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This run of the CFX Release 17.0 Solver started at 12:11:01 on 28 Apr 2016 by user A.Chernomazov on WS-NT-02 (intel_xeon64.sse2_winnt) using the command: "C:\Program Files\ANSYS Inc\v170\CFX\bin\perllib\cfx5solve.pl" -stdout-comms -batch -ccl - Release 17.0 Point Releases and Patches installed: ANSYS, Inc. Products Release 17.0 ANSYS Mechanical Products Release 17.0 ANSYS Autodyn Release 17.0 ANSYS LS-DYNA Release 17.0 ANSYS AIM Release 17.0 ANSYS CFX (includes ANSYS CFD-Post) Release 17.0 ANSYS Fluent (includes ANSYS CFD-Post) Release 17.0 ANSYS TurboGrid Release 17.0 ANSYS Polyflow (includes ANSYS CFD-Post) Release 17.0 ANSYS Forte Release 17.0 ANSYS ICEM CFD Release 17.0 ANSYS Aqwa Release 17.0 ANSYS Composite PrepPost Release 17.0 ANSYS Icepak (includes ANSYS CFD-Post) Release 17.0 AutoCAD Release 17.0 ACIS Release 17.0 Catia, Version 4 Release 17.0 Catia, Version 6 Release 17.0 Creo Elements/Direct Modeling Release 17.0 Inventor Release 17.0 JTOpen Release 17.0 NX Release 17.0 Parasolid Release 17.0 Creo Parametric (formerly Pro/ENGINEER) Release 17.0 Solid Edge Release 17.0 SolidWorks Release 17.0 ANSYS, Inc. License Manager Release 17.0 ANSYS Customization Files for User Programmable Features Release 17.0 ANSYS CFD-Post only Release 17.0 Catia, Version 5 Release 17.0 Setting up CFX Solver run ... +--------------------------------------------------------------------+ | | | CFX Command Language for Run | | | +--------------------------------------------------------------------+

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Page 1: cae-club.ru · Web viewANSYS ICEM CFD Release 17.0 ANSYS Aqwa Release 17.0 ANSYS Composite PrepPost Release 17.0 ANSYS Icepak (includes ANSYS CFD-Post) Release 17.0 AutoCAD Release

This run of the CFX Release 17.0 Solver started at 12:11:01 on 28 Apr 2016 by user A.Chernomazov on WS-NT-02 (intel_xeon64.sse2_winnt) using the command: "C:\Program Files\ANSYS Inc\v170\CFX\bin\perllib\cfx5solve.pl" -stdout-comms -batch -ccl - Release 17.0 Point Releases and Patches installed: ANSYS, Inc. Products Release 17.0 ANSYS Mechanical Products Release 17.0 ANSYS Autodyn Release 17.0 ANSYS LS-DYNA Release 17.0 ANSYS AIM Release 17.0 ANSYS CFX (includes ANSYS CFD-Post) Release 17.0 ANSYS Fluent (includes ANSYS CFD-Post) Release 17.0 ANSYS TurboGrid Release 17.0 ANSYS Polyflow (includes ANSYS CFD-Post) Release 17.0 ANSYS Forte Release 17.0 ANSYS ICEM CFD Release 17.0 ANSYS Aqwa Release 17.0 ANSYS Composite PrepPost Release 17.0 ANSYS Icepak (includes ANSYS CFD-Post) Release 17.0 AutoCAD Release 17.0 ACIS Release 17.0 Catia, Version 4 Release 17.0 Catia, Version 6 Release 17.0 Creo Elements/Direct Modeling Release 17.0 Inventor Release 17.0 JTOpen Release 17.0 NX Release 17.0 Parasolid Release 17.0 Creo Parametric (formerly Pro/ENGINEER) Release 17.0 Solid Edge Release 17.0 SolidWorks Release 17.0 ANSYS, Inc. License Manager Release 17.0 ANSYS Customization Files for User Programmable Features Release 17.0 ANSYS CFD-Post only Release 17.0 Catia, Version 5 Release 17.0 Setting up CFX Solver run ...

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

LIBRARY: MATERIAL: Air Ideal Gas Material Description = Air Ideal Gas (constant Cp) Material Group = Air Data, Calorically Perfect Ideal Gases Option = Pure Substance Thermodynamic State = Gas PROPERTIES: Option = General Material EQUATION OF STATE: Molar Mass = 28.96 [kg kmol^-1] Option = Ideal Gas

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END SPECIFIC HEAT CAPACITY: Option = Value Specific Heat Capacity = 1.0044E+03 [J kg^-1 K^-1] Specific Heat Type = Constant Pressure 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 DYNAMIC VISCOSITY: Dynamic Viscosity = 1.831E-05 [kg m^-1 s^-1] Option = Value END THERMAL CONDUCTIVITY: Option = Value Thermal Conductivity = 2.61E-2 [W m^-1 K^-1] END ABSORPTION COEFFICIENT: Absorption Coefficient = 0.01 [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 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 Blade Row EXTERNAL SOLVER COUPLING: Option = None END INITIAL TIME: Option = Automatic with Value Time = 0 [s] END END DOMAIN: R1 Coord Frame = Coord 0 Domain Type = Fluid Location = Entire Passage 2 BOUNDARY: R1 Blade Boundary Type = WALL

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Frame Type = Rotating Location = BLADE 2,BLADE 2 2 BOUNDARY CONDITIONS: HEAT TRANSFER: Option = Adiabatic END MASS AND MOMENTUM: Option = No Slip Wall END WALL ROUGHNESS: Option = Smooth Wall END END END BOUNDARY: R1 Hub Boundary Type = WALL Coord Frame = Coord 0 Frame Type = Rotating Location = HUB 2,HUB 2 2 BOUNDARY CONDITIONS: HEAT TRANSFER: Option = Adiabatic END MASS AND MOMENTUM: Option = No Slip Wall END WALL ROUGHNESS: Option = Smooth Wall END END END BOUNDARY: R1 Internal Interface 1 Side 1 Boundary Type = INTERFACE Location = PER1 2 2 BOUNDARY CONDITIONS: HEAT TRANSFER: Option = Conservative Interface Flux END MASS AND MOMENTUM: Option = Conservative Interface Flux END TURBULENCE: Option = Conservative Interface Flux END END END BOUNDARY: R1 Internal Interface 1 Side 2 Boundary Type = INTERFACE Location = PER2 2 BOUNDARY CONDITIONS: HEAT TRANSFER: Option = Conservative Interface Flux END MASS AND MOMENTUM: Option = Conservative Interface Flux END TURBULENCE: Option = Conservative Interface Flux END END END

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BOUNDARY: R1 Outlet Boundary Type = OUTLET Frame Type = Stationary Location = OUTFLOW 2,OUTFLOW 2 2 BOUNDARY CONDITIONS: FLOW REGIME: Option = Subsonic END MASS AND MOMENTUM: Normal Speed = 185 [m s^-1] Option = Normal Speed END END END BOUNDARY: R1 Shroud Boundary Type = WALL Coord Frame = Coord 0 Frame Type = Rotating Location = SHROUD 2,SHROUD 2 2 BOUNDARY CONDITIONS: HEAT TRANSFER: Option = Adiabatic END MASS AND MOMENTUM: Option = No Slip Wall WALL VELOCITY: Option = Counter Rotating Wall END END WALL ROUGHNESS: Option = Smooth Wall END END END BOUNDARY: R1 to R1 Internal 2 Side 1 Boundary Type = INTERFACE Location = SHROUD TIP GGI SIDE 1 2 BOUNDARY CONDITIONS: HEAT TRANSFER: Option = Conservative Interface Flux END MASS AND MOMENTUM: Option = Conservative Interface Flux END TURBULENCE: Option = Conservative Interface Flux END END END BOUNDARY: R1 to R1 Internal 2 Side 2 Boundary Type = INTERFACE Location = SHROUD TIP GGI SIDE 2 2 BOUNDARY CONDITIONS: HEAT TRANSFER: Option = Conservative Interface Flux END MASS AND MOMENTUM: Option = Conservative Interface Flux END TURBULENCE: Option = Conservative Interface Flux

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END END END BOUNDARY: R1 to R1 Internal Side 1 Boundary Type = INTERFACE Location = SHROUD TIP GGI SIDE 1 BOUNDARY CONDITIONS: HEAT TRANSFER: Option = Conservative Interface Flux END MASS AND MOMENTUM: Option = Conservative Interface Flux END TURBULENCE: Option = Conservative Interface Flux END END END BOUNDARY: R1 to R1 Internal Side 2 Boundary Type = INTERFACE Location = SHROUD TIP GGI SIDE 2 BOUNDARY CONDITIONS: HEAT TRANSFER: Option = Conservative Interface Flux END MASS AND MOMENTUM: Option = Conservative Interface Flux END TURBULENCE: Option = Conservative Interface Flux END END END BOUNDARY: R1 to R1 Periodic 1 Side 1 Boundary Type = INTERFACE Location = PER1 2 BOUNDARY CONDITIONS: HEAT TRANSFER: Option = Conservative Interface Flux END MASS AND MOMENTUM: Option = Conservative Interface Flux END TURBULENCE: Option = Conservative Interface Flux END END END BOUNDARY: R1 to R1 Periodic 1 Side 2 Boundary Type = INTERFACE Location = PER2 2 2 BOUNDARY CONDITIONS: HEAT TRANSFER: Option = Conservative Interface Flux END MASS AND MOMENTUM: Option = Conservative Interface Flux END TURBULENCE: Option = Conservative Interface Flux END

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END END BOUNDARY: R1 to S1 Side 1 Boundary Type = INTERFACE Location = INFLOW 2,INFLOW 2 2 BOUNDARY CONDITIONS: HEAT TRANSFER: Option = Conservative Interface Flux END MASS AND MOMENTUM: Option = Conservative Interface Flux END TURBULENCE: Option = Conservative Interface Flux END END END DOMAIN MODELS: BUOYANCY MODEL: Option = Non Buoyant END DOMAIN MOTION: Alternate Rotation Model = true Angular Velocity = 41500 [rev min^-1] Option = Rotating AXIS DEFINITION: Option = Coordinate Axis Rotation Axis = Coord 0.3 END END MESH DEFORMATION: Option = None END PASSAGE DEFINITION: Number of Passages in 360 = 16 Number of Passages in Component = 2 END REFERENCE PRESSURE: Reference Pressure = 0 [atm] END END FLUID DEFINITION: Air Ideal Gas Material = Air Ideal Gas Option = Material Library MORPHOLOGY: Option = Continuous Fluid END END FLUID MODELS: COMBUSTION MODEL: Option = None END HEAT TRANSFER MODEL: Include Viscous Work Term = True Option = Total Energy END THERMAL RADIATION MODEL: Option = None END TURBULENCE MODEL: Option = k epsilon

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END TURBULENT WALL FUNCTIONS: High Speed Model = Off Option = Scalable END END END DOMAIN: S1 Coord Frame = Coord 0 Domain Type = Fluid Location = Entire Passage BOUNDARY: R1 to S1 Side 2 Boundary Type = INTERFACE Location = OUTFLOW,OUTFLOW 3 BOUNDARY CONDITIONS: HEAT TRANSFER: Option = Conservative Interface Flux END MASS AND MOMENTUM: Option = Conservative Interface Flux END TURBULENCE: Option = Conservative Interface Flux END END END BOUNDARY: S1 Blade Boundary Type = WALL Location = BLADE,BLADE 3 BOUNDARY CONDITIONS: HEAT TRANSFER: Option = Adiabatic END MASS AND MOMENTUM: Option = No Slip Wall END WALL ROUGHNESS: Option = Smooth Wall END END END BOUNDARY: S1 Hub Boundary Type = WALL Location = HUB,HUB 3 BOUNDARY CONDITIONS: HEAT TRANSFER: Option = Adiabatic END MASS AND MOMENTUM: Option = No Slip Wall END WALL ROUGHNESS: Option = Smooth Wall END END END BOUNDARY: S1 Inlet Boundary Type = INLET Location = INFLOW,INFLOW 3 BOUNDARY CONDITIONS: FLOW REGIME:

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Blend Mach Number Type = Normal Speed Option = Mixed END HEAT TRANSFER: Option = Total Temperature Total Temperature = 1273 [K] END MASS AND MOMENTUM: Normal Speed = 177 [m s^-1] Option = Normal Speed and Total Pressure Relative Total Pressure = 693000 [Pa] END TURBULENCE: Option = Medium Intensity and Eddy Viscosity Ratio END END END BOUNDARY: S1 Internal Interface 2 Side 1 Boundary Type = INTERFACE Location = PER1 3 BOUNDARY CONDITIONS: HEAT TRANSFER: Option = Conservative Interface Flux END MASS AND MOMENTUM: Option = Conservative Interface Flux END TURBULENCE: Option = Conservative Interface Flux END END END BOUNDARY: S1 Internal Interface 2 Side 2 Boundary Type = INTERFACE Location = PER2 BOUNDARY CONDITIONS: HEAT TRANSFER: Option = Conservative Interface Flux END MASS AND MOMENTUM: Option = Conservative Interface Flux END TURBULENCE: Option = Conservative Interface Flux END END END BOUNDARY: S1 Shroud Boundary Type = WALL Location = SHROUD,SHROUD 3 BOUNDARY CONDITIONS: HEAT TRANSFER: Option = Adiabatic END MASS AND MOMENTUM: Option = No Slip Wall END WALL ROUGHNESS: Option = Smooth Wall END END

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END BOUNDARY: S1 to S1 Periodic 1 Side 1 Boundary Type = INTERFACE Location = PER1 BOUNDARY CONDITIONS: HEAT TRANSFER: Option = Conservative Interface Flux END MASS AND MOMENTUM: Option = Conservative Interface Flux END TURBULENCE: Option = Conservative Interface Flux END END END BOUNDARY: S1 to S1 Periodic 1 Side 2 Boundary Type = INTERFACE Location = PER2 3 BOUNDARY CONDITIONS: HEAT TRANSFER: Option = Conservative Interface Flux END MASS AND MOMENTUM: Option = Conservative Interface Flux END TURBULENCE: Option = Conservative Interface Flux END END END DOMAIN MODELS: BUOYANCY MODEL: Option = Non Buoyant END DOMAIN MOTION: Option = Stationary END MESH DEFORMATION: Option = None END PASSAGE DEFINITION: Number of Passages in 360 = 14 Number of Passages in Component = 2 END REFERENCE PRESSURE: Reference Pressure = 0 [atm] END END FLUID DEFINITION: Air Ideal Gas Material = Air Ideal Gas Option = Material Library MORPHOLOGY: Option = Continuous Fluid END END FLUID MODELS: COMBUSTION MODEL: Option = None END HEAT TRANSFER MODEL:

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Include Viscous Work Term = True Option = Total Energy END THERMAL RADIATION MODEL: Option = None END TURBULENCE MODEL: Option = k epsilon END TURBULENT WALL FUNCTIONS: High Speed Model = Off Option = Scalable END END END DOMAIN INTERFACE: R1 Internal Interface 1 Boundary List1 = R1 Internal Interface 1 Side 1 Boundary List2 = R1 Internal Interface 1 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 = Automatic END END DOMAIN INTERFACE: R1 to R1 Internal Boundary List1 = R1 to R1 Internal Side 1 Boundary List2 = R1 to R1 Internal 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

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DOMAIN INTERFACE: R1 to R1 Internal 2 Boundary List1 = R1 to R1 Internal 2 Side 1 Boundary List2 = R1 to R1 Internal 2 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: R1 to R1 Periodic 1 Boundary List1 = R1 to R1 Periodic 1 Side 1 Boundary List2 = R1 to R1 Periodic 1 Side 2 Interface Type = Fluid Fluid INTERFACE MODELS: Option = Rotational Periodicity AXIS DEFINITION: Option = Coordinate Axis Rotation Axis = Coord 0.3 END END MESH CONNECTION: Option = GGI END END DOMAIN INTERFACE: R1 to S1 Boundary List1 = R1 to S1 Side 1 Boundary List2 = R1 to S1 Side 2 Interface Type = Fluid Fluid INTERFACE MODELS: Option = General Connection FRAME CHANGE: Option = Transient Rotor Stator END MASS AND MOMENTUM: Option = Conservative Interface Flux MOMENTUM INTERFACE MODEL: Option = None END END PITCH CHANGE: Option = Automatic END END MESH CONNECTION: Option = GGI END END

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DOMAIN INTERFACE: S1 Internal Interface 2 Boundary List1 = S1 Internal Interface 2 Side 1 Boundary List2 = S1 Internal Interface 2 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 = Automatic END END DOMAIN INTERFACE: S1 to S1 Periodic 1 Boundary List1 = S1 to S1 Periodic 1 Side 1 Boundary List2 = S1 to S1 Periodic 1 Side 2 Interface Type = Fluid Fluid INTERFACE MODELS: Option = Rotational Periodicity AXIS DEFINITION: Option = Coordinate Axis Rotation Axis = Coord 0.3 END END MESH CONNECTION: Option = GGI END END OUTPUT CONTROL: MONITOR OBJECTS: EFFICIENCY OUTPUT: Efficiency Calculation Method = Total to Total Efficiency Type = Both Compression and Expansion Inflow Boundary = S1 Inlet Option = Output To Solver Monitor Outflow Boundary = R1 Outlet END MONITOR BALANCES: Option = Full END MONITOR FORCES: Option = Full END MONITOR PARTICLES: Option = Full END MONITOR RESIDUALS: Option = Full END MONITOR TOTALS: Option = Full

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END END RESULTS: File Compression Level = Default Option = Standard END TRANSIENT BLADE ROW OUTPUT: File Compression Level = Default Option = Selected Variables Output Variables List = Pressure,Velocity DATA COMPRESSION: Number of Fourier Coefficients = 7 Option = Fourier Series Start Accumulation Period = Moving Averages END END END SOLVER CONTROL: Turbulence Numerics = First Order 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 TRANSIENT BLADE ROW MODELS: Option = Fourier Transformation FOURIER TRANSFORMATION: Fourier Transformation 1 Domain Interface = R1 to S1 Option = Rotor Stator FOURIER TRANSFORMATION SIDE 1: Option = Phase Corrected Phase Corrected Interface = R1 to R1 Periodic 1 Sampling Domain Interface = R1 Internal Interface 1 END FOURIER TRANSFORMATION SIDE 2: Option = None END END TRANSIENT METHOD: Option = Time Integration TIME DURATION: Number of Periods per Run = 15 Option = Number of Periods per Run END TIME PERIOD: Computed Passing Period = 0.00010327[s] Domain = S1

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Minimum Number of Timesteps per Period = 8 Option = Automatic END TIME STEPS: Computed Timestep = 6.45438e-006[s] Option = Timestep Multiplier Timestep Multiplier = 2 END END END END COMMAND FILE: Version = 17.0 Results Version = 17.0 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: wsnt02 Remote Host Name = WS-NT-02 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 = \ D:\PROJECT_04\04_Cases\1st_State_TBR_FT\1st_stage_TBR_FT_.def Solver Results File = \ D:\PROJECT_04\04_Cases\1st_State_TBR_FT\1st_stage_TBR_FT__002.res INITIAL VALUES SPECIFICATION: INITIAL VALUES CONTROL: Use Mesh From = Solver Input File END

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INITIAL VALUES: Initial Values 1 File Name = \ D:/PROJECT_04/04_Cases/1st_Stage_SST/1st_stage_ST__001.res Option = Results File END END 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

+--------------------------------------------------------------------+ | | | Interpolation of Initial Values | | | +--------------------------------------------------------------------+

+--------------------------------------------------------------------+ | | | ANSYS(R) CFX(R) Interpolator | | | | Release 17.0 | | Build 17.0 2015.11.30-15.46-135354 | | Mon Nov 30 15:53:59 GMTST 2015 | | | | Executable Attributes | | | | single-64bit-int32-archfort-optimised-noprof-lcomp | | | | (C) 2015 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: serial run

Host computer: WS-NT-02 (PID:9028)

Job started: Thu Apr 28 12:11:03 2016

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

| Real | Integer | Character | Logical | Double ----------+------------+------------+-----------+----------+---------- Mwords | 39.39 | 29.54 | 0.20 | 0.01 | 0.30 Mbytes | 150.26 | 112.69 | 0.19 | 0.04 | 2.29 ----------+------------+------------+-----------+----------+----------

+--------------------------------------------------------------------+ | Host Memory Information (Mbytes) | +--------------------------------------------------------------------+ | Host | System | Allocated | % | +-------------------------+----------------+----------------+--------+ | WS-NT-02 | 8124.02 | 265.47 | 3.27 | +-------------------------+----------------+----------------+--------+

====================================================================== Interpolating Onto Domain "R1" ======================================================================

Total Number of Nodes in the Target Domain = 1203684 Bounding Box Volume of the Target Mesh = 1.00857E-04

Checking all source domains from the source file: Target mesh is different from domain "R1". Target domain motion is different from domain "S1".

Searching for Candidate Source Domains: Domain "R1" Number of Mapped Nodes = 607722 ( 50.5%) Bounding Box Overlap Volume = 6.16408E-05 ( 61.1%) Setting Up Unmapped Nodes: Number of Unmapped Nodes = 595962 ( 49.5%)

Start interpolation of variables: Source Domain Name Mapped Nodes R1 607722 ( 50.5%)

Note: Some candidate domains may not be used.

+--------------------------------------------------------------------+ | Variable Range Information | +--------------------------------------------------------------------+ +--------------------------------------------------------------------+ | Variable Name | min | max | +--------------------------------------------------------------------+ | Isothermal Compressibility | 1.75E-06 | 4.98E-06 | | Thermal Conductivity | 2.61E-02 | 2.61E-02 | | Courant Number | 8.69E-02 | 1.31E+03 | | Density | 5.99E-01 | 1.65E+00 | | Density Derivative wrt Pressure at Constant| 2.63E-06 | 3.60E-06 | | Static Enthalpy | 6.72E+05 | 1.03E+06 | | Rothalpy | 8.38E+05 | 9.80E+05 | | Total Enthalpy | 8.78E+05 | 1.05E+06 | | Static Entropy | 9.03E+02 | 1.17E+03 |

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| Pressure | 2.01E+05 | 5.73E+05 | | Rotational Energy | 2.97E+04 | 6.74E+04 | | Specific Heat Capacity at Constant Pressure| 1.00E+03 | 1.00E+03 | | Turbulence Eddy Dissipation | 3.09E+04 | 3.84E+10 | | Turbulence Eddy Frequency | 7.07E+04 | 5.61E+07 | | Temperature | 9.67E+02 | 1.32E+03 | | Turbulence Kinetic Energy | 4.50E+00 | 2.83E+04 | | Velocity | 2.45E-01 | 6.95E+02 | | Dynamic Viscosity | 1.83E-05 | 1.83E-05 | | Eddy Viscosity | 9.30E-06 | 2.55E-02 | +--------------------------------------------------------------------+

====================================================================== Interpolating Onto Domain "S1" ======================================================================

Total Number of Nodes in the Target Domain = 511314 Bounding Box Volume of the Target Mesh = 1.94600E-04

Checking all source domains from the source file: Target domain motion is different from domain "R1". Target mesh is different from domain "S1".

Searching for Candidate Source Domains: Domain "S1" Number of Mapped Nodes = 255657 ( 50.0%) Bounding Box Overlap Volume = 8.50151E-05 ( 43.7%) Setting Up Unmapped Nodes: Number of Unmapped Nodes = 255657 ( 50.0%) +====================================================================+ | ****** PROBLEM REPORT ****** | |--------------------------------------------------------------------| | Subsystem: Input and Output | | Subroutine name: ErrAction | | Severity level: Fatal Error | | Error message number: 001100279 | |--------------------------------------------------------------------| | Message: | | | | There are no mapped nodes in the domain. | | | | | | | | | | | +====================================================================+ +====================================================================+ | ****** PROBLEM REPORT ****** | |--------------------------------------------------------------------| | Subsystem: Input and Output | | Subroutine name: ErrAction | | Severity level: Fatal Error | | Error message number: 001100279 | |--------------------------------------------------------------------| | Message: | | | | Stopped in routine GET_KVxVxUnMap | | |

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| | | | | | | | +====================================================================+

+--------------------------------------------------------------------+ | An error has occurred in cfx5solve: | | | | Error interpolating results onto the new mesh: C:\Program | | Files\ANSYS Inc\v170\CFX\bin\winnt-amd64\solver-pcmpi.exe exited | | with return code 1. | +--------------------------------------------------------------------+

+--------------------------------------------------------------------+ | The following user files have been saved in the directory | | D:\PROJECT_04\04_Cases\1st_State_TBR_FT\1st_stage_TBR_FT__002: | | | | job | +--------------------------------------------------------------------+

+--------------------------------------------------------------------+ | Warning! | | | | After waiting for 60 seconds, 1 solver manager process(es) appear | | not to have noticed that this run has ended. You may get errors | | removing some files if they are still open in the solver manager. | +--------------------------------------------------------------------+

This run of the ANSYS CFX Solver has finished.