1600,1833,1800,3810,2000,3785,2200,3760
         Extend Max = On
         Extend Min = On
         Option = One Dimensional
       END
     END
   END
   MATERIAL: al2o3
     Material Group = CHT Solids
     Option = Pure Substance
     Thermodynamic State = Solid
     PROPERTIES:
       Option = General Material
       EQUATION OF STATE:
         Density = Al2
         Molar Mass = 101.96 [g mol^-1]
         Option = Value
       END
       SPECIFIC HEAT CAPACITY:
         Option = Value
         Specific Heat Capacity = AL2C
       END
       THERMAL CONDUCTIVITY:
         Option = Value
         Thermal Conductivity = 40 [W m^-1 K^-1]
       END
       THERMAL EXPANSIVITY:
         Option = Value
         Thermal Expansivity = AL2A
       END
     END
   END
   MATERIAL: x14X17H2
     Material Group = CHT Solids
     Option = Pure Substance
     Thermodynamic State = Solid
     PROPERTIES:
       Option = General Material
       EQUATION OF STATE:
         Density = 7750 [kg m^-3]
         Molar Mass = 1.0 [kg kmol^-1]
         Option = Value
       END
       SPECIFIC HEAT CAPACITY:
         Option = Value
         Specific Heat Capacity = X14c
       END
       THERMAL CONDUCTIVITY:
         Option = Value
         Thermal Conductivity = 20.9 [W m^-1 K^-1]
       END
       THERMAL EXPANSIVITY:
         Option = Value
         Thermal Expansivity = X17
       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 = Transient
     EXTERNAL SOLVER COUPLING:
       Option = None
     END
     INITIAL TIME:
       Option = Automatic with Value
       Time = 0 [s]
     END
     TIME DURATION:
       Option = Total Time
       Total Time = 500E-06 [s]
     END
     TIME STEPS:
       Option = Timesteps
       Timesteps = 5e-005 [s]
     END
   END
   DOMAIN: al
     Coord Frame = Coord 0
     Domain Type = Solid
     Location = B87
     BOUNDARY: Boundary 1
       Boundary Type = WALL
       Location = F89.87
       BOUNDARY CONDITIONS:
         HEAT TRANSFER:
           Option = Adiabatic
         END
       END
     END
     BOUNDARY: Default Solid Solid Interface Side 1
       Boundary Type = INTERFACE
       Location = F88.87
       BOUNDARY CONDITIONS:
         HEAT TRANSFER:
           Option = Conservative Interface Flux
         END
       END
     END
     BOUNDARY: al Default
       Boundary Type = WALL
       Location = F83.87,F84.87,F85.87,F86.87
       BOUNDARY CONDITIONS:
         HEAT TRANSFER:
           Option = Adiabatic
         END
       END
     END
     DOMAIN MODELS:
       DOMAIN MOTION:
         Option = Stationary
       END
       MESH DEFORMATION:
         Option = None
       END
     END
     INITIALISATION:
       Option = Automatic
       INITIAL CONDITIONS:
         TEMPERATURE:
           Option = Automatic with Value
           Temperature = 20 [C]
         END
       END
     END
     SOLID DEFINITION: Solid 1
       Material = x14X17H2
       Option = Material Library
       MORPHOLOGY:
         Option = Continuous Solid
       END
     END
     SOLID MODELS:
       HEAT TRANSFER MODEL:
         Option = Thermal Energy
       END
       THERMAL RADIATION MODEL:
         Option = None
       END
     END
   END
   DOMAIN: al2o3
     Coord Frame = Coord 0
     Domain Type = Solid
     Location = B30
     BOUNDARY: Boundary 2
       Boundary Type = WALL
       Location = F32.30
       BOUNDARY CONDITIONS:
         HEAT TRANSFER:
           Option = Adiabatic
         END
       END
       BOUNDARY SOURCE:
         SOURCES:
           EQUATION SOURCE: energy
             Flux = sourse
             Option = Flux
           END
         END
       END
     END
     BOUNDARY: Default Solid Solid Interface Side 2
       Boundary Type = INTERFACE
       Location = F70.30
       BOUNDARY CONDITIONS:
         HEAT TRANSFER:
           Option = Conservative Interface Flux
         END
       END
     END
     BOUNDARY: al2o3 Default
       Boundary Type = WALL
       Location = F33.30,F34.30,F35.30,F36.30
       BOUNDARY CONDITIONS:
         HEAT TRANSFER:
           Option = Adiabatic
         END
       END
     END
     DOMAIN MODELS:
       DOMAIN MOTION:
         Option = Stationary
       END
       MESH DEFORMATION:
         Option = None
       END
     END
     INITIALISATION:
       Option = Automatic
       INITIAL CONDITIONS:
         TEMPERATURE:
           Option = Automatic with Value
           Temperature = 20 [C]
         END
       END
     END
     SOLID DEFINITION: Solid 1
       Material = al2o3
       Option = Material Library
       MORPHOLOGY:
         Option = Continuous Solid
       END
     END
     SOLID MODELS:
       HEAT TRANSFER MODEL:
         Option = Thermal Energy
       END
       THERMAL RADIATION MODEL:
         Option = None
       END
     END
     SOURCE POINT: Source Point 1
       Cartesian Coordinates = 0 [m], 0 [m], 0 [m]
       Option = Cartesian Coordinates
     END
   END
   DOMAIN INTERFACE: Default Solid Solid Interface
     Boundary List1 = Default Solid Solid Interface Side 1
     Boundary List2 = Default Solid Solid Interface Side 2
     Interface Type = Solid Solid
     INTERFACE MODELS:
       Option = General Connection
       FRAME CHANGE:
         Option = None
       END
       PITCH CHANGE:
         Option = None
       END
     END
     MESH CONNECTION:
       Option = Automatic
     END
   END
   OUTPUT CONTROL:
     RESULTS:
       File Compression Level = Default
       Option = Standard
     END
     TRANSIENT RESULTS: Transient Results 1
       File Compression Level = Default
       Option = Standard
       OUTPUT FREQUENCY:
         Option = Timestep Interval
         Timestep Interval = 2
       END
     END
   END
   SOLVER CONTROL:
     ADVECTION SCHEME:
       Option = High Resolution
     END
     CONVERGENCE CONTROL:
       Maximum Number of Coefficient Loops = 10
       Minimum Number of Coefficient Loops = 1
       Timescale Control = Coefficient Loops
     END
     CONVERGENCE CRITERIA:
       Residual Target = 1.E-4
       Residual Type = RMS
     END
     TRANSIENT SCHEME:
       Option = Second Order Backward Euler
       TIMESTEP INITIALISATION:
         Option = Automatic
       END
     END
   END
 END
 COMMAND FILE:
   Version = 18.2
   Results Version = 18.2
 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: desktopknv36k5
         Remote Host Name = DESKTOP-KNV36K5
         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 = 2703.def
       Solver Results File = \
         D:/ansys/2703_pending/dp0_CFX_2_Solution_3/2703_002.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
 
Need at least 2 data pairs for interpolation
 +--------------------------------------------------------------------+
 |                An error has occurred in cfx5solve:                 |
 |                                                                    |
 | C:\Program Files\ANSYS Inc\v182\CFX\bin\winnt-amd64\ccl2flow.exe   |
 | was interrupted by signal QUIT (3)                                 |
 +--------------------------------------------------------------------+

 +--------------------------------------------------------------------+
 | 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.
 

и скриншот ошибки