CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > General Forums > Main CFD Forum

Turbomachinery and FLUENT

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   April 9, 1999, 03:02
Default Turbomachinery and FLUENT
  #1
chris
Guest
 
Posts: n/a
Hy, I want to design centrifugal pumps with FLUENT. My questions:

1. what do you think about the tools MRF and mixing plane ? do they provide good results and how is the convergence ? 2. sliding meshes: how many hours needs this unsteady 3D-calculation until you get usefull results? how much elements ? what type of hardware ? Is the sliding mesh tool really usefull in the "daily use" or is it more an "academic tool" for science and universities ?
  Reply With Quote

Old   April 9, 1999, 06:23
Default Re: Turbomachinery and FLUENT
  #2
Joern Beilke
Guest
 
Posts: n/a
For some cases MFR gives good results. Sometimes they even don't show the right direction. Then you have to use sliding mesh. Also if you are interested in transient phenomena like acoustics ... you have to use sliding mesh.

The computing time jumps from some hours (mfr) up to several weeks for sliding mesh Just expect to run 3 revolutions to get a periodic solution. To check this you should compute the integral values of the mass flux at the inlet and outlet at every time step and monitor them.

There are some articles about these things on my home page (www.beilke-cfd.de)
  Reply With Quote

Old   April 20, 1999, 15:56
Default Re: Turbomachinery and FLUENT
  #3
Alberto Tamm
Guest
 
Posts: n/a
Hello Chris,

First, sorry for my bad english.

The MRF tools give you good solutions when the interaction between rotor-stator is weak (now is the question what is weak?). It depends from the turbomachinery you are modelling. If you are modelling a pump with a volute, you will probably have problems in the tounge (born), but the global results will be reazonable.

Now I´m modelling a nq12 pump using MRF model (without lateral space (ohne radseitenraum), K-E, 3D. Operating under turbine and pump condition (betrieb).Structured mesh. 800.000 cells. aprox. 12 hours for converge.

In the nominal operating condition the results are good but with lower flow the Total presure are bigger in the static-rotor interface than in the inlet boundary face. Which is not good. (Turbinen-betrieb)

I´m very interesting in analize my results. If you have more experience in this topic, please write me an e.mail.
  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
Comparison of fluent and CFX for turbomachinery Far CFX 52 December 26, 2014 19:11
Fluent Errors during Turbomachinery Analysis kanduri FLUENT 0 June 20, 2011 03:44
I was no idea why i using Fluent other then cause by its reputation. herntan FLUENT 0 December 1, 2009 22:06
CFX, Fluent and Numeca? SA FLUENT 3 March 22, 2008 15:46
CFX or Fluent Confused guy CFX 8 October 19, 2005 01:09


All times are GMT -4. The time now is 15:07.