 |
 |
 |
|
|
|
[Sponsors] | ||||
September 6, 2007, 13:24
|
Iterations
|
#1 |
|
Guest
Posts: n/a
|
Hi I am using a structured c-mesh to analyze the GA (W)-1 airfoil to get a Y+ under 4.0 with Fluent at Spalart-Allmaras model taking into account the realistic conditions of Re, cord, Pt, Tt, density, Viscosity, and turbulent viscosity for an altitude of 966216 Pa, but the iterations are giving non-realistic results and don't converge. Could somebody teach me how I must define all conditions before initialize? Thanks for your help.
|
|
|
||
 |
| Thread Tools | Search this Thread |
| Display Modes | |
|
|
Similar Threads
|
||||
| Thread | Thread Starter | Forum | Replies | Last Post |
| transsonic nozzle with rhoSimpleFoam | Unseen | OpenFOAM Running, Solving & CFD | 8 | July 1, 2022 06:54 |
| Extrusion with OpenFoam problem No. Iterations 0 | Lord Kelvin | OpenFOAM Running, Solving & CFD | 8 | March 28, 2016 11:08 |
| How to write k and epsilon before the abnormal end | xiuying | OpenFOAM Running, Solving & CFD | 8 | August 27, 2013 15:33 |
| Orifice Plate with a fully developed flow - Problems with convergence | jonmec | OpenFOAM Running, Solving & CFD | 3 | July 28, 2011 05:24 |
| Differences between serial and parallel runs | carsten | OpenFOAM Bugs | 11 | September 12, 2008 11:16 |
Linear Mode
