| Mash |
March 10, 2017 12:21 |
omegaSST, 3D wing validation to openFoam
2 Attachment(s)
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
Code:
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"
}
Code:
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;
}
}
Code:
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"
}
// ************************************************************************* //
Code:
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"
}
// ************************************************************************* //
Code:
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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