I run multiphaseInterfoam, and I have trouble with the inlet being non-constant (I want it to be constant.)
Here are my alpha-files\
/--------------------------------- C++ -----------------------------------\
FoamFile { version 2.0; format ascii; class volScalarField; location "0"; object alpha.air; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0;
boundaryField { //- Set patchGroups for constraint patches #includeEtc "caseDicts/setConstraintTypes"
inlet { type alphaContactAngle; thetaProperties ( ( freshWater air ) 90 0 0 0 ( saltWater air ) 90 0 0 0 ( freshWater saltWater ) 90 0 0 0 ); value uniform 0; } outlet { type alphaContactAngle; thetaProperties ( ( freshWater air ) 90 0 0 0 ( saltWater air ) 90 0 0 0 ( freshWater saltWater ) 90 0 0 0 ); value uniform 0; } atmosphere { type inletOutlet; inletValue uniform 1; value uniform 1; } barge { type alphaContactAngle; thetaProperties ( ( freshWater air ) 90 0 0 0 ( saltWater air ) 90 0 0 0 ( freshWater saltWater ) 90 0 0 0 ); value uniform 0; } }
alpha.freshwater:
/--------------------------------- C++ -----------------------------------\
FoamFile { version 2.0; format ascii; class volScalarField; location "0"; object alpha.freshWater; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0;
boundaryField { //- Set patchGroups for constraint patches #includeEtc "caseDicts/setConstraintTypes"
inlet { type fixedValue; value $internalField; } outlet { type variableHeightFlowRate; lowerBound 0; upperBound 1; value $internalField; } atmosphere { type inletOutlet; inletValue $internalField; value $internalField; } barge { type zeroGradient; } }
alpha.saltWater
FoamFile { version 2.0; format ascii; class volScalarField; location "0"; object alpha.saltWater; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0;
boundaryField { //- Set patchGroups for constraint patches #includeEtc "caseDicts/setConstraintTypes"
inlet { type fixedValue; value $internalField; } outlet { type variableHeightFlowRate; lowerBound 0; upperBound 1; value $internalField; } atmosphere { type inletOutlet; inletValue $internalField; value $internalField; } barge { type zeroGradient; } }
// ************************************************************************* //
alphas
/--------------------------------- C++ -----------------------------------\
FoamFile { version 2.0; format ascii; class volScalarField; location "0"; object alphas; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0;
boundaryField { //- Set patchGroups for constraint patches #includeEtc "caseDicts/setConstraintTypes"
inlet { type fixedValue; value $internalField; } outlet { type variableHeightFlowRate; lowerBound 0; upperBound 1; value $internalField; } atmosphere { type inletOutlet; inletValue $internalField; value $internalField; } barge { type zeroGradient; } }
// ************************************************************************* //
The above gives the following, wanted, distribtion of fluids for timestep 1
However, after several time the above changes, also at the inlet:
I really don't understand the contactAngle functino used in alpha.air above. I have tried with the following alpha.air
/--------------------------------- C++ -----------------------------------\
FoamFile { version 2.0; format ascii; class volScalarField; location "0"; object alpha.air; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0;
boundaryField { //- Set patchGroups for constraint patches #includeEtc "caseDicts/setConstraintTypes"
inlet { type fixedValue; value $internalField; } outlet { type variableHeightFlowRate; lowerBound 0; upperBound 1; value $internalField; } atmosphere { type inletOutlet; inletValue $internalField; value $internalField; } barge { type zeroGradient; } }
// ************************************************************************* //
With the alpha.air above I get a long error message that includes stuff that is interpreted as internet links so that I am not allowed to pulblish them here. The error message can be seen on this link to the CDF-online forum, where I have also have asked this question.
Does anybvody know how to modify the above files to make the distribution of alpha's at the inlet constant?
In the last version of alpa.air I changed from "internalField uniform 0" to "internalField uniform 1", and now the inlet is constant. I think the internalFIeld value has to equal the default value set in setFieldsDict.