wall shear stress
Hello everyone
I want to plot wall shear stress contours and I did it by using"wallShearStress" command but it does not give me the right amount of that and it is some how irrelevant. I have also read this page http://www.cfd-online.com/Forums/ope...bend-pipe.html but I did not get what to do ,is there any idea? |
there is no idea?
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no one is interested in this topic?
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Greetings Ali Reza,
In the next few paragraphs I'll be going on a rant, because, well... it has been hard to get the time to help people on the forum and then I stumble on this kind of thread and it makes me feel like I should find better things to do in life. Therefore, if you don't want to read what I've written below, I strongly suggest you read instead the instructions given on this thread: http://www.cfd-online.com/Forums/ope...-get-help.html ------------------ Ready? Commencing ranting: Quote:
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You know, I and many people that use this forum have got plenty of ideas, but usually nobody has 20h to write every possible idea on how you could solve the problem :( In my case, pretty much because I have not understood what the problem was, since you did not clearly state what the problem is. Quote:
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Let me try to put this into a perspective to try and explain it to you, so that perhaps you can understand why I'm ranting. I like helping people here on the forum, because:
This to say that a few years ago every day I was able to come to the forums for an hour or two, and help a little few people every day. Nowadays it's a matter of great luck that I'm able to spend 2-4h per weekend to try and help a few people. ... and now I'm getting tired of ranting... yes, I'm getting that old :rolleyes:... OK, so to sum it up: with luck, I'll be able to answer your next post next Saturday, 6 days from now. And I can only hope that you will provide more than enough information in order to help you. If you do not provide enough information, that will mean that I will have to write every single detail I need to know from your case in order for me to be able to help you... and only 7 days from then will I be able to look at your answer with all of the necessary information. In other words:
End of rant. --------------- Best regards, Bruno PS: I wasn't very helpful on this post, I know, but unfortunately you did not provide enough information in order to help you :( |
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thanks for your complete analysis and remebering me to poste in the right way.:);)
I feel so good after reading your post,it was useful . ok. I am going to give the the whole things about this case.I have simulated,laminar,incompressible,newotoinian and transient flow in a pipe which is shown in the picture. I have got different contours like velocity maginitude and pressure,all of them show what I have expected to see but the wall shear stress contours were not in this way. the wall shear stress contours shoul be the same as which has been shown in picture2. As I said before,I think there some thing wrong between what I need and what openfoam shows,is that right? what should I do? inlet velocity profile is u=0.15-0.15cos(2.5pi*t) and nu is defined as =3.78e-6 source codes are here Code:
/*---------------------------------------------------------------------------*\ do you agree with that? |
Hi Ali,
My guess is that you did not take into account the fact that the wallShearStress utility will give you the results in the same units of the pressure field: http://www.cfd-online.com/Wiki/Wall_shear_stress Which for incompressible flow, in OpenFOAM, it usually is in "kinematic pressure", namely in "m2/s2". In post #46 of the other thread you pointed out, you'll find this comment: Quote:
Best regards, Bruno |
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I know "wallShearStress" utility will show the xyz components of wall shear stress. I want to show the skin friction coefficient (cf=tauw/(0.5*rho*U^2) around a circular cylinder, so which component of wall shear stress is the tauw or how to calculate it? |
Greetings killsecond,
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Oh, wait... you want to know what "tauw" is in fact from the wall shear stress vector? But what you want is the skin friction on the surface of a cylinder... you're referring to this: http://www.cfd-online.com/Wiki/Skin_...on_coefficient Honestly, I have no idea. My best guess is that you use the magnitude of the wall shear stress. This is a generic Fluid Dynamics question, so I suggest that you ask on the main CFD forum: http://www.cfd-online.com/Forums/main/ Best regards, Bruno |
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Thank you for your advices, I will try them. |
Same subject, different issue?
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Hi,
I have a case study in which I make use of simpleFoam to find the steady-state flow solution inside a microfluidic channel. I am attaching a print screen of the (obtained) flow velocity (magnitude to the left and vector to the right). Then, as according to many suggestions and the guide itself, I want to calculate the wall shear stress by running: Code:
simpleFoam -postProcess -func wallShearStress Code:
Create time Code:
dimensions [0 2 -2 0 0 0 0]; Thank you in advance. |
Quick answer @pnovo: Notice that the output shows this:
Code:
wallShearStress wallShearStress: Please look inside the file "constant/polyMesh/boundary" and see of what type is the patch/boundary named "Walls". If it's not of type "wall", then that's why it did not calculate the shear stress there on that non-wall ;). |
Hi,
Thanks for the analysis. That's was exactly the issue. I manually changed the type in "boundary" from "patch" to "wall" and ran again the Code:
simpleFoam -postProcess -func wallShearStress Now, I am preparing my meshes with Salome, export to UNV file type and use Code:
ideasUnvToFoam Thank you! |
Wall shear stress utility writing normal stress also
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Hello, I am solving a Marangoni Convection Problem. I am using boundary condition as used here https://www.cfd-online.com/Forums/op...tml#post197203. The solver I am using is buoyantPimpleFoam.
I also have to plot the Nusselt No as mentioned in here http://www.tandfonline.com/doi/abs/1...07788808913603. The geometry is a 20mm x 20mm square cavity with marangoni bc at top surface and no slip on all side. The simulation is 2D. When I plot Shear Stress at the top surface (Y plane), it shows y component of stress also, which in my opinion is not possible as it is a normal stress to the plane. I also checked the wallShearStress.C and found that it uses deviatoric Stress tensor. The dev stress tensor should have zero values at its diagonal locations. I am not able to understand this. Although the Y-stress value is 2 order less but still I think it should be zero. Here is the output from wallShearStress. One more thing. I am using the function object wallShearStress. But some how it is writing the values at every calculation time, where as I want at certain time intervals. Can you suggest what am I missing here? Code:
functions Thanks |
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-time <ranges> comma-separated time ranges - eg, ':10,20,40:70,1000:' As for your wallShearStress also printing the components you could try calculating the magnitude of the parameter. With regards, Robert |
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Check this. Says the wallShearStress is given as a volVectorField. So as Bruno said, you will have to take the magnitude of it as \sqrt(taux^2 + tauy^2 + tauz^2). |
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