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Commit 438d82ec authored by Henry's avatar Henry
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compressibleTwoPhaseEulerFoam/bubbleColumn: Updated phase names

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with 36 additions and 2186 deletions
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object T1;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 1 0 0 0];
internalField uniform 300;
boundaryField
{
walls
{
type zeroGradient;
}
outlet
{
type inletOutlet;
phi phi1;
inletValue $internalField;
value $internalField;
}
inlet
{
type fixedValue;
value $internalField;
}
frontAndBackPlanes
{
type empty;
}
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object T2;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 1 0 0 0];
internalField uniform 350;
boundaryField
{
walls
{
type zeroGradient;
}
outlet
{
type inletOutlet;
phi phi2;
inletValue uniform 300;
value $internalField;
}
inlet
{
type fixedValue;
value $internalField;
}
frontAndBackPlanes
{
type empty;
}
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format binary;
class volVectorField;
object U1;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (0 0.1 0);
boundaryField
{
inlet
{
type fixedValue;
value $internalField;
}
outlet
{
type pressureInletOutletVelocity;
phi phi1;
value $internalField;
}
walls
{
type fixedValue;
value uniform (0 0 0);
}
}
// ************************************************************************* //
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format binary;
class volVectorField;
object U2;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (0 0 0);
boundaryField
{
inlet
{
type fixedValue;
value $internalField;
}
outlet
{
type pressureInletOutletVelocity;
phi phi2;
value $internalField;
}
walls
{
type fixedValue;
value uniform (0 0 0);
}
}
// ************************************************************************* //
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object alpha1;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField nonuniform List<scalar>
1875
(
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)
;
boundaryField
{
inlet
{
type fixedValue;
value uniform 0.5;
}
outlet
{
type inletOutlet;
phi phi1;
inletValue uniform 1;
value uniform 1;
}
walls
{
type zeroGradient;
}
defaultFaces
{
type empty;
}
}
// ************************************************************************* //
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object alpha1;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0;
boundaryField
{
inlet
{
type fixedValue;
value uniform 0.5;
}
outlet
{
type inletOutlet;
phi phi1;
inletValue uniform 1;
value uniform 1;
}
walls
{
type zeroGradient;
}
}
// ************************************************************************* //
......@@ -15,13 +15,13 @@ FoamFile
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dragModel1 SchillerNaumann;
dragModel2 SchillerNaumann;
dragModelair SchillerNaumann;
dragModelwater SchillerNaumann;
heatTransferModel1 RanzMarshall;
heatTransferModel2 RanzMarshall;
heatTransferModelair RanzMarshall;
heatTransferModelwater RanzMarshall;
dispersedPhase both;
dispersedPhase both;
residualPhaseFraction 1e-3;
residualSlip 1e-2;
......
......@@ -38,6 +38,7 @@ FoamFile
defaultFaces
{
type empty;
inGroups 1(empty);
nFaces 3750;
startFace 3850;
}
......
......@@ -15,16 +15,10 @@ FoamFile
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
phase1
{
rho 1;
rho0 0;
R 287;
Cp 1007;
nu 1.589e-05;
kappa 2.63e-2;
phases (air water);
air
{
diameterModel isothermal;
isothermalCoeffs
{
......@@ -33,15 +27,9 @@ phase1
}
}
phase2
water
{
rho 1027;
rho0 1027;
R 1e10;
Cp 4195;
nu 3.55e-7;
kappa 0.668;
//R 1e10;
diameterModel constant;
constantCoeffs
......
......@@ -60,21 +60,21 @@ functions
outputControl outputTime;
fields
(
U1
Uair
{
mean on;
prime2Mean off;
base time;
}
U2
Uwater
{
mean on;
prime2Mean off;
base time;
}
alpha1
alphaair
{
mean on;
prime2Mean off;
......
......@@ -29,23 +29,23 @@ divSchemes
{
default none;
div(phi,alpha1) Gauss limitedLinear01 1;
div(phir,alpha1) Gauss limitedLinear01 1;
div(alphaPhi1,U1) Gauss limitedLinearV 1;
div(alphaPhi2,U2) Gauss limitedLinearV 1;
div(phi1,U1) Gauss limitedLinearV 1;
div(phi2,U2) Gauss limitedLinearV 1;
div((alpha1*Rc1)) Gauss linear;
div((alpha2*Rc2)) Gauss linear;
div(alphaPhi1,T1) Gauss limitedLinear 1;
div(alphaPhi2,T2) Gauss limitedLinear 1;
div(alphaPhi2,k) Gauss limitedLinear 1;
div(alphaPhi2,epsilon) Gauss limitedLinear 1;
div(phi,alpha) Gauss limitedLinear01 1;
div(phir,alpha) Gauss limitedLinear01 1;
div(alphaPhi,Uair) Gauss limitedLinearV 1;
div(alphaPhi,Uwater) Gauss limitedLinearV 1;
div(phiair,Uair) Gauss limitedLinearV 1;
div(phiwater,Uwater) Gauss limitedLinearV 1;
div((alphaair*Rc)) Gauss linear;
div((alphawater*Rc)) Gauss linear;
div(alphaPhi,hair) Gauss limitedLinear 1;
div(alphaPhi,hwater) Gauss limitedLinear 1;
div(alphaPhiwater,k) Gauss limitedLinear 1;
div(alphaPhiwater,epsilon) Gauss limitedLinear 1;
div(phi,Theta) Gauss limitedLinear 1;
div(phid1,p) Gauss upwind;
div(phid2,p) Gauss upwind;
div(phi1,K1) Gauss limitedLinear 1;
div(phi2,K2) Gauss limitedLinear 1;
div(phidair,p) Gauss upwind;
div(phidwater,p) Gauss upwind;
div(phiair,Kair) Gauss limitedLinear 1;
div(phiwater,Kwater) Gauss limitedLinear 1;
}
laplacianSchemes
......@@ -67,7 +67,7 @@ fluxRequired
{
default no;
p ;
alpha1 ;
alphaair ;
}
......
......@@ -47,10 +47,10 @@ solvers
relTol 0;
}
"T.*"
"h.*"
{
solver PBiCG;
preconditioner DILU;
solver PCG; //PBiCG;
preconditioner DIC; //DILU;
tolerance 1e-8;
relTol 0;
}
......@@ -105,7 +105,7 @@ relaxationFactors
equations
{
"U.*" 1;
"T.*" 1;
"h.*" 1;
"alpha.*" 1;
"Theta.*" 1;
"k.*" 1;
......
......@@ -27,7 +27,7 @@ regions
box (0 0 -0.1) (0.15 0.701 0.1);
fieldValues
(
volScalarFieldValue alpha1 0
volScalarFieldValue alphaair 0
);
}
);
......
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