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omegaSST, 3D wing validation to openFoam

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Old   March 10, 2017, 13:21
Default omegaSST, 3D wing validation to openFoam
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Matteo Biazotti
Join Date: Feb 2017
Posts: 4
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hey there, Im a bit of a newby to Openfoam, struggling to validate my results for Naca 0012 at 10deg angle of attack.
im not sure if it's a meshing or BC issue but looking at the velocity profile of the wake it seems way off.
any help will be much appreciated!!
primaraly interstead in the tip vortex
Quote:
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object k;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

#include "include/initialConditions"

dimensions [0 2 -2 0 0 0 0];

internalField uniform $turbulentKE;

boundaryField
{
#include "include/fixedInlet"

outlet
{
type inletOutlet;
inletValue $internalField;
value $internalField;
}

"wing_1.*"
{
type zeroGradient;
}

#include "include/frontBackUpperPatches"
}
Quote:
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object nut;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

dimensions [0 2 -1 0 0 0 0];

internalField uniform 0;

boundaryField
{
frontAndBack
{
type calculated;
value uniform 0;
}

inlet
{
type calculated;
value uniform 0;
}

outlet
{
type calculated;
value uniform 0;
}

lowerWall
{
type nutkWallFunction;
value uniform 0;
}

upperWall
{
type calculated;
value uniform 0;
}

"wing_1.*"
{
type nutkWallFunction;
value uniform 0;
}
}
Quote:
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object omega;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

#include "include/initialConditions"

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

internalField uniform $turbulentOmega;

boundaryField
{
#include "include/fixedInlet"

outlet
{
type inletOutlet;
inletValue $internalField;
value $internalField;
}

"wing_1.*"
{
type zeroGradient;
}

#include "include/frontBackUpperPatches"
}


// ************************************************** *********************** //
Quote:
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object p;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

#include "include/initialConditions"

dimensions [0 2 -2 0 0 0 0];

internalField uniform $pressure;

boundaryField
{
inlet
{
type zeroGradient;
}

outlet
{
type fixedValue;
value $internalField;
}

"wing_1.*"
{
type zeroGradient;
}

#include "include/frontBackUpperPatches"
}

// ************************************************** *********************** //
Quote:
version 2.0;
format ascii;
class volVectorField;
location "0";
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

#include "include/initialConditions"

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

internalField uniform $flowVelocity;

boundaryField
{
#include "include/fixedInlet"

outlet
{
type inletOutlet;
inletValue uniform (0 0 0);
value $internalField;
}

"wing_1.*"
{
type fixedValue;
value uniform (0 0 0);
}

#include "include/frontBackUpperPatches"
}


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