CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > Software User Forums > OpenFOAM > OpenFOAM Post-Processing

A question about volume field representations of forces

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   August 11, 2022, 12:18
Default A question about volume field representations of forces
  #1
New Member
 
Saddam Hijazi
Join Date: May 2016
Posts: 17
Rep Power: 10
SaddamH is on a distinguished road
Hello everyone,


I have a curiosity regarding the so-called volume field representations of forces when computing the forces. I set the writeFields in the forces dictionary to yes




Code:
// Store and write volume field representations of forces and moments
    writeFields     yes;
Then I ran the problem of the flow around a cylinder in 2D. I got the forces fields where I have in each output folder a forces file named forces:force (also a moment field)


My question is how one should understand these fields ?


I would like to understand how I could compute the overall force vector that is acting on the cylinder given these forces fields representations. I thought that I only have to compute the sum of the forces after projecting them on x and y component using the angle that the cell (at which I have the forces value) is making with center of the cylinder. Is that correct ?

Last edited by SaddamH; August 11, 2022 at 18:02.
SaddamH is offline   Reply With Quote

Old   August 11, 2022, 12:50
Default
  #2
Senior Member
 
Domenico Lahaye
Join Date: Dec 2013
Posts: 798
Blog Entries: 1
Rep Power: 17
dlahaye is on a distinguished road
force (N) =
mass (kg or [1 0 0 0 0 0 0 0]) * acceleration (m/s^2 or [0 1 -2 0 0 0 0 0])
dlahaye is offline   Reply With Quote

Old   August 11, 2022, 18:01
Default
  #3
New Member
 
Saddam Hijazi
Join Date: May 2016
Posts: 17
Rep Power: 10
SaddamH is on a distinguished road
Thank you dlahaye, I am sorry, I don't know why I messed up in understanding the unit.


So my question is only about how one could compute the resultant force on the whole body given these forces values on the cells which are NOT evenly distributed on the cylinder boundary.


Thanks.
SaddamH is offline   Reply With Quote

Old   August 12, 2022, 04:49
Default
  #4
Senior Member
 
Domenico Lahaye
Join Date: Dec 2013
Posts: 798
Blog Entries: 1
Rep Power: 17
dlahaye is on a distinguished road
No worries. We are all learning here.

Force-vector on patch = surface-integral stress-tensor * normal-on-patch.

See e.g. Section Simple Stress of https://en.wikipedia.org/wiki/Stress_(mechanics)
dlahaye is offline   Reply With Quote

Old   August 12, 2022, 18:59
Default
  #5
New Member
 
Saddam Hijazi
Join Date: May 2016
Posts: 17
Rep Power: 10
SaddamH is on a distinguished road
Thanks dlahaye, I am still a bit confused of what I should do with fields named forces:force do you mean that I have to compute the integral of these fields over the surface of the cylinder after taking the scalar product with the normal vector ?
SaddamH is offline   Reply With Quote

Reply

Tags
force vector, forces and force coeff., forcesincompressible


Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

BB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Trackbacks are Off
Pingbacks are On
Refbacks are On


Similar Threads
Thread Thread Starter Forum Replies Last Post
[snappyHexMesh] snappyHexMesh does not detect highly skewed faces? ptpacheco OpenFOAM Meshing & Mesh Conversion 1 January 4, 2022 13:37
[swak4Foam] swakExpression not writing to log alexfells OpenFOAM Community Contributions 3 March 16, 2020 19:19
[mesh manipulation] Importing Multiple Meshes thomasnwalshiii OpenFOAM Meshing & Mesh Conversion 18 December 19, 2015 19:57
Problem of simulating of small droplet with radius of 2mm liguifan OpenFOAM Running, Solving & CFD 5 June 3, 2014 03:53
fluent add additional zones for the mesh file SSL FLUENT 2 January 26, 2008 12:55


All times are GMT -4. The time now is 07:01.