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New densitybased solver AeroFoam

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Old   November 3, 2009, 17:18
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Is this AeroFoam for v1.5 available yet ? If so where can I find it ?
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Old   November 16, 2009, 06:22
Default rhoCentralFoam
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There is this code rhoCentralFoam, how does it differ from the newer AeroFoam?
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Old   May 26, 2010, 11:09
Default AeroFoam for OpenFoam 1.6
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Hi all,

Is AeroFoam available for OpenFoam 1.6. If so where can i download the source code.

thanks
mecbe
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Old   July 3, 2010, 06:47
Default Aerofoam for OpenFoam 1.6
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Gabriel D
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hello everybody,

i just wanted to know if AeroFoam is available for OF 1.6 .
thank you
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Old   July 3, 2010, 07:05
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Unfortunately No.

Thanks
mecbe
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Old   October 3, 2010, 20:48
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Quote:
Originally Posted by Julian K. View Post
That sounds very good! Thanks Giulio!
Hello,

Is it there any version of Aerofoam for OpenFoam 1.7.1?

Regards,
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Old   October 14, 2010, 08:47
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Hi all, i would like to use the 3D toolbox to make a movie of the AGARD wing of the tutorial. I have it activated, but i do not know how to use it.

Can someone tell me please?

Thanks a lot!

Marta
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Old   October 14, 2010, 08:53
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Dear all, i am trying to run the AGARD wing tutorial, but I do not know how to make the movie i saw on the website.
I have already activated the 3D toolbox and data are saved correctly, so everything is fine with the run.

Thanks a lot,

Marta
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Old   October 20, 2010, 02:59
Default Problem regarding adding another monoflux scheme in Aerofoam
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Hi Guilo,

I am trying to add a new monoflux scheme (KFVS) similar to that of AUSM, Roe fluxes, etc.,. I have made correction to include the file in header for Aerofoam.C (#include KFVSFlux.C) file and called successfully from build_fluxes.C, I got no compilation errors when I ran wmake in the AeroFoam folder through Terminal.

But when I use the scheme to run a test case it gives the following error.

Does everything look fine? [y] to continue [n] otherwise y

Starting time loop...

#0 Foam::error:: printStack(Foam::Ostream&) in "/home/xx/OpenFOAM/OpenFOAM-1.4.1/lib/linuxGccDPOpt/libOpenFOAM.so"
#1 Foam::sigFpe::sigFpeHandler(int) in "/home/xx/OpenFOAM/OpenFOAM-1.4.1/lib/linuxGccDPOpt/libOpenFOAM.so"
#2 Uninterpreted: [0x997400]
#3 kfvs_flux(double, double, double, Foam::Vector<double>, Foam::Vector<double>, double, double, Foam::Vector<double>, double*, Foam::Vector<double>*, double*, double) in "/home/madhu/OpenFOAM/OpenFOAM-1.4.1/applications/bin/linuxGccDPOpt/AeroFoam"
#4 build_fluxes(Foam::Field<double>*, Foam::word, Foam::dimensioned<double>*, Foam::dimensioned<double>*, Foam::dimensioned<double>*, Foam::fvMesh*, Foam::Field<int>*, Foam::Field<int>*, Foam::GeometricField<double, Foam::fvPatchField, Foam::volMesh>*, Foam::GeometricField<Foam::Vector<double>, Foam::fvPatchField, Foam::volMesh>*, Foam::GeometricField<double, Foam::fvPatchField, Foam::volMesh>*, Foam::GeometricField<double, Foam::fvPatchField, Foam::volMesh>*, Foam::GeometricField<Foam::Vector<double>, Foam::fvPatchField, Foam::volMesh>*, Foam::GeometricField<double, Foam::fvPatchField, Foam::volMesh>*, Foam::GeometricField<Foam::Vector<double>, Foam::fvPatchField, Foam::volMesh>*, Foam::GeometricField<Foam::Vector<double>, Foam::fvPatchField, Foam::volMesh>*, Foam::GeometricField<Foam::Vector<double>, Foam::fvPatchField, Foam::volMesh>*, Foam::GeometricField<Foam::Vector<double>, Foam::fvPatchField, Foam::volMesh>*, Foam::GeometricField<double, Foam::fvsPatchField, Foam::surfaceMesh>* at Foam::GeometricField<Foam::Vector<double>, Foam::fvsPatchField, Foam::surfaceMesh>*, Foam::GeometricField<double, Foam::fvsPatchField, Foam::surfaceMesh>*, Foam::word, Foam::word, Foam::word, Foam::word, double)
#5 main in "/home/xx/OpenFOAM/OpenFOAM-1.4.1/applications/bin/linuxGccDPOpt/AeroFoam"
#6 __libc_start_main in "/lib/tls/i686/cmov/libc.so.6"
#7 _start at /build/buildd/eglibc-2.10.1/csu/../sysdeps/i386/elf/start.S:122
Floating point exception


Do I need to make changes in other places to incorporate the file.

Thanks in advance,
Eeshwar.
Last edited by eeshwar; October 20, 2010 at 04:44.
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Old   December 25, 2010, 09:42
Arrow AeroFoam
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Dear all,
Any body have updated AeroFoam solver which works on Open Foam 1.6 or higher version? Please reply...
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Old   December 26, 2010, 10:35
Default run open foam
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hi
I new user open foam and can generate mesh but I can't run it
please help me.
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Old   December 26, 2010, 11:50
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Hi Iman,
Explain how you generated mesh in OpenFOAM. If you generated with Mesh Conversion utilities , please go through the following link http://www.afs.enea.it/funel/CFD/Ope...shconvtest.htm and user guide .
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Old   December 31, 2010, 10:39
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dear Rock.Senthil Kumar
Its good
thanks for help you
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Old   February 4, 2011, 22:53
Default new version of AeroFOAM for OpenFOAM 1.7.1
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AeroFoam-1.7-part1.zip

AeroFoam-1.7-part2.zip

enjoy~! this is not my contribution, but I hope it is helpful!
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Old   April 1, 2011, 02:39
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This is really helpful and I hope work continues in this area of OpenFOAM.
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Old   April 1, 2011, 07:44
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Thanks Solarberiden.

Is it not your contribution? I am sure that you contributed posting here...
Do you know the author of the codes? Or a URL where it is located?
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Old   April 6, 2011, 03:49
Exclamation Problem with Aerofoam for OF1.7.1
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Hello everybody,

I'm trying to use the solver AeroFoam with the 1.7.1 version of OF; it's part of an important project for my study. I downloaded the Aerofoam files at :
https://sourceforge.net/projects/aerofoam/files/Source/
And now I want to test this solver with a tutorial case : the oblique shock.
However, (after 'BlockMesh'), when I launch AeroFoam, I have :

-------------------------------------------------------------

// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
Create time

Create mesh for time = 0

========================================
Reading Thermodynamic Properties...
========================================
gamma [-] = 1.4
Pr [-] = 0.72
R [J/KgK] = 287.05
Cp [J/KgK] = 717.625
Cv [J/KgK] = 1004.67
----------------------------------------

========================================
Reading Initial Conditions...
========================================
Reading field p
Reading field T
Reading field U
----------------------------------------
Creating conservative variables at t^(k)
Creating conservative variables at t^(k-1)
Creating conservative variables at t^(k-2)
Creating conservative variables fluxes at t^(k)
Creating primitive variables gradient fields (optional)
----------------------------------------

========================================
Creating Mesh Connectivity...
========================================
Using adaptive algorithm...
id_LL_i7290SIZE3510Loop on Internal Faces...
i=0i=1i=2i=3i=4i=5i=6i=7i=8i=9i=10i=11i=1
until i=3509
Loop on Boundary Faces...
----------------------------------------

========================================
Mesh
========================================
# of Faces = 3510
# of Cells = 1800
# of BndPatch = 5
0) inlet @ top
1) supersonicInlet @ inlet
2) extrapolatedOutlet @ outlet
3) symmetryPlane @ bottom
4) empty @ frontAndBack
----------------------------------------

========================================
Numerical Scheme
========================================
flowType = Euler
timeScheme = RK2
CourantMax = 0.1
CourantSteps = 25
MonotoneFlux = Roe
HighResFlux = LW
fluxLimiter = VL
entropyFix = HH2
extrapolateBC = 1
residualNorm = L1
minResidual = -1
----------------------------------------
Does everything look fine? [y] to continue [n] otherwise

-------------------------------------------------------------
I type yes and get :

-------------------------------------------------------------
blf fx i=1
...
blf fx i=3509
#0 Foam::error:rintStack(Foam::Ostream&) in "/opt/openfoam171/lib/linux64GccDPOpt/libOpenFOAM.so"
#1 Foam::sigSegv::sigSegvHandler(int) in "/opt/openfoam171/lib/linux64GccDPOpt/libOpenFOAM.so"
#2 in "/lib/libc.so.6"
#3
at Foam::GeometricField<Foam::Vector<double>, Foam::fvsPatchField, Foam::surfaceMesh>*, Foam::GeometricField<double, Foam::fvsPatchField, Foam::surfaceMesh>*, Foam::word, Foam::word, Foam::word, Foam::word, double)
#4
in "/home/emilie/OpenFOAM/bruno-1.7.1/applications/bin/linux64GccDPOpt/AeroFoam"
#5 __libc_start_main in "/lib/libc.so.6"
#6
in "/home/emilie/OpenFOAM/bruno-1.7.1/applications/bin/linux64GccDPOpt/AeroFoam"
Segmentation fault

-------------------------------------------------------------

Does anyone has an idea why I have this error ?

Thank you very much for your help !

Emilie
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Old   May 31, 2011, 01:44
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is there any version can run in parallel？
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Old   June 17, 2011, 03:35
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could you please rebuild your openfoam in debug mode and repost the error message? The final error message you posted didn't bring forwards any location about the error position information, which is a little bit difficult for other "depanner" , LOL.
by the way, the author of the version you are using and downloading from sourceforge JLight2010 had mentioned that
http://www.cfd-online.com/Forums/ope...free-code.html
he is not sure about the code correctness, further discuss would be depending your reply, I have tried some examples including the OneraM6 case and YF-17 case.
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Old   June 17, 2011, 03:48
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Quote:
Originally Posted by abhi View Post
Thats a gre8 news. I was waiting this to happen.
Thanks a lot Giulio.
Is turbulence also available in this version ?
Finally, till now it didn't happen, the parallel version
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