tutorials: Moved the functions entry from controlDict into a functions file
This commit is contained in:
Henry Weller
@ -52,10 +52,5 @@ maxCo 0.5;
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maxDeltaT 1;
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functions
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{
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#includeFunc continuity
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#includeFunc plot
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}
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// ************************************************************************* //
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@ -0,0 +1,20 @@
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/*--------------------------------*- C++ -*----------------------------------*\
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========= |
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\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
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\\ / O peration | Website: https://openfoam.org
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\\ / A nd | Version: dev
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\\/ M anipulation |
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\*---------------------------------------------------------------------------*/
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FoamFile
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{
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format ascii;
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class dictionary;
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location "system";
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object functions;
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}
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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#includeFunc continuity
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#includeFunc plot
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// ************************************************************************* //
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@ -52,10 +52,5 @@ maxCo 0.5;
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maxDeltaT 1;
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functions
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{
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#includeFunc continuity
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#includeFunc plot
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}
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// ************************************************************************* //
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@ -0,0 +1,20 @@
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/*--------------------------------*- C++ -*----------------------------------*\
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========= |
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\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
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\\ / O peration | Website: https://openfoam.org
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\\ / A nd | Version: dev
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\\/ M anipulation |
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\*---------------------------------------------------------------------------*/
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FoamFile
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{
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format ascii;
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class dictionary;
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location "system";
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object functions;
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}
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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#includeFunc continuity
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#includeFunc plot
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// ************************************************************************* //
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@ -52,15 +52,5 @@ maxCo 0.5;
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maxDeltaT 1;
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functions
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{
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#includeFunc populationBalanceSizeDistribution
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(
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name=numberDensity,
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populationBalance=bubbles,
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functionType=numberDensity,
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coordinateType=volume
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)
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}
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// ************************************************************************* //
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@ -0,0 +1,25 @@
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/*--------------------------------*- C++ -*----------------------------------*\
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========= |
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\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
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\\ / O peration | Website: https://openfoam.org
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\\ / A nd | Version: dev
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\\/ M anipulation |
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\*---------------------------------------------------------------------------*/
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FoamFile
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{
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format ascii;
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class dictionary;
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location "system";
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object functions;
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}
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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#includeFunc populationBalanceSizeDistribution
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(
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name=numberDensity,
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populationBalance=bubbles,
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functionType=numberDensity,
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coordinateType=volume
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)
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// ************************************************************************* //
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@ -52,15 +52,5 @@ maxCo 0.5;
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maxDeltaT 1;
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functions
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{
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#includeFunc populationBalanceSizeDistribution
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(
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name=numberDensity,
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populationBalance=bubbles,
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functionType=numberDensity,
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coordinateType=volume
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)
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}
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// ************************************************************************* //
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@ -0,0 +1,25 @@
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/*--------------------------------*- C++ -*----------------------------------*\
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========= |
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\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
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||||
\\ / O peration | Website: https://openfoam.org
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\\ / A nd | Version: dev
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\\/ M anipulation |
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\*---------------------------------------------------------------------------*/
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FoamFile
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{
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format ascii;
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class dictionary;
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location "system";
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object functions;
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}
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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#includeFunc populationBalanceSizeDistribution
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(
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name=numberDensity,
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populationBalance=bubbles,
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functionType=numberDensity,
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coordinateType=volume
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)
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// ************************************************************************* //
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@ -52,15 +52,5 @@ maxCo 0.5;
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maxDeltaT 1;
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functions
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{
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#includeFunc populationBalanceSizeDistribution
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(
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name=numberDensity,
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populationBalance=bubbles,
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functionType=numberDensity,
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coordinateType=volume
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)
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}
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// ************************************************************************* //
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@ -0,0 +1,25 @@
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/*--------------------------------*- C++ -*----------------------------------*\
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========= |
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||||
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
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||||
\\ / O peration | Website: https://openfoam.org
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\\ / A nd | Version: dev
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\\/ M anipulation |
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\*---------------------------------------------------------------------------*/
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FoamFile
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{
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format ascii;
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class dictionary;
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location "system";
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object functions;
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}
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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#includeFunc populationBalanceSizeDistribution
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(
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name=numberDensity,
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populationBalance=bubbles,
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functionType=numberDensity,
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coordinateType=volume
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)
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// ************************************************************************* //
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@ -52,40 +52,5 @@ maxCo 0.5;
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maxDeltaT 1;
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functions
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{
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#includeFunc populationBalanceSizeDistribution
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(
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name=numberDensity,
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populationBalance=bubbles,
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functionType=numberDensity,
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coordinateType=volume
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)
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#includeFunc populationBalanceMoments
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(
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populationBalance=bubbles,
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momentType=integerMoment,
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coordinateType=volume,
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order=1
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)
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#includeFunc populationBalanceMoments
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(
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populationBalance=bubbles,
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momentType=integerMoment,
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coordinateType=volume,
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order=0
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)
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#includeFunc probes
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(
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name=probes,
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points=((0.5 0.5 0.5)),
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integerMoment0(N,v).bubbles,
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integerMoment1(N,v).bubbles,
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writeControl=writeTime
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)
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}
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// ************************************************************************* //
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@ -0,0 +1,50 @@
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/*--------------------------------*- C++ -*----------------------------------*\
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||||
========= |
|
||||
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
|
||||
\\ / O peration | Website: https://openfoam.org
|
||||
\\ / A nd | Version: dev
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||||
\\/ M anipulation |
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\*---------------------------------------------------------------------------*/
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FoamFile
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{
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format ascii;
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class dictionary;
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location "system";
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object functions;
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}
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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#includeFunc populationBalanceSizeDistribution
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(
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name=numberDensity,
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populationBalance=bubbles,
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functionType=numberDensity,
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coordinateType=volume
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)
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#includeFunc populationBalanceMoments
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(
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populationBalance=bubbles,
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momentType=integerMoment,
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coordinateType=volume,
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order=1
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)
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#includeFunc populationBalanceMoments
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(
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populationBalance=bubbles,
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momentType=integerMoment,
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coordinateType=volume,
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order=0
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)
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#includeFunc probes
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(
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name=probes,
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points=((0.5 0.5 0.5)),
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integerMoment0(N,v).bubbles,
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integerMoment1(N,v).bubbles,
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writeControl=writeTime
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)
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// ************************************************************************* //
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@ -52,32 +52,5 @@ maxCo 0.5;
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maxDeltaT 1;
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functions
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{
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#includeFunc residuals
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(
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p_rgh,
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f3.air1.bubbles,
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f9.air2.bubbles,
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f15.air3.bubbles
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)
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#includeFunc graphCell
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(
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name=graph,
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start=(0.05 0 0.05),
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end=(0.05 1.0 0.05),
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axis=y,
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d.bubbles,
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p,
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alpha.air1,
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alpha.air2,
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alpha.air3,
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alpha.bubbles
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)
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#includeFunc cellZoneAverage
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#includeFunc writeObjects(d.air1)
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#includeFunc writeObjects(d.air2)
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#includeFunc writeObjects(d.air3)
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}
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// ************************************************************************* //
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@ -0,0 +1,42 @@
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/*--------------------------------*- C++ -*----------------------------------*\
|
||||
========= |
|
||||
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
|
||||
\\ / O peration | Website: https://openfoam.org
|
||||
\\ / A nd | Version: dev
|
||||
\\/ M anipulation |
|
||||
\*---------------------------------------------------------------------------*/
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FoamFile
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{
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format ascii;
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class dictionary;
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location "system";
|
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object functions;
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}
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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#includeFunc residuals
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(
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p_rgh,
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f3.air1.bubbles,
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f9.air2.bubbles,
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f15.air3.bubbles
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)
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#includeFunc graphCell
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(
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name=graph,
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start=(0.05 0 0.05),
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end=(0.05 1.0 0.05),
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axis=y,
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d.bubbles,
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p,
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alpha.air1,
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alpha.air2,
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alpha.air3,
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alpha.bubbles
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)
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#includeFunc cellZoneAverage
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#includeFunc writeObjects(d.air1)
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#includeFunc writeObjects(d.air2)
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#includeFunc writeObjects(d.air3)
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// ************************************************************************* //
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@ -52,40 +52,5 @@ maxCo 0.5;
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maxDeltaT 1;
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functions
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{
|
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#includeFunc populationBalanceSizeDistribution
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(
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name=numberDensity,
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populationBalance=bubbles,
|
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functionType=numberDensity,
|
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coordinateType=volume
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)
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#includeFunc populationBalanceMoments
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(
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populationBalance=bubbles,
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momentType=integerMoment,
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coordinateType=volume,
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order=1
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)
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#includeFunc populationBalanceMoments
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(
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populationBalance=bubbles,
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momentType=integerMoment,
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coordinateType=volume,
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order=0
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)
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#includeFunc probes
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(
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name=probes,
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points=((0.5 0.5 0.5)),
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integerMoment0(N,v).bubbles,
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integerMoment1(N,v).bubbles,
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writeControl=writeTime
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||||
)
|
||||
}
|
||||
|
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// ************************************************************************* //
|
||||
|
||||
@ -0,0 +1,50 @@
|
||||
/*--------------------------------*- C++ -*----------------------------------*\
|
||||
========= |
|
||||
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
|
||||
\\ / O peration | Website: https://openfoam.org
|
||||
\\ / A nd | Version: dev
|
||||
\\/ M anipulation |
|
||||
\*---------------------------------------------------------------------------*/
|
||||
FoamFile
|
||||
{
|
||||
format ascii;
|
||||
class dictionary;
|
||||
location "system";
|
||||
object functions;
|
||||
}
|
||||
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
|
||||
|
||||
#includeFunc populationBalanceSizeDistribution
|
||||
(
|
||||
name=numberDensity,
|
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populationBalance=bubbles,
|
||||
functionType=numberDensity,
|
||||
coordinateType=volume
|
||||
)
|
||||
|
||||
#includeFunc populationBalanceMoments
|
||||
(
|
||||
populationBalance=bubbles,
|
||||
momentType=integerMoment,
|
||||
coordinateType=volume,
|
||||
order=1
|
||||
)
|
||||
|
||||
#includeFunc populationBalanceMoments
|
||||
(
|
||||
populationBalance=bubbles,
|
||||
momentType=integerMoment,
|
||||
coordinateType=volume,
|
||||
order=0
|
||||
)
|
||||
|
||||
#includeFunc probes
|
||||
(
|
||||
name=probes,
|
||||
points=((0.5 0.5 0.5)),
|
||||
integerMoment0(N,v).bubbles,
|
||||
integerMoment1(N,v).bubbles,
|
||||
writeControl=writeTime
|
||||
)
|
||||
|
||||
// ************************************************************************* //
|
||||
@ -52,25 +52,5 @@ maxCo 0.5;
|
||||
|
||||
maxDeltaT 1;
|
||||
|
||||
functions
|
||||
{
|
||||
#includeFunc populationBalanceSizeDistribution
|
||||
(
|
||||
name=numberDensity,
|
||||
populationBalance=bubbles,
|
||||
functionType=numberDensity,
|
||||
coordinateType=diameter,
|
||||
normalise=yes
|
||||
)
|
||||
|
||||
#includeFunc populationBalanceSizeDistribution
|
||||
(
|
||||
name=volumeDensity,
|
||||
populationBalance=bubbles,
|
||||
functionType=volumeDensity,
|
||||
coordinateType=diameter,
|
||||
normalise=yes
|
||||
)
|
||||
}
|
||||
|
||||
// ************************************************************************* //
|
||||
|
||||
@ -0,0 +1,35 @@
|
||||
/*--------------------------------*- C++ -*----------------------------------*\
|
||||
========= |
|
||||
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
|
||||
\\ / O peration | Website: https://openfoam.org
|
||||
\\ / A nd | Version: dev
|
||||
\\/ M anipulation |
|
||||
\*---------------------------------------------------------------------------*/
|
||||
FoamFile
|
||||
{
|
||||
format ascii;
|
||||
class dictionary;
|
||||
location "system";
|
||||
object functions;
|
||||
}
|
||||
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
|
||||
|
||||
#includeFunc populationBalanceSizeDistribution
|
||||
(
|
||||
name=numberDensity,
|
||||
populationBalance=bubbles,
|
||||
functionType=numberDensity,
|
||||
coordinateType=diameter,
|
||||
normalise=yes
|
||||
)
|
||||
|
||||
#includeFunc populationBalanceSizeDistribution
|
||||
(
|
||||
name=volumeDensity,
|
||||
populationBalance=bubbles,
|
||||
functionType=volumeDensity,
|
||||
coordinateType=diameter,
|
||||
normalise=yes
|
||||
)
|
||||
|
||||
// ************************************************************************* //
|
||||
@ -52,10 +52,5 @@ maxCo 0.5;
|
||||
|
||||
maxDeltaT 1;
|
||||
|
||||
functions
|
||||
{
|
||||
#includeFunc continuity
|
||||
#includeFunc plot
|
||||
}
|
||||
|
||||
// ************************************************************************* //
|
||||
|
||||
@ -0,0 +1,20 @@
|
||||
/*--------------------------------*- C++ -*----------------------------------*\
|
||||
========= |
|
||||
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
|
||||
\\ / O peration | Website: https://openfoam.org
|
||||
\\ / A nd | Version: dev
|
||||
\\/ M anipulation |
|
||||
\*---------------------------------------------------------------------------*/
|
||||
FoamFile
|
||||
{
|
||||
format ascii;
|
||||
class dictionary;
|
||||
location "system";
|
||||
object functions;
|
||||
}
|
||||
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
|
||||
|
||||
#includeFunc continuity
|
||||
#includeFunc plot
|
||||
|
||||
// ************************************************************************* //
|
||||
@ -58,386 +58,5 @@ cacheTemporaryObjects
|
||||
kEpsilon:G
|
||||
);
|
||||
|
||||
combustionFunctions
|
||||
{
|
||||
// Not possible to test here as it needs a case with a combustion model
|
||||
//#includeFunc Qdot
|
||||
|
||||
// Not possible to test here as it needs a XiFoam case
|
||||
//#includeFunc XiReactionRate
|
||||
}
|
||||
|
||||
controlFunctions
|
||||
{
|
||||
#includeFunc stopAtClockTime(stopTime=3600)
|
||||
|
||||
#includeFunc stopAtFile
|
||||
|
||||
#includeFunc time
|
||||
|
||||
#includeFunc writeObjects(kEpsilon:G)
|
||||
}
|
||||
|
||||
fieldsFunctions
|
||||
{
|
||||
#includeFunc age
|
||||
|
||||
#includeFunc components(U)
|
||||
|
||||
#includeFunc CourantNo
|
||||
|
||||
#includeFunc ddt(p)
|
||||
|
||||
#includeFunc div(phi)
|
||||
|
||||
#includeFunc enstrophy
|
||||
|
||||
// !!! Takes a list of fields, not a single field like most others. It has
|
||||
// an inconsistent name convention; i.e., "<fieldName>Mean", rather than
|
||||
// "mean(<fieldName>)". It also does both "mean" and "prime2Mean". Consider
|
||||
// fixing the output field naming and splitting into separate
|
||||
// configurations for the different outputs.
|
||||
#includeFunc fieldAverage(U, k, epsilon)
|
||||
|
||||
#includeFunc flowType
|
||||
|
||||
#includeFunc grad(p)
|
||||
|
||||
#includeFunc Lambda2
|
||||
|
||||
#includeFunc MachNo
|
||||
|
||||
#includeFunc mag(U)
|
||||
|
||||
#includeFunc magSqr(U)
|
||||
|
||||
#includeFunc PecletNo
|
||||
|
||||
// Not possible to test here as it needs a multiphase case
|
||||
//#includeFunc phaseMap
|
||||
|
||||
#includeFunc Q
|
||||
|
||||
#includeFunc randomise(U, magPerturbation=0.1)
|
||||
|
||||
#includeFunc reconstruct(phi)
|
||||
|
||||
#includeFunc scale(age, scale=0.1)
|
||||
|
||||
#includeFunc shearStress
|
||||
|
||||
#includeFunc streamFunction
|
||||
|
||||
#includeFunc surfaceInterpolate(rho, result=rhof)
|
||||
|
||||
#includeFunc totalEnthalpy
|
||||
|
||||
#includeFunc turbulenceFields(nuEff, R, devTau)
|
||||
|
||||
#includeFunc turbulenceIntensity
|
||||
|
||||
#includeFunc vorticity
|
||||
|
||||
#includeFunc wallHeatFlux
|
||||
|
||||
#includeFunc wallHeatTransferCoeff(rho=1.225, Cp=1005, Pr=0.7, Prt=0.9)
|
||||
|
||||
#includeFunc wallShearStress
|
||||
|
||||
#includeFunc writeCellCentres
|
||||
|
||||
#includeFunc writeCellVolumes
|
||||
|
||||
// !!! Only writes the internal parts of vol fields. The name should really
|
||||
// be less general to reflect this; e.g., writeInternalFieldsVTK. However,
|
||||
// a better change would be further library-ise the internals of foamToVTK
|
||||
// and incorporate it into this object so that it writes patches, surface
|
||||
// fields, point fields, lagrangian, etc... Then we could deprecate
|
||||
// foamToVTK in favour of this function.
|
||||
#includeFunc writeVTK(U, p)
|
||||
|
||||
#includeFunc yPlus
|
||||
}
|
||||
|
||||
fieldsOperationsFunctions
|
||||
{
|
||||
// Operation sequence to compute normalised direction of velocity
|
||||
// perturbation from mean
|
||||
#includeFunc subtract(U, UMean, result=u)
|
||||
#includeFunc uniform
|
||||
(
|
||||
fieldType=volScalarField,
|
||||
field=mag(smallU),
|
||||
dimensions=[0 1 -1 0 0 0 0],
|
||||
value=1e-16
|
||||
)
|
||||
#includeFunc add(mag(U), mag(smallU), result=stabilise(mag(U)))
|
||||
#includeFunc divide(u, stabilise(mag(U)), result=uFrac)
|
||||
|
||||
// Operation to compute a tensor by doing an outer vector product
|
||||
#includeFunc multiply(U, u)
|
||||
|
||||
// Operation sequence to compute the log of temperature divided by an
|
||||
// ambient value
|
||||
#includeFunc uniform
|
||||
(
|
||||
fieldType=volScalarField,
|
||||
field=Ta,
|
||||
dimensions=[0 0 0 1 0 0 0],
|
||||
value=297
|
||||
)
|
||||
#includeFunc divide(T, Ta)
|
||||
#includeFunc log(divide(T,Ta))
|
||||
}
|
||||
|
||||
forcesFunctions
|
||||
{
|
||||
#includeFunc forcesIncompressible
|
||||
(
|
||||
patches=(walls),
|
||||
rhoInf=1.225,
|
||||
CofR=(0 0 0),
|
||||
pitchAxis=(0 1 0)
|
||||
)
|
||||
|
||||
#includeFunc forceCoeffsIncompressible
|
||||
(
|
||||
patches=(walls),
|
||||
magUInf=20,
|
||||
lRef=1,
|
||||
Aref=1,
|
||||
CofR=(0 0 0),
|
||||
liftDir=(0 0 1),
|
||||
dragDir=(1 0 0),
|
||||
pitchAxis=(0 1 0)
|
||||
)
|
||||
|
||||
#includeFunc forcesCompressible
|
||||
(
|
||||
patches=(walls),
|
||||
CofR=(0 0 0),
|
||||
pitchAxis=(0 1 0)
|
||||
)
|
||||
|
||||
#includeFunc forceCoeffsCompressible
|
||||
(
|
||||
patches=(walls),
|
||||
magUInf=20,
|
||||
rhoInf=1.225,
|
||||
lRef=1,
|
||||
Aref=1,
|
||||
CofR=(0 0 0),
|
||||
liftDir=(0 0 1),
|
||||
dragDir=(1 0 0),
|
||||
pitchAxis=(0 1 0)
|
||||
)
|
||||
|
||||
// Not possible to test here as it needs a multiphase Euler-Euler case
|
||||
//#includeFunc phaseForces(phase=air)
|
||||
}
|
||||
|
||||
graphsFunctions
|
||||
{
|
||||
#includeFunc graphUniform
|
||||
(
|
||||
start=(-0.5 -0.5 0),
|
||||
end=(0.5 0.5 0),
|
||||
nPoints=100,
|
||||
fields=(p U)
|
||||
)
|
||||
|
||||
#includeFunc graphCell
|
||||
(
|
||||
start=(-0.500001 -0.500001 0),
|
||||
end=(0.500001 0.500001 0),
|
||||
fields=(p U)
|
||||
)
|
||||
|
||||
#includeFunc graphLayerAverage
|
||||
(
|
||||
patches=(inlet),
|
||||
axis=x,
|
||||
fields=(p U)
|
||||
)
|
||||
}
|
||||
|
||||
lagrangianFunctions
|
||||
{
|
||||
// Not possible to test here as it needs a DSMC case
|
||||
//#includeFunc dsmcFields
|
||||
}
|
||||
|
||||
numericalFunctions
|
||||
{
|
||||
#includeFunc residuals(p, U, h, k, epsilon)
|
||||
|
||||
#includeFunc timeStep
|
||||
}
|
||||
|
||||
pressureFunctions
|
||||
{
|
||||
#includeFunc divide(p, rho, result=kinematic(p))
|
||||
|
||||
#includeFunc staticPressureIncompressible(kinematic(p), rhoInf=1.2)
|
||||
|
||||
#includeFunc totalPressureIncompressible(kinematic(p), rhoInf=1.2)
|
||||
|
||||
#includeFunc totalPressureCompressible
|
||||
}
|
||||
|
||||
probesFunctions
|
||||
{
|
||||
#includeFunc probes(points=((-0.2 -0.2 0) (0 0 0) (0.2 0.2 0)), p, U, T)
|
||||
|
||||
#includeFunc internalProbes(points=((-0.2 -0.2 0) (0.2 0.2 0)), p, U, T)
|
||||
|
||||
#includeFunc boundaryProbes
|
||||
(
|
||||
points=((-0.2 -0.2 -0.04) (0.2 0.2 -0.04)),
|
||||
maxDistance=0.02,
|
||||
p,
|
||||
U,
|
||||
T
|
||||
)
|
||||
|
||||
#includeFunc uniform
|
||||
(
|
||||
fieldType=volScalarField,
|
||||
field=alpha.dummy,
|
||||
dimensions=[],
|
||||
value=0.2
|
||||
)
|
||||
|
||||
#includeFunc interfaceHeight
|
||||
(
|
||||
alpha=alpha.dummy,
|
||||
points=((-0.2 -0.2 0) (0.2 0.2 0))
|
||||
)
|
||||
}
|
||||
|
||||
solversFunctions
|
||||
{
|
||||
#includeFunc scalarTransport(s, schemesField=h)
|
||||
|
||||
#includeFunc phaseScalarTransport
|
||||
(
|
||||
s.dummy,
|
||||
solveAlphaPhi=yes,
|
||||
p=p_rgh,
|
||||
rho=rho,
|
||||
schemesField=h
|
||||
)
|
||||
|
||||
// Not possible to test here as not compatible with compressible solvers
|
||||
//#includeFunc particles
|
||||
}
|
||||
|
||||
streamlinesFunctions
|
||||
{
|
||||
#includeFunc streamlinesSphere
|
||||
(
|
||||
centre=(0 0 0),
|
||||
radius=0.1,
|
||||
nPoints=100,
|
||||
p,
|
||||
U,
|
||||
direction=forward
|
||||
)
|
||||
|
||||
#includeFunc streamlinesLine
|
||||
(
|
||||
start=(-0.5 -0.5 -0.05),
|
||||
end=(0.5 0.5 0.05),
|
||||
nPoints=100,
|
||||
p,
|
||||
U,
|
||||
direction=backward
|
||||
)
|
||||
|
||||
#includeFunc streamlinesPatch
|
||||
(
|
||||
patch=inlet,
|
||||
nPoints=100,
|
||||
p,
|
||||
U
|
||||
)
|
||||
|
||||
#includeFunc streamlinesPoints
|
||||
(
|
||||
points=((-0.2 -0.2 0) (0 0 0) (0.2 0.2 0))
|
||||
p,
|
||||
U,
|
||||
direction=forward
|
||||
)
|
||||
}
|
||||
|
||||
surfaceFunctions
|
||||
{
|
||||
#includeFunc cutPlaneSurface(point=(0 0 0), normal=(0 0 1), p, U)
|
||||
|
||||
#includeFunc isoSurface(isoField=nut, isoValue=0.1, p, U)
|
||||
|
||||
#includeFunc patchSurface(patch=walls, p, U)
|
||||
}
|
||||
|
||||
surfaceFieldValueFunctions
|
||||
{
|
||||
#includeFunc patchAverage(patch=inlet, k)
|
||||
|
||||
#includeFunc patchIntegrate(patch=inlet, epsilon)
|
||||
|
||||
#includeFunc patchFlowRate(patch=inlet)
|
||||
|
||||
#includeFunc patchDifference(patch1=inlet, patch2=outlet, p)
|
||||
|
||||
#includeFunc faceZoneAverage(faceZone=f0, U)
|
||||
|
||||
#includeFunc faceZoneFlowRate(faceZone=f0)
|
||||
|
||||
#includeFunc triSurfaceAverage(triSurface=mid.obj, p)
|
||||
|
||||
#includeFunc triSurfaceVolumetricFlowRate(triSurface=mid.obj)
|
||||
|
||||
#includeFunc triSurfaceDifference
|
||||
(
|
||||
name1=nearInlet.obj,
|
||||
name2=nearOutlet.obj,
|
||||
p
|
||||
)
|
||||
}
|
||||
|
||||
volFieldValueFunctions
|
||||
{
|
||||
#includeFunc cellMin(epsilon)
|
||||
|
||||
#includeFunc cellMax(k)
|
||||
|
||||
#includeFunc cellMinMag(U, writeLocation=yes)
|
||||
|
||||
#includeFunc cellMaxMag(U, writeLocation=yes)
|
||||
|
||||
#includeFunc volAverage(p)
|
||||
|
||||
#includeFunc volIntegrate(rho)
|
||||
}
|
||||
|
||||
functions
|
||||
{
|
||||
$combustionFunctions;
|
||||
$controlFunctions;
|
||||
$fieldsFunctions;
|
||||
$fieldsOperationsFunctions;
|
||||
$forcesFunctions;
|
||||
$graphsFunctions;
|
||||
$lagrangianFunctions;
|
||||
$numericalFunctions;
|
||||
$pressureFunctions;
|
||||
$probesFunctions;
|
||||
$solversFunctions;
|
||||
$streamlinesFunctions;
|
||||
$surfaceFunctions;
|
||||
$surfaceFieldValueFunctions;
|
||||
$volFieldValueFunctions;
|
||||
}
|
||||
|
||||
// ************************************************************************* //
|
||||
|
||||
397
test/postProcessing/channel/system/functionSets
Normal file
397
test/postProcessing/channel/system/functionSets
Normal file
@ -0,0 +1,397 @@
|
||||
/*--------------------------------*- C++ -*----------------------------------*\
|
||||
========= |
|
||||
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
|
||||
\\ / O peration | Website: https://openfoam.org
|
||||
\\ / A nd | Version: dev
|
||||
\\/ M anipulation |
|
||||
\*---------------------------------------------------------------------------*/
|
||||
FoamFile
|
||||
{
|
||||
version 2.0;
|
||||
format ascii;
|
||||
class dictionary;
|
||||
location "system";
|
||||
object functions;
|
||||
}
|
||||
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
|
||||
|
||||
combustionFunctions
|
||||
{
|
||||
// Not possible to test here as it needs a case with a combustion model
|
||||
//#includeFunc Qdot
|
||||
|
||||
// Not possible to test here as it needs a XiFoam case
|
||||
//#includeFunc XiReactionRate
|
||||
}
|
||||
|
||||
controlFunctions
|
||||
{
|
||||
#includeFunc stopAtClockTime(stopTime=3600)
|
||||
|
||||
#includeFunc stopAtFile
|
||||
|
||||
#includeFunc time
|
||||
|
||||
#includeFunc writeObjects(kEpsilon:G)
|
||||
}
|
||||
|
||||
fieldsFunctions
|
||||
{
|
||||
#includeFunc age
|
||||
|
||||
#includeFunc components(U)
|
||||
|
||||
#includeFunc CourantNo
|
||||
|
||||
#includeFunc ddt(p)
|
||||
|
||||
#includeFunc div(phi)
|
||||
|
||||
#includeFunc enstrophy
|
||||
|
||||
// !!! Takes a list of fields, not a single field like most others. It has
|
||||
// an inconsistent name convention; i.e., "<fieldName>Mean", rather than
|
||||
// "mean(<fieldName>)". It also does both "mean" and "prime2Mean". Consider
|
||||
// fixing the output field naming and splitting into separate
|
||||
// configurations for the different outputs.
|
||||
#includeFunc fieldAverage(U, k, epsilon)
|
||||
|
||||
#includeFunc flowType
|
||||
|
||||
#includeFunc grad(p)
|
||||
|
||||
#includeFunc Lambda2
|
||||
|
||||
#includeFunc MachNo
|
||||
|
||||
#includeFunc mag(U)
|
||||
|
||||
#includeFunc magSqr(U)
|
||||
|
||||
#includeFunc PecletNo
|
||||
|
||||
// Not possible to test here as it needs a multiphase case
|
||||
//#includeFunc phaseMap
|
||||
|
||||
#includeFunc Q
|
||||
|
||||
#includeFunc randomise(U, magPerturbation=0.1)
|
||||
|
||||
#includeFunc reconstruct(phi)
|
||||
|
||||
#includeFunc scale(age, scale=0.1)
|
||||
|
||||
#includeFunc shearStress
|
||||
|
||||
#includeFunc streamFunction
|
||||
|
||||
#includeFunc surfaceInterpolate(rho, result=rhof)
|
||||
|
||||
#includeFunc totalEnthalpy
|
||||
|
||||
#includeFunc turbulenceFields(nuEff, R, devTau)
|
||||
|
||||
#includeFunc turbulenceIntensity
|
||||
|
||||
#includeFunc vorticity
|
||||
|
||||
#includeFunc wallHeatFlux
|
||||
|
||||
#includeFunc wallHeatTransferCoeff(rho=1.225, Cp=1005, Pr=0.7, Prt=0.9)
|
||||
|
||||
#includeFunc wallShearStress
|
||||
|
||||
#includeFunc writeCellCentres
|
||||
|
||||
#includeFunc writeCellVolumes
|
||||
|
||||
// !!! Only writes the internal parts of vol fields. The name should really
|
||||
// be less general to reflect this; e.g., writeInternalFieldsVTK. However,
|
||||
// a better change would be further library-ise the internals of foamToVTK
|
||||
// and incorporate it into this object so that it writes patches, surface
|
||||
// fields, point fields, lagrangian, etc... Then we could deprecate
|
||||
// foamToVTK in favour of this function.
|
||||
#includeFunc writeVTK(U, p)
|
||||
|
||||
#includeFunc yPlus
|
||||
}
|
||||
|
||||
fieldsOperationsFunctions
|
||||
{
|
||||
// Operation sequence to compute normalised direction of velocity
|
||||
// perturbation from mean
|
||||
#includeFunc subtract(U, UMean, result=u)
|
||||
#includeFunc uniform
|
||||
(
|
||||
fieldType=volScalarField,
|
||||
field=mag(smallU),
|
||||
dimensions=[0 1 -1 0 0 0 0],
|
||||
value=1e-16
|
||||
)
|
||||
#includeFunc add(mag(U), mag(smallU), result=stabilise(mag(U)))
|
||||
#includeFunc divide(u, stabilise(mag(U)), result=uFrac)
|
||||
|
||||
// Operation to compute a tensor by doing an outer vector product
|
||||
#includeFunc multiply(U, u)
|
||||
|
||||
// Operation sequence to compute the log of temperature divided by an
|
||||
// ambient value
|
||||
#includeFunc uniform
|
||||
(
|
||||
fieldType=volScalarField,
|
||||
field=Ta,
|
||||
dimensions=[0 0 0 1 0 0 0],
|
||||
value=297
|
||||
)
|
||||
#includeFunc divide(T, Ta)
|
||||
#includeFunc log(divide(T,Ta))
|
||||
}
|
||||
|
||||
forcesFunctions
|
||||
{
|
||||
#includeFunc forcesIncompressible
|
||||
(
|
||||
patches=(walls),
|
||||
rhoInf=1.225,
|
||||
CofR=(0 0 0),
|
||||
pitchAxis=(0 1 0)
|
||||
)
|
||||
|
||||
#includeFunc forceCoeffsIncompressible
|
||||
(
|
||||
patches=(walls),
|
||||
magUInf=20,
|
||||
lRef=1,
|
||||
Aref=1,
|
||||
CofR=(0 0 0),
|
||||
liftDir=(0 0 1),
|
||||
dragDir=(1 0 0),
|
||||
pitchAxis=(0 1 0)
|
||||
)
|
||||
|
||||
#includeFunc forcesCompressible
|
||||
(
|
||||
patches=(walls),
|
||||
CofR=(0 0 0),
|
||||
pitchAxis=(0 1 0)
|
||||
)
|
||||
|
||||
#includeFunc forceCoeffsCompressible
|
||||
(
|
||||
patches=(walls),
|
||||
magUInf=20,
|
||||
rhoInf=1.225,
|
||||
lRef=1,
|
||||
Aref=1,
|
||||
CofR=(0 0 0),
|
||||
liftDir=(0 0 1),
|
||||
dragDir=(1 0 0),
|
||||
pitchAxis=(0 1 0)
|
||||
)
|
||||
|
||||
// Not possible to test here as it needs a multiphase Euler-Euler case
|
||||
//#includeFunc phaseForces(phase=air)
|
||||
}
|
||||
|
||||
graphsFunctions
|
||||
{
|
||||
#includeFunc graphUniform
|
||||
(
|
||||
start=(-0.5 -0.5 0),
|
||||
end=(0.5 0.5 0),
|
||||
nPoints=100,
|
||||
fields=(p U)
|
||||
)
|
||||
|
||||
#includeFunc graphCell
|
||||
(
|
||||
start=(-0.500001 -0.500001 0),
|
||||
end=(0.500001 0.500001 0),
|
||||
fields=(p U)
|
||||
)
|
||||
|
||||
#includeFunc graphLayerAverage
|
||||
(
|
||||
patches=(inlet),
|
||||
axis=x,
|
||||
fields=(p U)
|
||||
)
|
||||
}
|
||||
|
||||
lagrangianFunctions
|
||||
{
|
||||
// Not possible to test here as it needs a DSMC case
|
||||
//#includeFunc dsmcFields
|
||||
}
|
||||
|
||||
numericalFunctions
|
||||
{
|
||||
#includeFunc residuals(p, U, h, k, epsilon)
|
||||
|
||||
#includeFunc timeStep
|
||||
}
|
||||
|
||||
pressureFunctions
|
||||
{
|
||||
#includeFunc divide(p, rho, result=kinematic(p))
|
||||
|
||||
#includeFunc staticPressureIncompressible(kinematic(p), rhoInf=1.2)
|
||||
|
||||
#includeFunc totalPressureIncompressible(kinematic(p), rhoInf=1.2)
|
||||
|
||||
#includeFunc totalPressureCompressible
|
||||
}
|
||||
|
||||
probesFunctions
|
||||
{
|
||||
#includeFunc probes(points=((-0.2 -0.2 0) (0 0 0) (0.2 0.2 0)), p, U, T)
|
||||
|
||||
#includeFunc internalProbes(points=((-0.2 -0.2 0) (0.2 0.2 0)), p, U, T)
|
||||
|
||||
#includeFunc boundaryProbes
|
||||
(
|
||||
points=((-0.2 -0.2 -0.04) (0.2 0.2 -0.04)),
|
||||
maxDistance=0.02,
|
||||
p,
|
||||
U,
|
||||
T
|
||||
)
|
||||
|
||||
#includeFunc uniform
|
||||
(
|
||||
fieldType=volScalarField,
|
||||
field=alpha.dummy,
|
||||
dimensions=[],
|
||||
value=0.2
|
||||
)
|
||||
|
||||
#includeFunc interfaceHeight
|
||||
(
|
||||
alpha=alpha.dummy,
|
||||
points=((-0.2 -0.2 0) (0.2 0.2 0))
|
||||
)
|
||||
}
|
||||
|
||||
solversFunctions
|
||||
{
|
||||
#includeFunc scalarTransport(s, schemesField=h)
|
||||
|
||||
#includeFunc phaseScalarTransport
|
||||
(
|
||||
s.dummy,
|
||||
solveAlphaPhi=yes,
|
||||
p=p_rgh,
|
||||
rho=rho,
|
||||
schemesField=h
|
||||
)
|
||||
|
||||
// Not possible to test here as not compatible with compressible solvers
|
||||
//#includeFunc particles
|
||||
}
|
||||
|
||||
streamlinesFunctions
|
||||
{
|
||||
#includeFunc streamlinesSphere
|
||||
(
|
||||
centre=(0 0 0),
|
||||
radius=0.1,
|
||||
nPoints=100,
|
||||
p,
|
||||
U,
|
||||
direction=forward
|
||||
)
|
||||
|
||||
#includeFunc streamlinesLine
|
||||
(
|
||||
start=(-0.5 -0.5 -0.05),
|
||||
end=(0.5 0.5 0.05),
|
||||
nPoints=100,
|
||||
p,
|
||||
U,
|
||||
direction=backward
|
||||
)
|
||||
|
||||
#includeFunc streamlinesPatch
|
||||
(
|
||||
patch=inlet,
|
||||
nPoints=100,
|
||||
p,
|
||||
U
|
||||
)
|
||||
|
||||
#includeFunc streamlinesPoints
|
||||
(
|
||||
points=((-0.2 -0.2 0) (0 0 0) (0.2 0.2 0))
|
||||
p,
|
||||
U,
|
||||
direction=forward
|
||||
)
|
||||
}
|
||||
|
||||
surfaceFunctions
|
||||
{
|
||||
#includeFunc cutPlaneSurface(point=(0 0 0), normal=(0 0 1), p, U)
|
||||
|
||||
#includeFunc isoSurface(isoField=nut, isoValue=0.1, p, U)
|
||||
|
||||
#includeFunc patchSurface(patch=walls, p, U)
|
||||
}
|
||||
|
||||
surfaceFieldValueFunctions
|
||||
{
|
||||
#includeFunc patchAverage(patch=inlet, k)
|
||||
|
||||
#includeFunc patchIntegrate(patch=inlet, epsilon)
|
||||
|
||||
#includeFunc patchFlowRate(patch=inlet)
|
||||
|
||||
#includeFunc patchDifference(patch1=inlet, patch2=outlet, p)
|
||||
|
||||
#includeFunc faceZoneAverage(faceZone=f0, U)
|
||||
|
||||
#includeFunc faceZoneFlowRate(faceZone=f0)
|
||||
|
||||
#includeFunc triSurfaceAverage(triSurface=mid.obj, p)
|
||||
|
||||
#includeFunc triSurfaceVolumetricFlowRate(triSurface=mid.obj)
|
||||
|
||||
#includeFunc triSurfaceDifference
|
||||
(
|
||||
name1=nearInlet.obj,
|
||||
name2=nearOutlet.obj,
|
||||
p
|
||||
)
|
||||
}
|
||||
|
||||
volFieldValueFunctions
|
||||
{
|
||||
#includeFunc cellMin(epsilon)
|
||||
|
||||
#includeFunc cellMax(k)
|
||||
|
||||
#includeFunc cellMinMag(U, writeLocation=yes)
|
||||
|
||||
#includeFunc cellMaxMag(U, writeLocation=yes)
|
||||
|
||||
#includeFunc volAverage(p)
|
||||
|
||||
#includeFunc volIntegrate(rho)
|
||||
}
|
||||
|
||||
$combustionFunctions;
|
||||
$controlFunctions;
|
||||
$fieldsFunctions;
|
||||
$fieldsOperationsFunctions;
|
||||
$forcesFunctions;
|
||||
$graphsFunctions;
|
||||
$lagrangianFunctions;
|
||||
$numericalFunctions;
|
||||
$pressureFunctions;
|
||||
$probesFunctions;
|
||||
$solversFunctions;
|
||||
$streamlinesFunctions;
|
||||
$surfaceFunctions;
|
||||
$surfaceFieldValueFunctions;
|
||||
$volFieldValueFunctions;
|
||||
|
||||
// ************************************************************************* //
|
||||
34
test/postProcessing/channel/system/functions
Normal file
34
test/postProcessing/channel/system/functions
Normal file
@ -0,0 +1,34 @@
|
||||
/*--------------------------------*- C++ -*----------------------------------*\
|
||||
========= |
|
||||
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
|
||||
\\ / O peration | Website: https://openfoam.org
|
||||
\\ / A nd | Version: dev
|
||||
\\/ M anipulation |
|
||||
\*---------------------------------------------------------------------------*/
|
||||
FoamFile
|
||||
{
|
||||
version 2.0;
|
||||
format ascii;
|
||||
class dictionary;
|
||||
location "system";
|
||||
object functions;
|
||||
}
|
||||
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
|
||||
|
||||
$functionSets!combustionFunctions;
|
||||
$functionSets!controlFunctions;
|
||||
$functionSets!fieldsFunctions;
|
||||
$functionSets!fieldsOperationsFunctions;
|
||||
$functionSets!forcesFunctions;
|
||||
$functionSets!graphsFunctions;
|
||||
$functionSets!lagrangianFunctions;
|
||||
$functionSets!numericalFunctions;
|
||||
$functionSets!pressureFunctions;
|
||||
$functionSets!probesFunctions;
|
||||
$functionSets!solversFunctions;
|
||||
$functionSets!streamlinesFunctions;
|
||||
$functionSets!surfaceFunctions;
|
||||
$functionSets!surfaceFieldValueFunctions;
|
||||
$functionSets!volFieldValueFunctions;
|
||||
|
||||
// ************************************************************************* //
|
||||
Reference in New Issue
Block a user