|
[Sponsors] |
![]() |
![]() |
#1 |
Senior Member
Giles Richardson
Join Date: Jun 2012
Location: Cambs UK
Posts: 111
Rep Power: 15 ![]() |
finally getting rhoSimplecFoam (with transonic=yes) to run and converge for a Mach 0.8 aircraft case, although it is very twitchy for initial values for omega.
|
|
![]() |
![]() |
![]() |
Tags |
convergence, openfoam, rhosimplecfoam |
Thread Tools | Search this Thread |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
2D Hypersonic Inlet in FLUENT - Convergence Issues | Fraisdegout | FLUENT | 6 | December 15, 2016 02:07 |
Convergence issues for steady turbulent diffusion flame | stuntmanmike | CFX | 5 | November 7, 2014 17:37 |
Convergence Issues 2D Airfoil | AeroEngiNerd | STAR-CCM+ | 1 | February 28, 2012 09:34 |
Force can not converge | colopolo | CFX | 13 | October 4, 2011 22:03 |
convergence issues on steady state solver | icemaniac178 | CFX | 1 | March 30, 2011 19:11 |