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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
This commit is contained in:
Kutalmis Bercin
committed by
Andrew Heather
Andrew Heather
parent
33ef139ac1
commit
14a2a8bf55
@ -0,0 +1,59 @@
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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 | Version: v1906 |
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| \\ / A nd | Web: www.OpenFOAM.com |
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| \\/ M anipulation | |
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\*---------------------------------------------------------------------------*/
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FoamFile
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{
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version 2.0;
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format ascii;
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class volVectorField;
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location "0";
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object U;
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}
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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dimensions [0 1 -1 0 0 0 0];
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internalField uniform (0 0 0);
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boundaryField
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{
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bottomWall
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{
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type fixedValue;
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value uniform (0 0 0);
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}
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topWall
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{
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type fixedValue;
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value uniform (0 0 0);
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}
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sides_half0
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{
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type cyclic;
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}
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sides_half1
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{
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type cyclic;
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}
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inlet
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{
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type turbulentDFSEMInlet;
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delta 2;
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nCellPerEddy 1;
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mapMethod nearestCell;
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value uniform (0 0 0);
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}
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outlet
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{
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type inletOutlet;
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inletValue uniform (0 0 0);
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value uniform (0 0 0);
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}
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}
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// ************************************************************************* //
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@ -0,0 +1,61 @@
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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 | Version: v1906 |
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| \\ / A nd | Web: www.OpenFOAM.com |
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| \\/ M anipulation | |
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\*---------------------------------------------------------------------------*/
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FoamFile
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{
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version 2.0;
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format ascii;
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class volVectorField;
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location "0";
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object U;
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}
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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dimensions [0 1 -1 0 0 0 0];
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internalField uniform (0 0 0);
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boundaryField
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{
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bottomWall
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{
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type fixedValue;
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value uniform (0 0 0);
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}
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topWall
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{
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type fixedValue;
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value uniform (0 0 0);
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}
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sides_half0
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{
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type cyclic;
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}
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sides_half1
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{
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type cyclic;
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}
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inlet
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{
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type turbulentDigitalFilterInlet;
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variant digitalFilter;
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planeDivisions ( 64 70 );
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L ( 0.78035508 0.31085352 0.342261 0.1728125 0.171875
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0.22459375 0.172787596 0.171889998 0.224578995 );
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patchNormalSpeed 20.133;
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value uniform (0 0 0);
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}
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outlet
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{
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type inletOutlet;
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inletValue uniform (0 0 0);
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value uniform (0 0 0);
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}
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}
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// ************************************************************************* //
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@ -0,0 +1,61 @@
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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 | Version: v1906 |
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| \\ / A nd | Web: www.OpenFOAM.com |
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| \\/ M anipulation | |
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\*---------------------------------------------------------------------------*/
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FoamFile
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{
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version 2.0;
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format ascii;
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class volVectorField;
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location "0";
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object U;
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}
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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dimensions [0 1 -1 0 0 0 0];
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internalField uniform (0 0 0);
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boundaryField
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{
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bottomWall
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{
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type fixedValue;
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value uniform (0 0 0);
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}
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topWall
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{
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type fixedValue;
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value uniform (0 0 0);
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}
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sides_half0
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{
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type cyclic;
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}
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sides_half1
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{
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type cyclic;
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}
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inlet
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{
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type turbulentDigitalFilterInlet;
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variant reducedDigitalFilter;
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planeDivisions ( 64 70 );
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L ( 0.78035508 0.31085352 0.342261 0.1728125 0.171875
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0.22459375 0.172787596 0.171889998 0.224578995 );
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patchNormalSpeed 20.133;
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value uniform (0 0 0);
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}
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outlet
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{
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type inletOutlet;
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inletValue uniform (0 0 0);
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value uniform (0 0 0);
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}
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}
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// ************************************************************************* //
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@ -0,0 +1,53 @@
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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 | Version: v1906 |
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| \\ / A nd | Web: www.OpenFOAM.com |
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| \\/ M anipulation | |
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\*---------------------------------------------------------------------------*/
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FoamFile
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{
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version 2.0;
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format ascii;
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class volScalarField;
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location "0";
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object nut;
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}
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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dimensions [0 2 -1 0 0 0 0];
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internalField uniform 0;
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boundaryField
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{
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bottomWall
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{
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type zeroGradient;
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}
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topWall
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{
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type zeroGradient;
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}
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sides_half0
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{
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type cyclic;
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}
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sides_half1
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{
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type cyclic;
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}
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inlet
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{
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type calculated;
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value uniform 1e-08;
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}
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outlet
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{
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type calculated;
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value uniform 1e-08;
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}
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}
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// ************************************************************************* //
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52
tutorials/verificationAndValidation/turbulentInflow/0.orig/p
Normal file
52
tutorials/verificationAndValidation/turbulentInflow/0.orig/p
Normal file
@ -0,0 +1,52 @@
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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 | Version: v1906 |
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||||
| \\ / A nd | Web: www.OpenFOAM.com |
|
||||
| \\/ M anipulation | |
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||||
\*---------------------------------------------------------------------------*/
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FoamFile
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{
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version 2.0;
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format ascii;
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class volScalarField;
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location "0";
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object p;
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}
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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dimensions [0 2 -2 0 0 0 0];
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internalField uniform 0;
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boundaryField
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{
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bottomWall
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{
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type zeroGradient;
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}
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topWall
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{
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type zeroGradient;
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}
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sides_half0
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{
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type cyclic;
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}
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sides_half1
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{
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type cyclic;
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}
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inlet
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{
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type zeroGradient;
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}
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outlet
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{
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type fixedValue;
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value uniform 0;
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}
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}
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// ************************************************************************* //
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