Files
openfoam/tutorials/verificationAndValidation/turbulentInflow/system/controlDict
Kutalmis Bercin 14a2a8bf55 TUT: add new tutorial case for turbulent inflow BCs
The following three synthetic turbulence inflow boundary conditions are
examined through single-cell-domain smooth-wall plane channel flow setup:

- turbulentDFSEMInlet
- turbulentDigitalFilterInlet variant=digitalFilter
- turbulentDigitalFilterInlet variant=reducedDigitalFilter

The examinations are performed in terms of the first-/second-order turbulence
statistics provided by (Moser et al., (1999)) doi.org/10.1063/1.869966
from smooth-wall plane channel flow direct numerical simulations at Re=395.

Serial executing:

./Allrun

Parallel (decompositionMethod=scotch) executing:

./Allrunparallel
2019-06-19 19:23:53 +01:00

104 lines
2.5 KiB
C++

/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: v1906 |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
application pimpleFoam;
startFrom latestTime;
startTime 0;
stopAt endTime;
endTime 85;
deltaT 4e-3;
writeControl timeStep;
writeInterval 1250;
purgeWrite 0;
writeFormat ascii;
writePrecision 8;
writeCompression off;
timeFormat general;
timePrecision 8;
runTimeModifiable false;
adjustTimeStep false;
functions
{
fieldAverage1
{
type fieldAverage;
libs ("libfieldFunctionObjects.so");
enabled true;
writeControl writeTime;
timeStart 8.5;
restartOnRestart false;
fields
(
U
{
mean on;
prime2Mean on;
base time;
}
);
}
inletSampling
{
type sets;
libs ("libsampling.so");
enabled true;
writeControl writeTime;
timeStart 8.5;
restartOnRestart false;
interpolationScheme cellPoint;
setFormat raw;
fields (UPrime2Mean);
sets
(
inletPatch
{
type face;
axis y;
start (0.0 0 1.57);
end (0.0 2 1.57);
}
inletCell
{
type face;
axis y;
start (0.062832 0 1.57);
end (0.062832 2 1.57);
}
);
}
}
// ************************************************************************* //