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Simplified Runscript #4

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17fac0d
Added RAE2822_Airfoil_HISA to validations
nmadison11 Nov 19, 2025
f1117df
Simplified Runscript
nmadison11 Dec 4, 2025
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49 changes: 49 additions & 0 deletions RAE2822_Airfoil_HISA/0_orig/T
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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object T;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
#include "include/freestreamConditions"
dimensions [0 0 0 1 0 0 0];

internalField uniform $T;

boundaryField
{
"wing.*"
{
type characteristicWallTemperature;
value $internalField;
}
symmetry1
{
type symmetry;
}
symmetry2
{
type symmetry;
}
inout
{
type characteristicFarfieldTemperature;
#include "include/freestreamConditions"
value $internalField;
//type inletOutlet;
//inletValue $internalField;
//value $internalField;
}
}


// ************************************************************************* //
51 changes: 51 additions & 0 deletions RAE2822_Airfoil_HISA/0_orig/U
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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volVectorField;
location "0";
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

#include "include/freestreamConditions"

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

internalField uniform $U;

boundaryField
{
"wing.*"
{
type boundaryCorrectedFixedValue;
value uniform (0 0 0);
}
symmetry1
{
type symmetry;
}
symmetry2
{
type symmetry;
}
inout
{
type characteristicFarfieldVelocity;
#include "include/freestreamConditions"
value uniform (0 0 0);
//type inletOutlet;
//inletValue $internalField;
//value $internalField;
}
}


// ************************************************************************* //
45 changes: 45 additions & 0 deletions RAE2822_Airfoil_HISA/0_orig/alphat
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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object alphat;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

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

internalField uniform 0;

boundaryField
{
"wing.*"
{
type boundaryCorrectedFixedValue;
value uniform 0;
}
symmetry1
{
type symmetry;
}
symmetry2
{
type symmetry;
}
inout
{
type calculated;
value $internalField;
}
}


// ************************************************************************* //
14 changes: 14 additions & 0 deletions RAE2822_Airfoil_HISA/0_orig/include/freestreamConditions
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/*--------------------------------*- C++ -*----------------------------------*\
| |
| HiSA: High Speed Aerodynamic solver |
| Copyright (C) 2014-2017 Johan Heyns - CSIR, South Africa |
| Copyright (C) 2014-2017 Oliver Oxtoby - CSIR, South Africa |
| |
\*---------------------------------------------------------------------------*/

U (233.603 0 0);
p 108988.0;
T 255.56;
#inputMode merge

// ************************************************************************* //
46 changes: 46 additions & 0 deletions RAE2822_Airfoil_HISA/0_orig/nuTilda
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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object nuTilda;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

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

internalField uniform 4.5e-05;

boundaryField
{
"wing.*"
{
type boundaryCorrectedFixedValue;
value uniform 0.0;
}
symmetry1
{
type symmetry;
}
symmetry2
{
type symmetry;
}
inout
{
type inletOutlet;
inletValue $internalField;
value $internalField;
}
}


// ************************************************************************* //
46 changes: 46 additions & 0 deletions RAE2822_Airfoil_HISA/0_orig/nut
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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object nut;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

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

internalField uniform 0;

boundaryField
{
"wing.*"
{
type boundaryCorrectedNutLowReWallFunction;
value uniform 0;
}
symmetry1
{
type symmetry;
}
symmetry2
{
type symmetry;
}
inout
{
type calculated;
value $internalField;
}

}


// ************************************************************************* //
51 changes: 51 additions & 0 deletions RAE2822_Airfoil_HISA/0_orig/p
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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object p;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
#include "include/freestreamConditions"

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

internalField uniform $p;

boundaryField
{
"wing.*"
{
type characteristicWallPressure;
value $internalField;
}
symmetry1
{
type symmetry;
}
symmetry2
{
type symmetry;
}
inout
{
type characteristicFarfieldPressure;
#include "include/freestreamConditions"
value $internalField;

//type outletInlet;
//outletValue $internalField;
//value $internalField;
}
}


// ************************************************************************* //
24 changes: 24 additions & 0 deletions RAE2822_Airfoil_HISA/Allclean.sh
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#!/bin/bash

while true
do
read -p "Delete everything and resume to the default setup (y/n)?" yn
case $yn in
[Yy]* )
# clean everyting
echo "Cleaning..."
rm -rf 0
rm -rf postProcessing
rm -rf constant/extendedFeatureEdgeMesh
rm -rf constant/triSurface
rm -rf constant/polyMesh/
rm -rf *.bin *.info *.dat *.xyz *.stl *.txt
rm -rf processor* 0.0000*
rm -rf {1..9}*
exit
;;
[Nn]* ) exit;;
* ) echo "Please answer yes or no.";;
esac
done

50 changes: 50 additions & 0 deletions RAE2822_Airfoil_HISA/constant/thermophysicalProperties
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/*--------------------------------*- C++ -*----------------------------------*\
| |
| HiSA: High Speed Aerodynamic solver |
| Copyright (C) 2014-2017 Johan Heyns - CSIR, South Africa |
| Copyright (C) 2014-2017 Oliver Oxtoby - CSIR, South Africa |
| |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object thermophysicalProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

thermoType
{
type hePsiThermo;
mixture pureMixture;
transport const;
thermo hConst;
equationOfState perfectGas;
specie specie;
energy sensibleInternalEnergy;
}


mixture
{
specie
{
nMoles 1;
molWeight 28.966;
}
thermodynamics
{
Cp 1005;
Hf 0;
}
transport
{
mu 1.8e-5;
Pr 0.700000;
TRef 300.000000;
}
}

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