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added airlift tutorial case #89

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merged 4 commits into from
Jan 29, 2025
Merged

added airlift tutorial case #89

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7c83767
added airlift tutorial case
mjrahimi Jan 29, 2025
01a7aed
add readme and run.sh to airlift
mjrahimi Jan 29, 2025
d205bac
run the airlift case for one timestep
mjrahimi Jan 29, 2025
5a4cd81
fix the outlet mass fraction
mjrahimi Jan 29, 2025
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44 changes: 44 additions & 0 deletions tutorial_cases/airlift_40m/0.org/H2O.liquid
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/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: 9
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
object water.liquid;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

dimensions [0 0 0 0 0 0 0];

internalField uniform 1;

boundaryField
{
#includeEtc "caseDicts/setConstraintTypes"

inlet
{
type fixedValue;
value $internalField;
}

outlet
{
type inletOutlet;
phi phi.liquid;
inletValue $internalField;
value $internalField;
}

walls
{
type zeroGradient;
}
}

// ************************************************************************* //
44 changes: 44 additions & 0 deletions tutorial_cases/airlift_40m/0.org/N2.gas
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/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: 9
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
object N2.gas;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

dimensions [0 0 0 0 0 0 0];

internalField uniform 1;

boundaryField
{
#includeEtc "caseDicts/setConstraintTypes"

inlet
{
type fixedValue;
value uniform 0.77;
}

outlet
{
type inletOutlet;
phi phi.gas;
inletValue uniform 0;
value uniform 0;
}

walls
{
type zeroGradient;
}
}

// ************************************************************************* //
45 changes: 45 additions & 0 deletions tutorial_cases/airlift_40m/0.org/O2.gas
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/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: 9
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
object O2.gas;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];

internalField uniform 0.0;

#include "${FOAM_CASE}/constant/globalVars"

boundaryField
{
#includeEtc "caseDicts/setConstraintTypes"

inlet
{
type fixedValue;
value uniform 0.23;
}

outlet
{
type inletOutlet;
phi phi.gas;
inletValue uniform 0;
value uniform 0;
}

walls
{
type zeroGradient;
}
}

// ************************************************************************* //
47 changes: 47 additions & 0 deletions tutorial_cases/airlift_40m/0.org/T.gas
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/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: 9
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
object T.gas;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

dimensions [0 0 0 1 0 0 0];

#include "${FOAM_CASE}/constant/globalVars"

internalField uniform $T0;

boundaryField
{
#includeEtc "caseDicts/setConstraintTypes"

inlet
{
type fixedValue;
value $internalField;
}

outlet
{
type inletOutlet;
phi phi.gas;
inletValue $internalField;
value $internalField;
}

walls
{
type zeroGradient;
}

}

// ************************************************************************* //
47 changes: 47 additions & 0 deletions tutorial_cases/airlift_40m/0.org/T.liquid
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/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: 9
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
object T.liquid;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

dimensions [0 0 0 1 0 0 0];

#include "${FOAM_CASE}/constant/globalVars"

internalField uniform $T0;

boundaryField
{
#includeEtc "caseDicts/setConstraintTypes"

inlet
{
type zeroGradient; // As the inlet is only gas we can use zerograd for T.liq
// type fixedValue;
// value $internalField;
}

outlet
{
type inletOutlet;
phi phi.liquid;
inletValue $internalField;
value $internalField;
}

walls
{
type zeroGradient;
}
}

// ************************************************************************* //
45 changes: 45 additions & 0 deletions tutorial_cases/airlift_40m/0.org/U.gas
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/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: 9
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volVectorField;
object U.gas;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

dimensions [0 1 -1 0 0 0 0];

internalField uniform (0 0 0);

#include "${FOAM_CASE}/constant/globalVars"

boundaryField
{
#includeEtc "caseDicts/setConstraintTypes"

inlet
{
type flowRateInletVelocity;
volumetricFlowRate $V_flowRate;
}

outlet
{
type pressureInletOutletVelocity;
phi phi.gas;
value $internalField;
}

walls
{
type slip;
}
}

// ************************************************************************* //
43 changes: 43 additions & 0 deletions tutorial_cases/airlift_40m/0.org/U.liquid
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Original file line number Diff line number Diff line change
@@ -0,0 +1,43 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: 9
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2;
format ascii;
class volVectorField;
object U.liquid;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

dimensions [0 1 -1 0 0 0 0];

internalField uniform (0 0 0);

boundaryField
{
#includeEtc "caseDicts/setConstraintTypes"

inlet
{
type fixedValue;
value $internalField;
}
outlet
{
type pressureInletOutletVelocity;
phi phi.liquid;
value $internalField;
}
walls
{
type noSlip;
}
}


// ************************************************************************* //
45 changes: 45 additions & 0 deletions tutorial_cases/airlift_40m/0.org/Ydefault.gas
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Original file line number Diff line number Diff line change
@@ -0,0 +1,45 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: 9
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
object Ydefault.gas;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

dimensions [0 0 0 0 0 0 0];

internalField uniform 0.0;

boundaryField
{
#includeEtc "caseDicts/setConstraintTypes"

inlet
{
type fixedValue;
value uniform 0.0;
}

outlet
{
type inletOutlet;
phi phi.gas;
inletValue $internalField;
value $internalField;
}

walls
{
type zeroGradient;
}
}


// ************************************************************************* //
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