CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > Software User Forums > SU2

Mesh deformation not converging with 'GRID_DEFORM_METHOD' as "FEA"

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   October 9, 2013, 01:53
Default Mesh deformation not converging with 'GRID_DEFORM_METHOD' as "FEA"
  #1
Member
 
Anant Diwakar
Join Date: Jan 2013
Posts: 68
Rep Power: 13
diwakaranant is on a distinguished road
Hi

I was trying to find the gradients for Onera M6 wing for rans case using
finite_differences.py using SU2 v 2.0.5

I am using "FEA" as grid deform method, but the mesh deformation doesn't
seem to converge when the mesh is deformed after each flow run.

HTML Code:
----------------- FFD technique (parametric -> cartesian) ---------------
Update cartesian coord        | FFD box: 0. Max diff: 1.46435e-07.

----------------------- Volumetric grid deformation ---------------------
Performing the deformation of the volumetric grid.
=> BCGSTAB residual history
=> residual tolerance target = 1e-08
=> initial residual norm     = 7.61365e+06
     0     3.20299e+12
     50     15819.9
     100     2367.66
     150     851.439
     200     613.143
     250     23395.4
     300     3507.32
# BCGSTAB final (true) residual:
# iteration = 300: |res|/|res0| = 3507.32
End and write output files.

------------------------- Exit Success (SU2_MDC) ------------------------
The mesh deformation code seems to run upto 300 iterations leading
to incomplete convergence.

Why is this happening ?

Thanks
Anant
diwakaranant is offline   Reply With Quote

Old   October 9, 2013, 17:09
Default
  #2
Super Moderator
 
Francisco Palacios
Join Date: Jan 2013
Location: Long Beach, CA
Posts: 404
Rep Power: 15
fpalacios is on a distinguished road
Quote:
Originally Posted by diwakaranant View Post
Hi

I was trying to find the gradients for Onera M6 wing for rans case using
finite_differences.py using SU2 v 2.0.5

I am using "FEA" as grid deform method, but the mesh deformation doesn't
seem to converge when the mesh is deformed after each flow run.

HTML Code:
----------------- FFD technique (parametric -> cartesian) ---------------
Update cartesian coord        | FFD box: 0. Max diff: 1.46435e-07.

----------------------- Volumetric grid deformation ---------------------
Performing the deformation of the volumetric grid.
=> BCGSTAB residual history
=> residual tolerance target = 1e-08
=> initial residual norm     = 7.61365e+06
     0     3.20299e+12
     50     15819.9
     100     2367.66
     150     851.439
     200     613.143
     250     23395.4
     300     3507.32
# BCGSTAB final (true) residual:
# iteration = 300: |res|/|res0| = 3507.32
End and write output files.

------------------------- Exit Success (SU2_MDC) ------------------------
The mesh deformation code seems to run upto 300 iterations leading
to incomplete convergence.

Why is this happening ?

Thanks
Anant
The current 3D implementation of the grid deformation is based on Tets (as a preprocessing the Hex are divided into Tets). This is not optimal, we are working in a real FEM implementation of the Hex element. But this going to take some time unless somebody in the open-source community helps us with this "easy" development.

Meanwhile, our recommendation is use Tets grids or perform small deformations and use the parameter.
LINEAR_SOLVER_ITER=10

Cheers,
Francisco
fpalacios is offline   Reply With Quote

Old   October 11, 2013, 15:51
Default
  #3
Super Moderator
 
Thomas D. Economon
Join Date: Jan 2013
Location: Stanford, CA
Posts: 271
Rep Power: 14
economon is on a distinguished road
Hi,

I'll also pitch in and say that it may be worth trying with one of the newer versions of SU2, such as V2.0.8, as we have made a few improvements to the FEA since V2.0.5.

T
economon is offline   Reply With Quote

Reply


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
Star CCM Overset Mesh Error (Rotating Turbine) thezack Siemens 7 October 12, 2016 11:14
Update of the variables after dynamic mesh motion. gtg258f OpenFOAM Programming & Development 9 January 18, 2014 10:08
overflow and negative volume error in mesh deformation sakalido CFX 11 November 27, 2012 15:16
[snappyHexMesh] snappyHexMesh won't work - zeros everywhere! sc298 OpenFOAM Meshing & Mesh Conversion 2 March 27, 2011 21:11
How to control Minximum mesh space? hung FLUENT 7 April 18, 2005 09:38


All times are GMT -4. The time now is 02:15.