 |
 |
 |
|
|
|
[Sponsors] | ||||
October 31, 2012, 19:25
|
C-mesh problem
|
#1 |
|
Member
Umut Can
Join Date: Oct 2012
Posts: 42
Rep Power: 14  |
 high guys, I have a problem with c-meshing. Although i was able to mesh the domain for naca0012, i could not do it for sd7003 case. Problem was about mapped face meshing option. Mapped option was used for the two faces behind the trealing edge of the airfoil. However, it did not work for the other faces. If you look at the picture you will see this case. Could anyone help ? Best regards... |
|
|
|
|
|
November 3, 2012, 18:51
|
|
#2 |
|
Member
Umut Can
Join Date: Oct 2012
Posts: 42
Rep Power: 14 |
anybody? i really need help
|
|
|
|
|
|
|
November 3, 2012, 23:28
|
|
#3 |
|
Senior Member
|
It should work. I remember, I worked with tyler on the scripting in ICEM which automatically take care of meshing of any airfoil. So if you need that script, I can send it to you
|
|
|
|
|
|
 |
|
|
Similar Threads
|
||||
| Thread | Thread Starter | Forum | Replies | Last Post |
| Dynamic Mesh Problem. | Tom Clark | FLUENT | 10 | June 21, 2021 05:27 |
| Gambit problems | Althea | FLUENT | 22 | January 4, 2017 04:19 |
| Icemcfd 11: Loss of mesh from surface mesh option? | Joe | CFX | 2 | March 26, 2007 19:10 |
| Convergence problem when ustructured mesh is used. | SangJin Ryu | Siemens | 3 | October 5, 2000 21:26 |
| Mesh | Mignard | FLUENT | 2 | March 22, 2000 06:12 |
Linear Mode
