src/OpenFOAM logo
The Open Source CFD Toolbox
  Search
  
  Back to OpenFOAM Home
 
  OpenFOAM FEATURES
  Solvers
  Creating solvers
  Standard solvers
  Pre-processing
  The FoamX case manager
  Other pre-processing utilities
  Post-processing
  The paraFoam post-processor
  Third-party post-processing
  Other post-processing utilities
  Mesh processing
  Mesh generation
  Mesh converters
  Mesh manipulation
  Model libraries
  Turbulence
  Large-eddy simulation (LES)
  Transport models
  Thermophysical models
  Lagrangian particle tracking
  Chemical kinetics
  Other features
  Linear system solvers
  ODE system solvers
  Parallel computing
  Mesh motion
  Numerical method
 
  © 2004-2008 OpenCFD Ltd
SourceForge.net Logo
OpenCFD Solutions Contact OpenFOAM
Other post-processing utilities

OpenFOAM is distributed with a set of utilities that perform specific post-processing tasks, as listed below.

Post-processing the velocity field


Co Configurable graph drawing program
divU Calculates and writes the divergence of velocity field U at each time
enstrophy Calculates and writes the enstrophy of velocity field U at each time
flowType Calculates and writes the flowType of velocity field U at each time
Lambda2 Calculates and writes the second largest eigenvalue of the sum of the square of the symmetrical and anti-symmetrical parts of the velocity gradient tensor, for each time
Mach Calculates and writes the local Mach number from the velocity field U at each time
magGradU Calculates and writes the scalar magnitude of velocity field U at each time
magU Calculates and writes the scalar magnitude of the gradient of the velocity field U for each time
Pe Calculates and writes the Pe number as a surfaceScalarField obtained from field phi for each time
Q Calculates and writes the second invariant of the velocity gradient tensor for each time
streamFunction Calculates and writes the stream function of velocity field U at each time
Ucomponents Writes the three scalar fields, Ux, Uy and Uz, for each component of the velocity field U for each time
uprime Calculates and writes the scalar field of uprime ( V~ ---
  2k
  3  \special {t4ht=) at each time
vorticity Calculates and writes the vorticity of velocity field U at each time
Post-processing the stress field


R Calculates and writes the Reynolds stress R for the current time step
Rcomponents Calculates and writes the scalar fields of the six components of the Reynolds stress R for each time
stressComponents Calculates and writes the scalar fields of the six components of the stress tensor sigma for each time
Post-processing at patches


patchAverage Calculate average of fields over all patches
patchIntegrate Integrates fields over all patches
Post-processing at a wall


checkYPlus Calculates and reports yPlus for all wall patches, for each time in a database
wallGradU Calculates and writes the gradient of U at the wall
wallHeatFlux Calculates and writes the heat flux for all patches as the boundary field of a volScalarField and also prints the integrated flux for all wall patches
wallShearStress Calculates and writes the wall shear stress for the current time step
yPlusLES Calculates the yPlus of the near-wall cells for an LES
Other post-processing


engineCompRatio Calculate the geometric compression ratio. Note that if you have valves and/or extra volumes it will not work, since it calculates the volume at BDC and TCD
postChannel Post-processes data from channel flow calculations
ptot For each time: calculate the total pressure
sample Sample field data with a choice of interpolation schemes, sampling options and write formats
sampleSurface Surface sampling. Runs in parallel (but does not merge points)
wdot Calculates and writes wdot for each time
writeCellCentres Write the three components of the cell centres as volScalarFields so they can be used in postprocessing in thresholding