Fluid flow cfx не запускается расчёт

Доброго времени суток! Уважаемые знатоки, подскажите пожалуйста, как мне запустить расчёт. Я подготовил расчёт в Fluid flow cfx, ошибок никаких не показало, после открытия Solution и запуска расчёта мне выдало вот такую штуку - 

The ANSYS CFX partitioner has terminated without writing a partitioning

information file.

далее было - 

Fluid Flow CFX_003 has terminated with errors.

Run concluded at: Чт 28. янв 16:18:09 2016

No results are available.

В итоге, в окне Workbench вышло - update failed for the solution component in Fluid flow (CFX). The solcer failed with a non_zero exit code of : 2

Вот лог расчёта:

 This run of the CFX-15.0.7 Solver started at 16:17:52 on 28 Jan 2016 by
 user ansys on USER (intel_xeon64.sse2_winnt) using the command:
 
  "C:\Program Files\ANSYS Inc\v150\CFX\bin\perllib\cfx5solve.pl" -batch
    -ccl runInput.ccl -fullname "Fluid Flow CFX_003"
 
 Point Releases and Patches installed:
 
  ANSYS, Inc. Products 15.0.7
  ANSYS Mechanical Products 15.0.7
  ANSYS Autodyn 15.0.7
  ANSYS LS-DYNA 15.0.7
  ANSYS CFX (includes ANSYS CFD-Post) 15.0.7
  ANSYS Fluent (includes ANSYS CFD-Post) 15.0.7
  ANSYS TurboGrid 15.0.7
  ANSYS Polyflow (includes ANSYS CFD-Post) 15.0.7
  ANSYS Aqwa 15.0.7
  ANSYS ICEM CFD 15.0.7
  ANSYS Icepak (includes ANSYS CFD-Post) 15.0.7
  Catia, Version 6 15.0.7
  ANSYS, Inc. License Manager 15.0.7
 
 Setting up CFX Solver run ...
 

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

 LIBRARY:
   MATERIAL: Aluminium
     Material Group = CHT Solids, Particle Solids
     Option = Pure Substance
     Thermodynamic State = Solid
     PROPERTIES:
       Option = General Material
       EQUATION OF STATE:
         Density = 2702 [kg m^-3]
         Molar Mass = 26.98 [kg kmol^-1]
         Option = Value
       END
       SPECIFIC HEAT CAPACITY:
         Option = Value
         Specific Heat Capacity = 9.03E+02 [J kg^-1 K^-1]
       END
       REFERENCE STATE:
         Option = Specified Point
         Reference Specific Enthalpy = 0 [J/kg]
         Reference Specific Entropy = 0 [J/kg/K]
         Reference Temperature = 25 [C]
       END
       THERMAL CONDUCTIVITY:
         Option = Value
         Thermal Conductivity = 237 [W m^-1 K^-1]
       END
     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: Default Domain
     Coord Frame = Coord 0
     Domain Type = Fluid
     Location = B18
     BOUNDARY: Default Domain Default
       Boundary Type = WALL
       Location = F21.18,F22.18
       BOUNDARY CONDITIONS:
         HEAT TRANSFER:
           Option = Adiabatic
         END
         MASS AND MOMENTUM:
           Option = No Slip Wall
         END
         WALL ROUGHNESS:
           Option = Smooth Wall
         END
       END
     END
     BOUNDARY: Default Fluid Solid Interface Side 1
       Boundary Type = INTERFACE
       Location = F19.18,F20.18
       BOUNDARY CONDITIONS:
         HEAT TRANSFER:
           Option = Conservative Interface Flux
         END
         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 = Thermal Energy
       END
       THERMAL RADIATION MODEL:
         Option = None
       END
       TURBULENCE MODEL:
         Option = SST
       END
       TURBULENT WALL FUNCTIONS:
         Option = Automatic
       END
     END
   END
   DOMAIN: gilza
     Coord Frame = Coord 0
     Domain Type = Solid
     Location = B295
     BOUNDARY: Default Fluid Solid Interface in gilza Side 2
       Boundary Type = INTERFACE
       Location = F298.295,F302.295,F303.295,F306.295
       BOUNDARY CONDITIONS:
         HEAT TRANSFER:
           Option = Conservative Interface Flux
         END
       END
     END
     BOUNDARY: Default Solid Solid Interface Side 1
       Boundary Type = INTERFACE
       Location = F304.295,F313.295,F314.295
       BOUNDARY CONDITIONS:
         HEAT TRANSFER:
           Option = Conservative Interface Flux
         END
       END
     END
     BOUNDARY: gilza Default
       Boundary Type = WALL
       Location = \
         F297.295,F299.295,F300.295,F301.295,F305.295,F307.295,F308.295,F309.2\
         95,F310.295,F311.295,F312.295
       BOUNDARY CONDITIONS:
         HEAT TRANSFER:
           Option = Adiabatic
         END
       END
     END
     BOUNDARY: gilza_korpus Side 1
       Boundary Type = INTERFACE
       Location = F296.295
       BOUNDARY CONDITIONS:
         HEAT TRANSFER:
           Option = Conservative Interface Flux
         END
       END
     END
     DOMAIN MODELS:
       DOMAIN MOTION:
         Option = Stationary
       END
       MESH DEFORMATION:
         Option = None
       END
     END
     INITIALISATION:
       Option = Automatic
       INITIAL CONDITIONS:
         TEMPERATURE:
           Option = Automatic
         END
       END
     END
     SOLID DEFINITION: Solid 1
       Material = Aluminium
       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: korpus
     Coord Frame = Coord 0
     Domain Type = Solid
     Location = B165
     BOUNDARY: Default Fluid Solid Interface Side 2
       Boundary Type = INTERFACE
       Location = F179.165,F180.165,F181.165,F182.165
       BOUNDARY CONDITIONS:
         HEAT TRANSFER:
           Option = Conservative Interface Flux
         END
       END
     END
     BOUNDARY: Default Solid Solid Interface Side 2
       Boundary Type = INTERFACE
       Location = F174.165,F175.165
       BOUNDARY CONDITIONS:
         HEAT TRANSFER:
           Option = Conservative Interface Flux
         END
       END
     END
     BOUNDARY: gilza_korpus Side 2
       Boundary Type = INTERFACE
       Location = F166.165
       BOUNDARY CONDITIONS:
         HEAT TRANSFER:
           Option = Conservative Interface Flux
         END
       END
     END
     BOUNDARY: korpus Default
       Boundary Type = WALL
       Location = \
         F167.165,F168.165,F169.165,F171.165,F172.165,F176.165,F177.165,F178.1\
         65,F183.165,F184.165,F185.165,F186.165,F187.165,F188.165,F189.165,F19\
         0.165,F191.165,F192.165,F193.165,F194.165,F195.165,F196.165,F197.165,\
         F198.165
       BOUNDARY CONDITIONS:
         HEAT TRANSFER:
           Option = Adiabatic
         END
       END
     END
     BOUNDARY: ten_korpus Side 2
       Boundary Type = INTERFACE
       Location = F170.165,F173.165
       BOUNDARY CONDITIONS:
         HEAT TRANSFER:
           Option = Conservative Interface Flux
         END
       END
     END
     DOMAIN MODELS:
       DOMAIN MOTION:
         Option = Stationary
       END
       MESH DEFORMATION:
         Option = None
       END
     END
     INITIALISATION:
       Option = Automatic
       INITIAL CONDITIONS:
         TEMPERATURE:
           Option = Automatic
         END
       END
     END
     SOLID DEFINITION: Solid 1
       Material = Aluminium
       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: potok
     Coord Frame = Coord 0
     Domain Type = Fluid
     Location = B45
     BOUNDARY: Default Fluid Solid Interface in potok Side 1
       Boundary Type = INTERFACE
       Location = F49.45,F50.45,F51.45
       BOUNDARY CONDITIONS:
         HEAT TRANSFER:
           Option = Conservative Interface Flux
         END
         MASS AND MOMENTUM:
           Option = No Slip Wall
         END
         WALL ROUGHNESS:
           Option = Smooth Wall
         END
       END
     END
     BOUNDARY: inlet
       Boundary Type = INLET
       Location = F46.45
       BOUNDARY CONDITIONS:
         FLOW REGIME:
           Option = Subsonic
         END
         HEAT TRANSFER:
           Option = Static Temperature
           Static Temperature = 10 [C]
         END
         MASS AND MOMENTUM:
           Normal Speed = 0.5 [m s^-1]
           Option = Normal Speed
         END
         TURBULENCE:
           Option = Medium Intensity and Eddy Viscosity Ratio
         END
       END
     END
     BOUNDARY: outlet
       Boundary Type = OUTLET
       Location = F47.45
       BOUNDARY CONDITIONS:
         FLOW REGIME:
           Option = Subsonic
         END
         MASS AND MOMENTUM:
           Option = Static Pressure
           Relative Pressure = 101325 [Pa]
         END
       END
     END
     BOUNDARY: ten_potok Side 1
       Boundary Type = INTERFACE
       Location = F48.45,F52.45,F53.45
       BOUNDARY CONDITIONS:
         HEAT TRANSFER:
           Option = Conservative Interface Flux
         END
         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 = Thermal Energy
       END
       THERMAL RADIATION MODEL:
         Option = None
       END
       TURBULENCE MODEL:
         Option = SST
       END
       TURBULENT WALL FUNCTIONS:
         Option = Automatic
       END
     END
     INITIALISATION:
       Option = Automatic
       INITIAL CONDITIONS:
         Velocity Type = Cartesian
         CARTESIAN VELOCITY COMPONENTS:
           Option = Automatic
         END
         STATIC PRESSURE:
           Option = Automatic
         END
         TEMPERATURE:
           Option = Automatic
         END
         TURBULENCE INITIAL CONDITIONS:
           Option = Medium Intensity and Eddy Viscosity Ratio
         END
       END
     END
   END
   DOMAIN: ten
     Coord Frame = Coord 0
     Domain Type = Solid
     Location = B78
     BOUNDARY: ten Default
       Boundary Type = WALL
       Location = F79.78,F80.78
       BOUNDARY CONDITIONS:
         HEAT TRANSFER:
           Option = Adiabatic
         END
       END
     END
     BOUNDARY: ten_korpus Side 1
       Boundary Type = INTERFACE
       Location = F82.78,F84.78
       BOUNDARY CONDITIONS:
         HEAT TRANSFER:
           Option = Conservative Interface Flux
         END
       END
     END
     BOUNDARY: ten_potok Side 2
       Boundary Type = INTERFACE
       Location = F81.78,F83.78
       BOUNDARY CONDITIONS:
         HEAT TRANSFER:
           Option = Conservative Interface Flux
         END
       END
     END
     DOMAIN MODELS:
       DOMAIN MOTION:
         Option = Stationary
       END
       MESH DEFORMATION:
         Option = None
       END
     END
     INITIALISATION:
       Option = Automatic
       INITIAL CONDITIONS:
         TEMPERATURE:
           Option = Automatic
         END
       END
     END
     SOLID DEFINITION: Solid 1
       Material = Aluminium
       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 INTERFACE: Default Fluid Solid Interface
     Boundary List1 = Default Fluid Solid Interface Side 1,Default Fluid \
       Solid Interface in potok Side 1
     Boundary List2 = Default Fluid Solid Interface Side 2,Default Fluid \
       Solid Interface in gilza Side 2
     Interface Type = Fluid Solid
     INTERFACE MODELS:
       Option = General Connection
       FRAME CHANGE:
         Option = None
       END
       PITCH CHANGE:
         Option = None
       END
     END
     MESH CONNECTION:
       Option = GGI
     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 = GGI
     END
   END
   DOMAIN INTERFACE: gilza_korpus
     Boundary List1 = gilza_korpus Side 1
     Boundary List2 = gilza_korpus Side 2
     Interface Type = Solid Solid
     INTERFACE MODELS:
       Option = General Connection
       FRAME CHANGE:
         Option = None
       END
       HEAT TRANSFER:
         Option = Conservative Interface Flux
         HEAT TRANSFER INTERFACE MODEL:
           Option = None
         END
       END
       PITCH CHANGE:
         Option = None
       END
     END
     MESH CONNECTION:
       Option = Automatic
     END
   END
   DOMAIN INTERFACE: ten_korpus
     Boundary List1 = ten_korpus Side 1
     Boundary List2 = ten_korpus 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
   DOMAIN INTERFACE: ten_potok
     Boundary List1 = ten_potok Side 1
     Boundary List2 = ten_potok Side 2
     Interface Type = Fluid 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
   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
       Solid Timescale Control = Auto Timescale
       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
   END
 END
 COMMAND FILE:
   Version = 15.0
   Results Version = 15.0.7
 END
 SIMULATION CONTROL:
   EXECUTION CONTROL:
     EXECUTABLE SELECTION:
       Double Precision = Off
     END
     INTERPOLATOR STEP CONTROL:
       Runtime Priority = Standard
       DOMAIN SEARCH CONTROL:
         Bounding Box Tolerance = 0.01
       END
       INTERPOLATION MODEL CONTROL:
         Enforce Strict Name Mapping for Phases = Off
         Mesh Deformation Option = Automatic
         Particle Relocalisation Tolerance = 0.01
       END
       MEMORY CONTROL:
         Memory Allocation Factor = 1.0
       END
     END
     PARALLEL HOST LIBRARY:
       HOST DEFINITION: user
         Host Architecture String = winnt-amd64
         Installation Root = C:\Program Files\ANSYS Inc\v%v\CFX
       END
     END
     PARTITIONER STEP CONTROL:
       Multidomain Option = Independent Partitioning
       Runtime Priority = Standard
       EXECUTABLE SELECTION:
         Use Large Problem Partitioner = Off
       END
       MEMORY CONTROL:
         Memory Allocation Factor = 1.0
       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 = Fluid Flow CFX.def
     END
     SOLVER STEP CONTROL:
       Runtime Priority = Standard
       MEMORY CONTROL:
         Memory Allocation Factor = 1.0
       END
       PARALLEL ENVIRONMENT:
         Number of Processes = 4
         Start Method = Platform MPI Local Parallel
         Parallel Host List = user*4
       END
     END
   END
 END
 

 +--------------------------------------------------------------------+
 |                                                                    |
 |                            Partitioning                            |
 |                                                                    |
 +--------------------------------------------------------------------+

 +--------------------------------------------------------------------+
 |                                                                    |
 |                 ANSYS(R) CFX(R) Partitioner 15.0.7                 |
 |                                                                    |
 | Version 2014.04.10-23.00-131675     Thu Apr 10 23:23:37 GMTDT 2014 |
 |                                                                    |
 |                        Executable Attributes                       |
 |                                                                    |
 |          single-64bit-int32-supfort-optimised-noprof-lcomp         |
 |                                                                    |
 | (C) 2014 ANSYS, Inc.                                               |
 |                                                                    |
 | All rights reserved. Unauthorized use, distribution or duplication |
 | is prohibited. This product is subject to U.S. laws governing      |
 | export and re-export. For full Legal Notice, see documentation.    |
 +--------------------------------------------------------------------+

 +--------------------------------------------------------------------+
 |                  Job Information at Start of Run                   |
 +--------------------------------------------------------------------+

 Run mode:       partitioning run

 +------------------------------+------+--------+----------+----------+
 | Host                         | Mesh |  PID   |     Job Started     |
 |                              | Part |        | DD/MM/YY | hh:mm:ss |
 +------------------------------+------+--------+----------+----------+
 | USER                         |    1 |   4948 | 28/01/16 | 16:17:54 |
 +------------------------------+------+--------+----------+----------+

 +--------------------------------------------------------------------+
 |        Memory Allocated for Run  (Actual usage may be less)        |
 +--------------------------------------------------------------------+

           | Real       | Integer    | Character | Logical  | Double
 ----------+------------+------------+-----------+----------+----------
 Mwords    |       5.03 |       7.57 |      3.42 |     0.12 |     1.20
 Mbytes    |      19.20 |      28.88 |      3.26 |     0.46 |     9.16
 ----------+------------+------------+-----------+----------+----------

 +--------------------------------------------------------------------+
 |                  Host Memory Information (Mbytes)                  |
 +--------------------------------------------------------------------+
 |          Host           |     System     |   Allocated    |   %    |
 +-------------------------+----------------+----------------+--------+
 | USER                    |      4059.79   |        60.96   |   1.50 |
 +-------------------------+----------------+----------------+--------+

 +--------------------------------------------------------------------+
 |                   ********* WARNING *********                      |
 | No control surfaces have been found for the domain interface       |
 |                                                                    |
 |       gilza_korpus                                                 |
 |                                                                    |
 | If you expect this to occur, please set the INTERSECTION CONTROL   |
 | CCL parameter 'Permit No Intersection' to work around this message.|
 | Non-intersecting interfaces are only supported for 'dynamic'       |
 | interfaces which are re-intersected at every time step             |
 | (e.g. transient rotor stator interfaces or non-stationary          |
 | interfaces in moving mesh cases).                                  |
 |                                                                    |
 | Possible setup errors leading to this situation are:               |
 | 1. An incorrect axis of rotation for a rotating domain or domain   |
 |    interface.                                                      |
 | 2. A frame change model is used in which there is unequal pitch    |
 |    shapes, or circumferential orientation, but the Pitch Change    |
 |    model is set to None.                                           |
 | 3. The transient rotor stator model is used when the geometry      |
 |    does not span 360 degrees and the Pitch Change model is set to  |
 |    'None'.                                                         |
 | 4. The detected normal gap between interface sides is larger than  |
 |    the allowed tolerance. See the documentation for controlling    |
 |    this tolerance.                                                 |
 +--------------------------------------------------------------------+

 +--------------------------------------------------------------------+
 |                An error has occurred in cfx5solve:                 |
 |                                                                    |
 | The ANSYS CFX partitioner has terminated without writing a         |
 | partitioning information file.                                     |
 +--------------------------------------------------------------------+

This run of the ANSYS CFX Solver has finished.

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