 |
 |
 |
|
|
|
[Sponsors] | ||||
Stalling problem with simpleFoam on a NACA0012 |
 |
|
|
LinkBack | Thread Tools | Search this Thread | Display Modes |
March 2, 2010, 04:13
|
Stalling problem with simpleFoam on a NACA0012
|
#1 |
|
New Member
Damien Guénot
Join Date: Mar 2009
Location: France
Posts: 1
Rep Power: 0  |
Hello,
I have a problem with a simpleFoam computation : I tried to compute a 2D NACA0012 at Re=100000 (Mach~0.17) but the stalling effect on drag and lift coefficient is underestimated, as can be seen on the following curves. I am using Spalart-Allmaras model. This mesh is the one used by Strelets (STRELETS, M., 2001, Detached eddy simulation of massively separated flows, AIAA Paper 2001-0879). It is a O shaped fine mesh (no wall function) expanding at 15 chords around the wing. I already used this mesh with an other solver and I didn't face this problem If someone has an idea, he would be welcome. Thank you Damien |
|
|
|
|
|
March 3, 2010, 07:46
|
link
|
#2 |
|
Senior Member
maddalena
Join Date: Mar 2009
Posts: 436
Rep Power: 23 |
Hello Damien,
welcome to the OpenFoam community! I had similar problems some time ago. Maybe this thread can help you: http://www.cfd-online.com/Forums/ope...omparison.html Good luck! maddalena |
|
|
|
|
|
|
|
|
Similar Threads
|
||||
| Thread | Thread Starter | Forum | Replies | Last Post |
| UDF compiling problem | Wouter | Fluent UDF and Scheme Programming | 6 | June 6, 2012 04:43 |
| Incoherent problem table in hollow-fiber spinning | Gianni | FLUENT | 0 | April 5, 2008 10:33 |
| natural convection problem for a CHT problem | Se-Hee | CFX | 2 | June 10, 2007 06:29 |
| Adiabatic and Rotating wall (Convection problem) | ParodDav | CFX | 5 | April 29, 2007 19:13 |
| convergence problem | Trushar | Phoenics | 5 | August 27, 2002 23:40 |
Linear Mode
