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

 LIBRARY:
   CEL:
     EXPRESSIONS:
       at = atstep
       ps = 1[bar]
       pr = ps-atstep^(10)*1[bar]
     END
   END
   ADDITIONAL VARIABLE: zeit
     Option = Definition
     Tensor Type = SCALAR
     Units = [ s]
     Variable Type = Unspecified
   END
   MATERIAL: Air at 25 C
     Material Description = Air at 25 C and 1 atm (dry)
     Material Group = Air Data, Constant Property Gases
     Option = Pure Substance
     Thermodynamic State = Gas
     PROPERTIES:
       Option = General Material
       Thermal Expansivity = 0.003356 [K^-1]
       ABSORPTION COEFFICIENT:
         Absorption Coefficient = 0.01 [m^-1]
         Option = Value
       END
       DYNAMIC VISCOSITY:
         Dynamic Viscosity = 1.831E-05 [kg m^-1 s^-1]
         Option = Value
       END
       EQUATION OF STATE:
         Density = 1.185 [kg m^-3]
         Molar Mass = 28.96 [kg kmol^-1]
         Option = Value
       END
       REFERENCE STATE:
         Option = Specified Point
         Reference Pressure = 1 [atm]
         Reference Specific Enthalpy = 0. [J/kg]
         Reference Specific Entropy = 0. [J/kg/K]
         Reference Temperature = 25 [C]
       END
       REFRACTIVE INDEX:
         Option = Value
         Refractive Index = 1.0 [m m^-1]
       END
       SCATTERING COEFFICIENT:
         Option = Value
         Scattering Coefficient = 0.0 [m^-1]
       END
       SPECIFIC HEAT CAPACITY:
         Option = Value
         Specific Heat Capacity = 1.0044E+03 [J kg^-1 K^-1]
         Specific Heat Type = Constant Pressure
       END
       THERMAL CONDUCTIVITY:
         Option = Value
         Thermal Conductivity = 2.61E-02 [W m^-1 K^-1]
       END
     END
   END
 END
 FLOW:
   SOLUTION UNITS:
     Angle Units = [rad]
     Length Units = [m]
     Mass Units = [kg]
     Solid Angle Units = [sr]
     Temperature Units = [K]
     Time Units = [s]
   END
   SIMULATION 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 = 0.9 [s]
     END
     TIME STEPS:
       Option = Timesteps
       Timesteps = 0.05 [s]
     END
   END
   DOMAIN: Default Domain
     Coord Frame = Coord 0
     Domain Type = Fluid
     Fluids List = Air at 25 C
     Location = B215
     BOUNDARY: Auslass1
       Boundary Type = OUTLET
       Location = outlet_1
       BOUNDARY CONDITIONS:
         FLOW REGIME:
           Option = Subsonic
         END
         MASS AND MOMENTUM:
           Option = Static Pressure
           Relative Pressure = pr
         END
       END
     END
     BOUNDARY: Einlass
       Boundary Type = OPENING
       Location = inlet
       BOUNDARY CONDITIONS:
         FLOW REGIME:
           Option = Subsonic
         END
         MASS AND MOMENTUM:
           Option = Static Pressure for Entrainment
           Relative Pressure = 0 [bar]
         END
         TURBULENCE:
           Option = Zero Gradient
         END
       END
     END
     BOUNDARY: Wall
       Boundary Type = WALL
       Location = \
         outlet_2,outlet_3,outlet_4,F188.215,F189.215,F190.215,F191.215,F192.2\
         15,F193.215,F194.215,F195.215,F196.215,F197.215,F202.215,F203.215,F20\
         4.215,F205.215,F206.215,F207.215,F208.215,F209.215,F210.215,F211.215,\
         F212.215,F213.215,F214.215,F216.215,F217.215,F218.215,F219.215,F220.2\
         15,F221.215,F222.215,F223.215,F224.215,F225.215,F226.215,F227.215,F22\
         8.215,F229.215,F230.215,F231.215,F232.215,F233.215,F234.215,F235.215,\
         F236.215,F237.215,F238.215,F239.215,F240.215,F241.215,F242.215,F243.2\
         15,F244.215,F245.215,F246.215,F247.215,F248.215,F249.215,F250.215,F25\
         1.215,F252.215,F253.215,F254.215,F255.215,F256.215,F257.215,F259.215,\
         F260.215,F261.215,F262.215
       BOUNDARY CONDITIONS:
         WALL INFLUENCE ON FLOW:
           Option = No Slip
         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 [bar]
       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
     INITIALISATION:
       Option = Automatic
       INITIAL CONDITIONS:
         Velocity Type = Cartesian
         CARTESIAN VELOCITY COMPONENTS:
           Option = Automatic with Value
           U = -10 [m s^-1]
           V = 0 [m s^-1]
           W = 0 [m s^-1]
         END
         EPSILON:
           Option = Automatic
         END
         K:
           Option = Automatic with Value
         END
         STATIC PRESSURE:
           Option = Automatic with Value
           Relative Pressure = 0 [bar]
         END
       END
     END
   END
   OUTPUT CONTROL:
     RESULTS:
       File Compression Level = Default
       Option = Standard
     END
     TRANSIENT RESULTS: results
       File Compression Level = Default
       Option = Standard
       OUTPUT FREQUENCY:
         Option = Every Timestep
       END
     END
   END
   SOLVER CONTROL:
     ADVECTION SCHEME:
       Option = High Resolution
     END
     CONVERGENCE CONTROL:
       Maximum Number of Coefficient Loops = 10
       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 = 11.0
   Results Version = 11.0
 END
 PARAMETERIZATION:
   INPUT FIELD: Expressions
     Expression Name = Expressions
     Method = Expression
   END
 END
 EXECUTION CONTROL:
   INTERPOLATOR STEP CONTROL:
     Runtime Priority = Standard
     EXECUTABLE SELECTION:
       Double Precision = Off
     END
     MEMORY CONTROL:
       Memory Allocation Factor = 1.0
     END
   END
   PARALLEL HOST LIBRARY:
     HOST DEFINITION: rzc3021
       Host Architecture String = intel_xeon64.sse2_winnt5.1
       Installation Root = C:\Programme\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
     END
   END
   RUN DEFINITION:
     Definition File = \
       W:/CAD_DATEN_WR03/Motor/Ansaugsystem/Ansaug_wr03_venturi/RPM_ansaug_wr0\
       3/saugen.def
     Interpolate Initial Values = Off
     Run Mode = Full
   END
   SOLVER STEP CONTROL:
     Runtime Priority = Standard
     EXECUTABLE SELECTION:
       Double Precision = Off
     END
     MEMORY CONTROL:
       Memory Allocation Factor = 1.0
     END
     PARALLEL ENVIRONMENT:
       Number of Processes = 1
       Start Method = Serial
     END
   END
 END
 
 Missing K initial condition CCL; using Automatic
 +--------------------------------------------------------------------+
 |                                                                    |
 |                               Solver                               |
 |                                                                    |
 +--------------------------------------------------------------------+




 +--------------------------------------------------------------------+
 |                                                                    |
 |                       ANSYS CFX Solver 11.0                        |
 |                                                                    |
 | Version 2007.01.15-19.20            Mon Jan 15 19:24:21 GMTST 2007 |
 |                                                                    |
 |                       Executable Attributes                        |
 |                                                                    |
 |  single-int32-32bit-novc6-optimised-supfort-noprof-nospag-lcomp    |
 |                                                                    |
 | Copyright 1996-2007 ANSYS Europe Ltd.                              |
 +--------------------------------------------------------------------+





 +--------------------------------------------------------------------+
 |                          Job Information                           |
 +--------------------------------------------------------------------+

 Run mode:       serial run

 Host computer:  rzc3021
 Job started:    Mon Oct 15 19:52:38 2007


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

  Data Type      Kwords  Words/Node  Words/Elem      Kbytes Bytes/Node
 
  Real          36521.7      424.81       78.89    142663.0    1699.26
  Integer       15543.6      180.80       33.58     60717.2     723.20
  Character      2815.8       32.75        6.08      2749.8      32.75
  Logical          65.0        0.76        0.14       253.9       3.02
  Double          608.0        7.07        1.31      4750.0      56.58

 +--------------------------------------------------------------------+
 |                          Mesh Statistics                           |
 +--------------------------------------------------------------------+

 Domain Name : Default Domain

     Total Number of Nodes                                =       85971

     Total Number of Elements                             =      462926
         Total Number of Tetrahedrons                     =      462926

     Total Number of Faces                                =       25412
 
     Minimum Orthogonality Angle [degrees]                =     28.5 ok
     Maximum Aspect Ratio                                 =      7.9 OK
     Maximum Mesh Expansion Factor                        =    982.1  !

 +--------------------------------------------------------------------+
 |                     Average Scale Information                      |
 +--------------------------------------------------------------------+

 Domain Name : Default Domain
     Global Length                                         = 1.8529E-01
     Minimum Extent                                        = 2.2775E-01
     Maximum Extent                                        = 4.4665E-01
     Density                                               = 1.1850E+00
     Dynamic Viscosity                                     = 1.8310E-05
     Velocity                                              = 1.0000E+01
     Advection Time                                        = 1.8529E-02
     RMS Courant Number                                    = 7.0588E+02
     Maximum Courant Number                                = 2.4042E+04
     Reynolds Number                                       = 1.1992E+05

 +--------------------------------------------------------------------+
 |                Checking for Isolated Fluid Regions                 |
 +--------------------------------------------------------------------+
 
 No isolated fluid regions were found.
 +--------------------------------------------------------------------+
 | Writing transient file 0_full.trn                                  |
 |   Name   : results                                                 |
 |   Type   : Standard                                                |
 |   Option : Every Timestep                                          |
 +--------------------------------------------------------------------+

 +--------------------------------------------------------------------+
 |              The Equations Solved in This Calculation              |
 +--------------------------------------------------------------------+

 Subsystem : Momentum and Mass

   U-Mom
   V-Mom
   W-Mom
   P-Mass

 Subsystem : TurbKE and Diss.K

   K-TurbKE
   E-Diss.K
                   
 CFD Solver started: Mon Oct 15 19:52:59 2007


 +--------------------------------------------------------------------+
 |                       Convergence History                          |
 +--------------------------------------------------------------------+


 ======================================================================
 |                      Timestepping Information                      |
 ----------------------------------------------------------------------
 |       Timestep       |  RMS Courant Number  |  Max Courant Number  |
 +----------------------+----------------------+----------------------+
 |      5.0000E-02      |        705.88        |        999.99        |
 ----------------------------------------------------------------------

 ======================================================================
 TIME STEP =     1 SIMULATION TIME = 5.0000E-02 CPU SECONDS = 1.041E+01
 ----------------------------------------------------------------------
 COEFFICIENT LOOP ITERATION =    1              CPU SECONDS = 1.041E+01
 ----------------------------------------------------------------------
 |       Equation       | Rate | RMS Res | Max Res |  Linear Solution |
 +----------------------+------+---------+---------+------------------+
 | U-Mom                | 0.00 | 3.8E-04 | 4.7E-03 |       2.6E+00  ok|
 | V-Mom                | 0.00 | 7.7E-05 | 5.8E-04 |       2.9E+00  ok|
 | W-Mom                | 0.00 | 8.6E-05 | 6.2E-04 |       3.1E+00  ok|
 | P-Mass               | 0.00 | 1.7E-02 | 1.9E-01 |  8.5  2.4E-02  OK|
 +----------------------+------+---------+---------+------------------+
 +--------------------------------------------------------------------+
 |                     ****** Notice ******                           |
 |  A wall has been placed at portion(s) of an OUTLET                 |
 |  boundary condition (at  26.9% of the faces,  24.9% of the area)   |
 |  to prevent fluid from flowing into the domain.                    |
 |  The boundary condition name is: Auslass1.                         |
 |  The fluid name is: Air at 25 C.                                   |
 |  If this situation persists, consider switching                    |
 |  to an Opening type boundary condition instead.                    |
 +--------------------------------------------------------------------+
 | K-TurbKE             | 0.00 | 3.4E-02 | 2.0E-01 |  5.4  2.0E-02  OK|
 | E-Diss.K             | 0.00 | 7.8E-02 | 9.6E-01 |  7.5  3.5E-03  OK|
 +----------------------+------+---------+---------+------------------+
 ----------------------------------------------------------------------
 COEFFICIENT LOOP ITERATION =    2              CPU SECONDS = 3.150E+01
 ----------------------------------------------------------------------
 |       Equation       | Rate | RMS Res | Max Res |  Linear Solution |
 +----------------------+------+---------+---------+------------------+