[cote2714]

Hi. I have Problem with the Remesh, the interrupt condition. shooting and does not Remesh. Can you help me with that? thanks.


ICEM-CFX.CCL
------------------------------------------------------------------------------------------------------
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 = 10 [s]
END
TIME STEPS:
Option = Timesteps
Timesteps = 0.01 [s]
END
END
DOMAIN: Default Domain
Coord Frame = Coord 0
Domain Type = Fluid
Location = BODY
BOUNDARY: Inlet
Boundary Type = INLET
Location = INLET
BOUNDARY CONDITIONS:
FLOW DIRECTION:
Option = Normal to Boundary Condition
END
FLOW REGIME:
Option = Subsonic
END
MASS AND MOMENTUM:
Mass Flow Rate = 50 [kg s^-1]
Option = Mass Flow Rate
END
MESH MOTION:
Option = Stationary
END
TURBULENCE:
Option = Medium Intensity and Eddy Viscosity Ratio
END
END
END
BOUNDARY: Oulet
Boundary Type = OUTLET
Location = OULET
BOUNDARY CONDITIONS:
FLOW REGIME:
Option = Subsonic
END
MASS AND MOMENTUM:
Option = Average Static Pressure
Pressure Profile Blend = 0.05
Relative Pressure = 5 [psi]
END
MESH MOTION:
Option = Stationary
END
PRESSURE AVERAGING:
Option = Average Over Whole Outlet
END
END
END
BOUNDARY: Pared
Boundary Type = WALL
Location = WALL
BOUNDARY CONDITIONS:
MASS AND MOMENTUM:
Option = Free Slip Wall
END
MESH MOTION:
Option = Unspecified
END
END
END
BOUNDARY: Wall
Boundary Type = WALL
Location = BOX
BOUNDARY CONDITIONS:
MASS AND MOMENTUM:
Option = No Slip Wall
Wall Velocity Relative To = Mesh Motion
END
MESH MOTION:
Option = Specified Displacement
DISPLACEMENT:
Displacement X Component = 0 [m]
Displacement Y Component = 0 [m]
Displacement Z Component = -Movimiento
Option = Cartesian Components
END
END
WALL ROUGHNESS:
Option = Smooth Wall
END
END
END
DOMAIN MODELS:
BUOYANCY MODEL:
Option = Non Buoyant
END
DOMAIN MOTION:
Option = Stationary
END
MESH DEFORMATION:
Displacement Relative To = Previous Mesh
Option = Regions of Motion Specified
MESH MOTION MODEL:
Option = Displacement Diffusion
MESH STIFFNESS:
Option = Increase near Small Volumes
Stiffness Model Exponent = 10
REFERENCE VOLUME:
Option = Mean Control Volume
END
END
END
END
REFERENCE PRESSURE:
Reference Pressure = 1 [atm]
END
END
FLUID DEFINITION: agua
Material = Water
Option = Material Library
MORPHOLOGY:
Option = Continuous Fluid
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
END
INITIALISATION:
Option = Automatic
INITIAL CONDITIONS:
Velocity Type = Cartesian
CARTESIAN VELOCITY COMPONENTS:
Option = Automatic with Value
U = 0 [m s^-1]
V = 0 [m s^-1]
W = 0 [m s^-1]
END
STATIC PRESSURE:
Option = Automatic with Value
Relative Pressure = 0 [psi]
END
TURBULENCE INITIAL CONDITIONS:
Option = Medium Intensity and Eddy Viscosity Ratio
END
END
END
OUTPUT CONTROL:
BACKUP RESULTS: Backup Results 1
File Compression Level = Default
Option = Standard
OUTPUT FREQUENCY:
Option = Timestep Interval
Timestep Interval = 50
END
END
MONITOR OBJECTS:
MONITOR BALANCES:
Option = Full
END
MONITOR FORCES:
Option = Full
END
MONITOR PARTICLES:
Option = Full
END
MONITOR POINT: Desplazamiento en Z
Coord Frame = Coord 0
Expression Value = areaAve(Total Centroid Displacement Z)@Wall
Option = Expression
END
MONITOR POINT: Mesh Quality
Coord Frame = Coord 0
Expression Value = minVal(Orthogonality Angle Minimum)@Default Domain
Option = Expression
END
MONITOR POINT: Remesh
Coord Frame = Coord 0
Expression Value = minVal(Orthogonality Angle Minimum)@Default Domain \
< 15[deg]
Option = Expression
END
MONITOR RESIDUALS:
Option = Full
END
MONITOR TOTALS:
Option = Full
END
END
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 = 10
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
INTERRUPT CONTROL:
INTERRUPT CONDITION: Interrupt Condition 1
Logical Expression = RemeshingCond
Option = Logical Expression
END
END
TRANSIENT SCHEME:
Option = Second Order Backward Euler
TIMESTEP INITIALISATION:
Option = Automatic
END
END
END
END
COMMAND FILE:
Version = 15.0
END
SIMULATION CONTROL:
CONFIGURATION CONTROL:
CONFIGURATION: Configuration 1
Flow Name = Flow Analysis 1
ACTIVATION CONTROL:
CONTROL CONDITION: Activation Condition 1
Option = Start of Simulation
END
END
REMESH: Remesh 1
Activation Condition List = Interrupt Condition 1
Geometry File = D:\Simulaciones \
Tesistas\PIG\Caja-Tubo\ICEM-CFX\ICEM-CFX_files\dp0\ICM\ICEMCFD\ICM.t\
in
Location = BODY
Mesh Replay File = D:\Simulaciones \
Tesistas\PIG\Caja-Tubo\ICEM-CFX\ICEM-CFX_files\dp0\ICM\ICEMCFD\caja.\
rpl
Option = ICEM CFD Replay
ICEM CFD GEOMETRY CONTROL:
Option = Automatic
ICEM CFD PART MAP: box
Boundary = Wall
ICEM CFD Parts List = BOX
END
END
ICEM CFD MESH CONTROL:
Option = None
END
SCALAR PARAMETER: Desplazamiento en Z
Monitor Point = Desplazamiento en Z
END
END
END
---------------------------------------------------------------------------
I used this tutorial of the EDR company.

http://es.scribd.com/doc/73381400/AN...ing-EDR#scribd

if you want image of the setup, I can give it to you.