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

Error in optimization of the RAE2822 airfoil with the mesh in the test case

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   May 21, 2013, 01:14
Default
  #21
Super Moderator
 
Francisco Palacios
Join Date: Jan 2013
Location: Long Beach, CA
Posts: 404
Rep Power: 15
fpalacios is on a distinguished road
Hi,

The new developer version 2.0.4 is now available. In this version we have improved a lot the stability of the direct solver. Give it a shot and increase the CFL number (Krylov based linear solvers are highly recommended)

Cheers,
Francisco
fpalacios is offline   Reply With Quote

Old   May 29, 2013, 07:30
Default
  #22
Member
 
Tommy Chen
Join Date: Mar 2011
Location: University of Michigan
Posts: 96
Rep Power: 15
Tommy Chen is on a distinguished road
Quote:
Originally Posted by diwakaranant View Post
Hi Francisco

Is the current developer (working RANS case) version available for download ?

Thanks
Anant
Hi Anant

I could run Su2 v2.0.4 well on rans optimization with airfoils, but when the frozen_vicosity option is NO, the iteration seems to diverge all the time.

Have you done a statisfied case with the frozen_viscosity=NO with rans airfoil optimization ?

Tommy
Tommy Chen is offline   Reply With Quote

Old   May 29, 2013, 07:32
Default
  #23
Member
 
Tommy Chen
Join Date: Mar 2011
Location: University of Michigan
Posts: 96
Rep Power: 15
Tommy Chen is on a distinguished road
Quote:
Originally Posted by fpalacios View Post
Hi Anant,

The adjoint RANS capability is a priority for SU2 developers team. For the time being we are developing two techniques: frozen eddy viscosity, and a new technique called hybrid adjoint.

Could you please try the new release 2.0.3 using the frozen viscosity adjoint?

Best,
Francisco
Hi Francisco

Could the current version handle the adjoint withle the frozen_viscosity equals to NO ? I have tried but the iteration seems to diverge all the time on a testcase of RAE2822 airfoil.

Tommy
Tommy Chen is offline   Reply With Quote

Old   May 30, 2013, 03:28
Default
  #24
Member
 
Anant Diwakar
Join Date: Jan 2013
Posts: 68
Rep Power: 13
diwakaranant is on a distinguished road
Hi Tommy

I ran RANS based shape design on RAE2822 airfoil and obtained
2.5 % reduction in drag, I used Frozen viscosity parameters as 'Yes'.

I tried to run the case with Frozen viscosity parameter as 'No', but the case
was not able to run and gave error after 1st flow solution.
The log and configuration file is attached.

Thanks
Anant
Attached Files
File Type: gz log.txt.gz (32.8 KB, 10 views)
File Type: txt turb_SA_RAE2822.cfg.txt (15.1 KB, 7 views)
diwakaranant is offline   Reply With Quote

Old   May 30, 2013, 06:09
Default
  #25
Member
 
Tommy Chen
Join Date: Mar 2011
Location: University of Michigan
Posts: 96
Rep Power: 15
Tommy Chen is on a distinguished road
Quote:
Originally Posted by diwakaranant View Post
Hi Tommy

I ran RANS based shape design on RAE2822 airfoil and obtained
2.5 % reduction in drag, I used Frozen viscosity parameters as 'Yes'.

I tried to run the case with Frozen viscosity parameter as 'No', but the case
was not able to run and gave error after 1st flow solution.
The log and configuration file is attached.

Thanks
Anant

Anant

I guess it is due to the absence of the Adjoint_Turbulent_Options , please check the configuration_template.

Tommy
Tommy Chen is offline   Reply With Quote

Old   May 30, 2013, 06:21
Default
  #26
Member
 
Anant Diwakar
Join Date: Jan 2013
Posts: 68
Rep Power: 13
diwakaranant is on a distinguished road
Hi Tommy

Can you share the configuration file ?

Thanks
Anant
diwakaranant is offline   Reply With Quote

Old   May 30, 2013, 06:37
Default
  #27
Member
 
Anant Diwakar
Join Date: Jan 2013
Posts: 68
Rep Power: 13
diwakaranant is on a distinguished road
Hi Tommy

Are you referring to CONV_NUM_METHOD_ADJTURB parameter ?

I am using nearly the same configuration file posted in this link (post no. 18)
by Francisco, in which too, this parameter is missing.

Even if we don't mention this parameter explicitly, won't SU2 take some default parameter for this variable ?

Can you share the configuration file used by you ?

Thanks
Anant
diwakaranant 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
how to set periodic boundary conditions Ganesh FLUENT 15 November 18, 2020 07:09
Gambit problems Althea FLUENT 22 January 4, 2017 04:19
[Other] 2D hex mesh on multi element airfoil Verfblikje OpenFOAM Meshing & Mesh Conversion 0 January 19, 2012 11:55
[snappyHexMesh] SnappyHexMesh not generate mesh first time mavimo OpenFOAM Meshing & Mesh Conversion 4 August 26, 2008 08:08
How to control Minximum mesh space? hung FLUENT 7 April 18, 2005 10:38


All times are GMT -4. The time now is 20:26.