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March 11, 2014, 20:22 |
I got code 1 error from ANSYS CFX
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New Member
Chaeyeong Kim
Join Date: Mar 2014
Posts: 1
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you can check my modelling from attachment file.
below this line is the error message which i got from ANSYS CFX I don't know What is the PROBLEM!!! would you guys explain this in detail? ------------------------------------------------------------------------- Setting up CFX Solver run ... +--------------------------------------------------------------------+ | | | CFX Command Language for Run | | | +--------------------------------------------------------------------+ LIBRARY: 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 EQUATION OF STATE: Density = 1.185 [kg m^-3] Molar Mass = 28.96 [kg kmol^-1] Option = Value 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 = Automatic END DYNAMIC VISCOSITY: Dynamic Viscosity = 1.831E-05 [kg m^-1 s^-1] Option = Value END THERMAL CONDUCTIVITY: Option = Value Thermal Conductivity = 2.61E-02 [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 THERMAL EXPANSIVITY: Option = Value Thermal Expansivity = 0.003356 [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 = B20, B6 BOUNDARY: Default Domain Default Boundary Type = WALL Location = F7.6 BOUNDARY CONDITIONS: MASS AND MOMENTUM: Option = No Slip Wall END WALL ROUGHNESS: Option = Smooth Wall END END END BOUNDARY: inlet Boundary Type = INLET Location = F26.20 BOUNDARY CONDITIONS: FLOW REGIME: Option = Subsonic END MASS AND MOMENTUM: Normal Speed = 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 = F22.20 BOUNDARY CONDITIONS: FLOW REGIME: Option = Subsonic END MASS AND MOMENTUM: Option = Static Pressure Relative Pressure = 0 [Pa] END END END BOUNDARY: wall Boundary Type = WALL Location = F21.20,F23.20,F24.20,F25.20 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: Fluid 1 Material = Air at 25 C 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 = k epsilon END TURBULENT WALL FUNCTIONS: Option = Scalable END END END OUTPUT CONTROL: RESULTS: File Compression Level = Default Option = Standard END END SOLVER CONTROL: Turbulence Numerics = First Order ADVECTION SCHEME: Option = Upwind END CONVERGENCE CONTROL: Length Scale Option = Conservative Maximum Number of Iterations = 20 Minimum Number of Iterations = 1 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 = 13.0 Results Version = 13.0 END SIMULATION CONTROL: EXECUTION CONTROL: EXECUTABLE SELECTION: Double Precision = Off END INTERPOLATOR STEP CONTROL: Runtime Priority = Standard MEMORY CONTROL: Memory Allocation Factor = 1.0 END END PARALLEL HOST LIBRARY: HOST DEFINITION: kimliapc Remote Host Name = KIMLIA-PC 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 END END RUN DEFINITION: Run Mode = Full Solver Input File = Fluid Flow CFX.def INITIAL VALUES SPECIFICATION: INITIAL VALUES CONTROL: Use Mesh From = Solver Input File Continue History From = Workbench Initial Values END INITIAL VALUES: Workbench Initial Values Option = Results File File Name = Fluid Flow CFX_001.res 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 CFX Interpolator 13.0 | | | | Version 2010.10.01-23.02 Sat Oct 2 02:31:59 GMTDT 2010 | | | | Executable Attributes | | | | single-int32-64bit-novc8-noifort-novc6-optimised-supfort-noprof-nos| | | | Copyright 2010 ANSYS Inc. | +--------------------------------------------------------------------+ +--------------------------------------------------------------------+ | Job Information | +--------------------------------------------------------------------+ Run mode: serial run Host computer: KIMLIA-PC (PID:4004) Job started: Wed Mar 12 09:16:33 2014 +--------------------------------------------------------------------+ | Memory Allocated for Run (Actual usage may be less) | +--------------------------------------------------------------------+ Data Type Kwords Words/Node Words/Elem Kbytes Bytes/Node Real 12672.0 71.05 13.57 49499.9 284.19 Integer 16508.7 92.56 17.68 64487.0 370.24 Character 200.0 1.12 0.21 195.3 1.12 Logical 10.0 0.06 0.01 39.1 0.22 Double 300.0 1.68 0.32 2343.8 13.46 ================================================== ==================== Interpolating Onto Domain "Default Domain" ================================================== ==================== Total Number of Nodes in the Target Domain = 178357 Bounding Box Volume of the Target Mesh = 2.88000E+03 Checking all source domains from the source file: Target mesh is the same as domain "Default Domain". Start direct copying of variables from domain "Default Domain". +--------------------------------------------------------------------+ | Variable Range Information | +--------------------------------------------------------------------+ +--------------------------------------------------------------------+ | Variable Name | min | max | +--------------------------------------------------------------------+ | Thermal Conductivity | 2.61E-02 | 2.61E-02 | | Courant Number | 0.00E+00 | 0.00E+00 | | Density | 1.18E+00 | 1.18E+00 | | Isolated Volumes | 1.00E+00 | 2.00E+00 | | Static Entropy | 0.00E+00 | 0.00E+00 | | Pressure | 8.06E+05 | 8.06E+05 | | Specific Heat Capacity at Constant Pressure| 1.00E+03 | 1.00E+03 | | Turbulence Eddy Dissipation | 3.20E+03 | 3.20E+03 | | Temperature | 2.98E+02 | 2.98E+02 | | Turbulence Kinetic Energy | 2.34E+00 | 2.34E+00 | | Velocity | 2.50E+01 | 2.50E+01 | | Dynamic Viscosity | 1.83E-05 | 1.83E-05 | | Eddy Viscosity | 1.83E-04 | 1.83E-04 | Details of error:- Details of error:- ---------------- ---------------- Error detected by routine MAKDAT Error detected by routine MAKDAT Illegal data area length CDANAM = NCOMPT CDTYPE = INTR ISIZE = 0 Illegal data area length CDANAM = NCOMPT CDTYPE = INTR ISIZE = 0 CRESLT = SIZE CRESLT = SIZE Current Directory : /INTERP/SOLUTION/DST/VX Current Directory : /INTERP/SOLUTION/DST/VX +================================================= ===================+ | ****** PROBLEM REPORT ****** | |--------------------------------------------------------------------| | Subsystem: Input and Output | | Subroutine name: ErrAction | | Severity level: Fatal Error | | Error message number: 001100279 | |--------------------------------------------------------------------| | Message: | | | | Stopped in routine MEMERR | | | | | | | | | | | +================================================= ===================+ +--------------------------------------------------------------------+ | An error has occurred in cfx5solve: | | | | Error interpolating results onto the new mesh: C:\Program | | Files\ANSYS Inc\v130\CFX\bin\winnt-amd64\solver-hpmpi.exe exited | | with return code 1. | +--------------------------------------------------------------------+ |
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