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LiftDrag Utility for Compressible Flow Fields

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Old   January 11, 2008, 01:55
Default Hello, has anyone have a modif
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Shaun Darmody
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Hello, has anyone have a modified liftDrag utility for use with the compressible flow solvers such as rhopSonicFoam?

I note that the incompressible version uses nu and not mu. My C++ is not up to scratch. Any assistance would be appreciated.

Thanks

Shaun.D
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Old   January 14, 2008, 08:24
Default Hello Shaun, Yes, I have mo
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Ivan Bychkov
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Hello Shaun,

Yes, I have modified liftDrag.

An enhanced version of liftDrag has the next features:
- support incompressible and compressible solvers (Euler equations, laminar, turbulent);
- user can specify drag force direction and reference values;
- forces and moments (not coefficients) printed when the option dimensioned is specified.

You can download it from this:
http://mmpp.110mb.com/OpenFOAM/liftDragTool.tar.gz

Be careful the new version overwrite old liftDrag files.

I also want to upload it to svn. Does anyone known Do I need registration on svn to upload files?

Ivan
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Old   January 14, 2008, 22:53
Default Hello Ivan, Thanks for repl
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Shaun Darmody
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Hello Ivan,

Thanks for replying and thank you for the updated tool.

I am not sure about the registration process.

Regards

Shaun.D
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Old   March 25, 2008, 14:25
Default Hi Ivan, thanks for sharing
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Laurence Griffiths
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Hi Ivan,

thanks for sharing the updated liftdrag tool.

I was just wondering what you've taken as the moment origin?

thanks,
Laurence
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Old   March 25, 2008, 17:34
Default Hello Laurence, The moment
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Ivan Bychkov
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Hello Laurence,

The moment origin is the origin of the coordinate system. The same as in earlier liftDrag.

I also found that reference density, velocity and others reference values can be computed incorrectly for compressible flow. So you can use the option -dimensionless or manually set reference values for compressible flow.

Ivan
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Old   April 18, 2008, 02:34
Default Hi Ivan, I'm a newbie at wr
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Simon Vun
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Hi Ivan,

I'm a newbie at writing C++ code so forgive me if this is an obvious question but I was looking through the liftDrag utility you modified and was wondering how the "dragCoefficient" variable in incompressible.H finds the turbulent drag coefficient in liftDrag.H in the src/... folder. Why don't we have to change the "dragCoefficent" in the incompressible.H file to "turbDragCoefficient" to get the drag coefficient that includes turbulent effects?

Thanks,

Simon.
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Old   July 15, 2008, 12:24
Default Hey, I was stumbling over t
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Hey,

I was stumbling over the same thing. Any clues yet? I'm sure the turbLift/DragCoefficient function is never called...
I'll try fixing it, but don't know if I'll succeed.

My problem is that I have no idea how to find out which turbulence model is used, which is needed for the turbLiftCoefficient function as the first argument:
const autoPtr<turbulencemodel>& turbulence

And if you want to make this a smooth function, you have to find out automatically in advance whether it's a turbulent or laminar simulation, and which model is used.

Cheers,

Axel
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Old   July 16, 2008, 08:53
Default Looking at the latest 1.5 rele
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Gregor Veble
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Looking at the latest 1.5 release, it seems the liftDrag utility is obsolete now, there is a new force postprocessor in 1.5. I haven't tested it yet but it might be just what you are looking for.
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Old   July 17, 2008, 00:18
Default I followed the instructions fo
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Anant Grewal
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I followed the instructions for installing the enhanced version of the liftDrag utility on OF 1.4.1-dev, but got the following error when running wmake:

liftDrag.C: In function 'int main(int, char**)':
liftDrag.C:89: error: no match for 'operator=' in 'nu = transportProperties.Foam::IOdictionary::<anonymous >.Foam::dictionary::lookup(((c onst Foam::word&)(& Foam::word(((const char*)"nu")))))'

Any ideas?
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Old   September 16, 2008, 06:36
Default Hello Friends http://www.cfd-o
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Mahendra
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Hello Friends

I am curious to know how to get the values of lift and drag coefficients from log file for flow across a cylinder case in OpenFOam 1.5?
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