|July 1, 2009, 11:36||
Join Date: May 2009
Posts: 14Rep Power: 8
I am looking to do computations about a turbine blade in a canal. I meshed it with Icem and already got a good solution with CFX, but I wanted to do a comparison of these results with OpenFoam solvers “SimpleFoam” or “rhoSimpleFoam”. The convergence with OpenFoam was as good as with CFX but when I want to have the distribution of the Total Pressure in a Slice Plane after the blade, I have no Secondary Flow. There was no problem with CFX. Has someone already being confronted with this problem? Where are the possibly failures in the Solvers or Fluid properties.
I joined my Case File for helping.
Thanks a lot.
|Thread||Thread Starter||Forum||Replies||Last Post|
|benchmark: flow over a circular cylinder||goodegg||Main CFD Forum||12||January 22, 2013 12:47|
|Flow meter Design||CD adapco Group Marketing||CD-adapco||3||June 21, 2011 08:33|
|Can 'shock waves' occur in viscous fluid flows?||diaw||Main CFD Forum||105||November 20, 2009 05:19|
|how to predict secondary flow in star-cd.||kathir||CD-adapco||4||April 3, 2006 16:37|
|mass flow inlet||Denis Tschumperle||FLUENT||7||August 9, 2000 02:19|