
[Sponsors] 
May 24, 2011, 22:11 
Calculating Lift and Drag in Paraview (paraFoam)

#1 
Member
Scott
Join Date: Sep 2009
Posts: 41
Rep Power: 10 
Hi there,
I have a body that I wish to extract the lift and drag forces for in Paraview. I assume that this can be achieved using the calculator but I cannot work it out. Could someone please give me some pointers on this. Basically I need to calculate the normals for each surface, then find the pressure on each surface in the components of X (or Y or Z, depending on if it is Drag, Lift or side force), then intergrate these values for the whole body to get the Force value. If someone has a procedure for something like this then please let me know! Thanks for your help, Scott 

May 25, 2011, 02:49 

#2 
Member
Scott
Join Date: Sep 2009
Posts: 41
Rep Power: 10 
I found a solution:
Extract Surfaces Generate Surface Normals Use the calculator to multiply pressure by the surface normals (Normals*p) This then prints the values in the data tab at the right in three columns, one for each normal direction. I then integrate these to get total forces on the area using Integrate Variables. Let me know if you see any problems with this approach! Cheers, Scott 

July 18, 2011, 15:17 

#3 
New Member
Join Date: Aug 2010
Posts: 15
Rep Power: 9 
Hey Scott,
I am trying to do the same thing and am attempting your approach. I was just wondering if you've made any more progress since you posted. I'd like to collaborate with you if possible. 

July 18, 2011, 17:33 

#4 
New Member
Join Date: Aug 2010
Posts: 15
Rep Power: 9 
Scott,
Where (and how) do you calculate the area of each panel? I'm struggling finding a particularly good way of doing this. Right now I'm performing a similar calculation in Fortran, but I would prefer to do this in paraview. 

September 12, 2011, 10:28 

#5 
Member
Daniel
Join Date: Apr 2010
Location: Manchester
Posts: 31
Rep Power: 9 
Any advances on this? Also, how would you go about including the effect of skin friction? I guess the wallShearStress postpro function would be a start.


January 3, 2014, 04:19 
lift and drag coeffs in paraview

#6 
Member

Hi
How can I calculate lift and drag coefficient in paraview? I've run an oscillating airfoil with pitching motion.I've calculated lift and drag coefficient through libforces in controlDict, but the values are wrong. I want to calculate them in paraview and plot them over the time or angle. Please tell me how to do this? 

March 27, 2014, 12:38 

#7 
Senior Member

In 2D, you might want to try something like this in paraview on the surfaces you want to evaluate,
1. filter: generate surface normals (disable splitting, activate compute cell normals) 2. filter: calculator using something like this for moments : Normals_Y*p*yourDensity*(yourCoRx16) + Normals_X*p*yourDensity*(yourCoRycoordsY) replacing yourDensity and yourCoR* by appropriate values or simplify it to get forces 3. filter: integrate variables and look for the results of the integration in the table that appears in the end this procedure gives you sum_cells(P*rho*A*norm_y) I think this can be easily adapted to 3D. cheers 

April 16, 2014, 07:13 

#8 
Member
Daniel
Join Date: Apr 2010
Location: Manchester
Posts: 31
Rep Power: 9 
I've had some success working with cell data (as opposed to point data) on 3D surface meshes, if it's of use:
Cell area can be obtained using the Mesh Quality filter and the Area option. Use the Point Data to Cell Data on your pressure data. Then use Generate Surface Normals (may need to Extract Surface first) with the Compute Cell Nomals option enabled. Pop these into a calculator using the Cell Data mode and that should have you on the right track for the pressure side of things. 

February 12, 2016, 08:58 

#9 
New Member
Join Date: Jan 2016
Posts: 3
Rep Power: 3 
Hello louisgag, could you please explain what do you mean by "yourCoR"?
Thank you very much. 

February 12, 2016, 08:59 

#10 
Senior Member

Center of Rotation
Regards, Louis 

February 12, 2016, 09:00 

#11 
New Member
Join Date: Jan 2016
Posts: 3
Rep Power: 3 

February 12, 2016, 09:07 

#12 
New Member
Join Date: Jan 2016
Posts: 3
Rep Power: 3 
Thank you for your quick reply.
Another question if you don't mind, So, If my center of rotation is (0,0,0), Does this mean that CoRx=0, and CoRy=0? Sorry if the question is too simple, I am new to CFD. 

February 12, 2016, 09:10 

#13 
Senior Member

Yes, that is correct.
Louis 

October 24, 2016, 06:50 

#14  
Member
Emre
Join Date: Nov 2015
Location: Izmir, Turkey
Posts: 47
Rep Power: 3 
Quote:


November 18, 2016, 10:20 

#15  
New Member
bruce
Join Date: May 2012
Posts: 12
Rep Power: 7 
Quote:
May I ask why it's 16 in your equation: Normals_Y*p*yourDensity*(yourCoRx16) + Normals_X*p*yourDensity*(yourCoRycoordsY) ? Another quenstion is about the center of rotation in paraView. My understanding is that the center of the geometry will be the center of rotation. please correct me if I am wrong. It will be very appreciated if you can indicate how to get or display the coordinates of the center of rotation. Thank you very much in advance! 

November 18, 2016, 10:42 

#16 
Senior Member

Hi Bruce,
I'm pretty sure that's a typo, and should read "coordsX" thanks for noting it I'll correct it. Regards, Louis 

November 18, 2016, 22:34 

#17 
New Member
bruce
Join Date: May 2012
Posts: 12
Rep Power: 7 
Hi Louis,
Thank you very much for your prompt reply. It's clear now. By the way, I found a way to get the center of rotation: simply click the Probe Location button in the tool bar and the 'Center' followed by three values in the Properties tab would be the Center of Rotation used in the equation. If you cannot find the Probe Location button in your tool bar, go to the main menu, then Fliters>Data Analysis>Probe Location, you will get the same thing. This may be very redundant for experienced ParaView user, but I think it should be helpful for newbie of ParaView, like me. Cheers, Bruce 

December 24, 2016, 06:34 
Mesh Quality working?

#18 
New Member
Join Date: Sep 2014
Posts: 5
Rep Power: 5 
I'm trying to apply the methods in this thread to 3D data from a car inside a "wind tunnel" but I have some questions. My coordinate system is Z in the direction of flow, Y up and X is the right hand vector when facing the flow.
 Wouldn't the drag force in Newtons be given by p*cell area*Normals_Z? I see that density is being suggested in the formula but I don't understand why, isn't force equal to pressure times area?  I have tried using the Mesh Quality filter to get the area of a surface in a cell, but this doesn't seem to be giving me the result I expected. Here's my setup: Capture.PNG In case the snapshot doesn't work, in text form, my filters are: 1. Simulation Run Data coming from OpenFOAM 2. ExtractSurface 3. GenerateSurfaceNormals (Splitting disabled, Filed Association=Cell Data) 4. ExtractCellsByRegion (to only extract faces of the object in the wind tunnel, not the boundaries of the computation, i.e. not the wind tunnel walls) 5. Mesh Quality (Triangle Quality Measure=Area, Quad Quality Measure=Area, Filed Association=Cell Data). This adds a Quality column to the data set which I would have expected to be the area of the triangle or quad in the cell 6. Calculator with formula p*Quality*Normals_Z (Attribute Mode=Cell Data) 7. IntegrateVariables (Field Association=Cell Data) The result of the integration is incorrect. If I look at the integration of Quality, I would have expected to find the total area of the object but it gives me 0.0716 for a car, way too low. As if just to nag me, on top of that the IntegrateVariables added a column named Area (I don't know why and how this appears) and that area seems perfectly reasonable at 27 m2 for a car, so somehow it managed to calculate this for me. Any idea of what is going wrong with the Mesh Quality filter? Has anybody had any luck computing all forces in Newtons? I'm so close... 

December 26, 2016, 05:41 
Figured it out

#19 
New Member
Join Date: Sep 2014
Posts: 5
Rep Power: 5 
My mistake.
For some reason I thought the Integrate Variables filter was only doing the sum of all rows, when instead it multiplies each row by the measure of the cell, which is the surface area in my case, when summing. So the Mesh Quality filter is unnecessary, and the formula p*Normals_Z is all that is needed in the Calculator before integrating which will multiply by the area of each cell under the hood. One can easily see the Integration multiplying by the surface by modifying the formula in the calculator to be 1 (constant). The integration of 1 gives the total area, not the number of cells. Just a noob error on my part. 

January 9, 2017, 09:22 

#20 
Senior Member

Hi kubashmuba,
Thanks for posting the answer to your question, it might help other people. Depending on the solver you use, the "pressure" that OpenFOAM returns may actually be pressure divided by density (I think this holds for every incompressible flow solver in OF). Thus, the density multiplier. Regards, Louis 

Thread Tools  
Display Modes  


Similar Threads  
Thread  Thread Starter  Forum  Replies  Last Post 
calculating drag and lift in fluent  morteza08  FLUENT  4  December 13, 2012 16:34 
Reference Area for Calculating Lift and Drag Coefficient of 3D wing  mahbub03  Main CFD Forum  3  May 19, 2011 00:21 
Lift and Drag Monitor Point Values Converging to Zero  Josh  CFX  24  May 9, 2011 10:38 
Correct lift but wrong pressure drag  possible?  zx  Main CFD Forum  4  July 27, 2007 23:38 
Fluid mechanics / drag & lift  Jamcam  Main CFD Forum  0  October 31, 2002 05:39 