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Modified the motorBike tutorial, getting very high drag |
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October 23, 2012, 06:37 |
Modified the motorBike tutorial, getting very high drag
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#1 |
Member
Ben
Join Date: Sep 2012
Posts: 40
Rep Power: 14 |
I wanted to test the drag on a car design that I had made so from the help of the users of this forum I managed to replace the motorbike with the car in the wind tunnel.
I opened the forceCoefs.dat file to view my drag coefficients, there was a huge list of very big numbers up to about 2000 and the minimum being about 1000, this was the same for lift and down force also.I forces { type forceCoeffs; functionObjectLibs ( "libforces.so" ); outputControl timeStep; outputInterval 1; patches ( "motorBike.*" ); pName p; UName U; rhoName rhoInf; // Indicates incompressible log true; rhoInf 1; // Redundant for incompressible liftDir (0 0 1); dragDir (1 0 0); CofR (0.72 0 0); // Axle midpoint on ground pitchAxis (0 1 0); magUInf 20; lRef 1.42; // Wheelbase length Aref 0.75; // Estimated <- EDIT: changed this to 100.75 and am suddenly getting lower drag coefficients, they are still very high but getting numbers like 19.0 } Please could you tell me how to fix this problem, I know the drag coefficient should only be around 0.2 but I am getting numbers up to about 5000 now. EDIT: So after changing the area I notice I am getting better results, so I am guessing I need to find the estimated area of my car to get any good results, does anyone know how I can do this through OpenFOAM or paraView, and also when it says area does it mean frontal area? Thank you Last edited by ben1793; October 24, 2012 at 12:44. |
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October 23, 2012, 09:03 |
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#2 |
Senior Member
Join Date: Aug 2010
Location: Groningen, The Netherlands
Posts: 216
Rep Power: 19 |
Dear Ben,
indeed the reference area is important and has to be correct! However take care that there are "several" reference areas possible: the cross-section of the car or the "wetted surface" which is for single flow basically the whole surface. From my experience in two phase flows the wetted surface is used (e.g. ship resistance) and for single phase flows the cross-section is used (e.g. flow around a NACA profile) I'm not sure whether there are exceptions of that rule and which one is valid for your case, but I guess google will help you ;-) regards |
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October 23, 2012, 10:09 |
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#3 |
Senior Member
Anonymous
Join Date: Dec 2011
Location: USA
Posts: 108
Rep Power: 15 |
You can get the cross-sectional area through paraview. Google it and you will find it. I recommend just using your CAD software however because it is easier.
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August 13, 2013, 15:36 |
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#4 | |
Senior Member
saeideh mohamadi
Join Date: Aug 2012
Posts: 229
Rep Power: 15 |
Quote:
Dear Plucas, would you please explain more that how can we get the cross-sectional area through paraview? Thank you very much. |
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August 16, 2013, 03:25 |
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#5 |
Senior Member
Nima Samkhaniani
Join Date: Sep 2009
Location: Tehran, Iran
Posts: 1,267
Blog Entries: 1
Rep Power: 25 |
one rough way, i guess, you can create an slice, then you can saw in information tab box boundness
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