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

Unsteady Multirow computation

Register Blogs Community New Posts Updated Threads Search

Like Tree3Likes
  • 3 Post By colinda1

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   January 18, 2019, 02:26
Default Unsteady Multirow computation
  #1
New Member
 
Vishwas Verma
Join Date: Mar 2016
Location: Mumbai India
Posts: 25
Rep Power: 10
vishwasvemra is on a distinguished road
Hi all,


I am trying to perform unsteady computations of two stage machine with domains R1, S1, R2, S2. Originally I had different blade counts(22,34,18,26) but to save computational time I have changed them to (24,36,18,24) method suggesting in Fine/Turbo theory guide p.179 i.e. domain scaling. With the modified blade counts and blades in ratio of(4,6,3,4) accounting to 60degree perfect sector for each row, I am trying to generate solution using Fine/Turbo 12.1.
Blade rotations are(-16000,0,24000,0).

The problem I encounter is solver exits with error message of 'SPEEDS OF ROTATION ARE DIFFERENT' (from .std file).
I am not sure what is causing solver failure. Is multistage computation not allowed? I found a discussion on this forum(https://www.cfd-online.com/Forums/nu...imulation.html) where Mr. Ji could perform computations with different rotation speeds.
Also I don't see NOFROT and IDOMSC expert parameters as suggested by Mr. Alain in same discussion forum.


Please help how to fix this.


Thankyou!


Kind Regards,
vishwas
vishwasvemra is offline   Reply With Quote

Old   January 21, 2019, 05:33
Default
  #2
Senior Member
 
Colinda
Join Date: May 2012
Location: Brussels
Posts: 153
Rep Power: 14
colinda1 is on a distinguished road
Hi Vishwas,

Did you define rotor/stator interfaces in between the rows? With the correct definition of rotor/stator interfaces there should indeed not be any problem to run such a domain scaling simulation.

The post you link to is from 2003 so the version used is already very old and FINE/Turbo has evolved a lot since then. For the way to define the number of time steps and the activation of domain scaling, please do take a look at the user guide of your FINE/Turbo release.

Best regards,
Colinda
colinda1 is offline   Reply With Quote

Old   January 21, 2019, 08:32
Default
  #3
New Member
 
Vishwas Verma
Join Date: Mar 2016
Location: Mumbai India
Posts: 25
Rep Power: 10
vishwasvemra is on a distinguished road
Hi Colinda,


Thanks for replying!


Yes, the rotor/stator interface is defined correctly by default, as the complete mesh is generated using Autogrid5.

While going through the Fine/Turbo user guide, on page 253, its mentioned ''The FINE™/Turbo solver allows only one rotation speed (combined with a zero rotation speed) when performing an unsteady simulation using the Domain Scaling method.''


From this text it seems like the solver doesn't allow multiple rotation speed.

For the shake of checking above statement, when I made the rotation speed of both rotor same the simulation starts without any issue.


Thankyou


Kind Regards,
Vishwas
vishwasvemra is offline   Reply With Quote

Old   January 21, 2019, 10:42
Default
  #4
Senior Member
 
Colinda
Join Date: May 2012
Location: Brussels
Posts: 153
Rep Power: 14
colinda1 is on a distinguished road
Sorry, I confused one important information in your email with the one in the link: in your case it is not counter-rotating with an equal magnitude of rotation. You have -16000 and 24000 (not 16000). This is indeed not possible.
colinda1 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
use unsteady computation results to other compute turbinesv CFX 2 October 12, 2008 09:55
Unsteady turbulence model computation K.S. Cjang Main CFD Forum 0 January 6, 2006 22:06
blade interface for unsteady computation wang CFX 1 June 11, 2003 19:33
blade interface for unsteady computation wang Main CFD Forum 2 June 11, 2003 13:02
Unsteady computation using sliding mesh Ales Skotak FLUENT 0 September 7, 2000 08:03


All times are GMT -4. The time now is 07:39.