|June 4, 2011, 13:28||
Join Date: Aug 2010
Posts: 26Rep Power: 7
" 'rhoCentralFoam' is a transient/time accurate solver.
Then using higher Courant numbers (which is say under stability criterion) will help
in time marching to a steady state solution (SSS) which would be faster than the SSS reached using time accurate procedure."
(or) If it is not, any other alternate way to modify the code to reach the SSS faster!
I want anyone's suggestion/comment on this issue.
|Thread||Thread Starter||Forum||Replies||Last Post|
|rhoCentralFoam with totalPressure/totalTemperature at inlet of subsonic channel||deepblue17||OpenFOAM Running, Solving & CFD||5||February 11, 2013 03:42|
|Question about rhoCentralFoam||praveen||OpenFOAM||0||April 24, 2011 02:09|
|Hypersonic flow rhoCentralFoam||ishaninair||OpenFOAM Running, Solving & CFD||0||April 7, 2011 04:38|
|Always crash when solve a C-D nozzle flow field using rhoCentralFoam||hawklion||OpenFOAM Running, Solving & CFD||0||March 9, 2011 07:13|
|Always crash when solve a C-D nozzle flow field using rhoCentralFoam||hawklion||OpenFOAM||3||March 8, 2011 20:03|