|
[Sponsors] |
![]() |
![]() |
#1 |
Guest
Posts: n/a
|
Hi! I wrote a 3d turbomachinery Euler code based on Runge Kutta Jameson (JST) four time step scheme. It works well with the exception, that the radial momentum equation is allways finishing with 10 to 100x higher average residual error as the other equations. What might be the reason for it. Has anybody similar experience?
|
|
![]() |
![]() |
Thread Tools | Search this Thread |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
transsonic nozzle with rhoSimpleFoam | Unseen | OpenFOAM Running, Solving & CFD | 8 | July 1, 2022 07:54 |
Extrusion with OpenFoam problem No. Iterations 0 | Lord Kelvin | OpenFOAM Running, Solving & CFD | 8 | March 28, 2016 12:08 |
How to write k and epsilon before the abnormal end | xiuying | OpenFOAM Running, Solving & CFD | 8 | August 27, 2013 16:33 |
Orifice Plate with a fully developed flow - Problems with convergence | jonmec | OpenFOAM Running, Solving & CFD | 3 | July 28, 2011 06:24 |
Differences between serial and parallel runs | carsten | OpenFOAM Bugs | 11 | September 12, 2008 12:16 |