|
[Sponsors] | |||||
|
|
|
#1 |
|
Guest
Posts: n/a
|
Hi! Everyone Someone told me in order to obtain good converged results I need to keep the grid aspect ratio low too. But how about at the boundary layer? A.R usually high at the boundary layer.
|
|
|
||
|
|
|
#2 |
|
Guest
Posts: n/a
|
the key is how low is low...10 or 100 or 1000
|
|
|
||
|
|
|
#3 |
|
Guest
Posts: n/a
|
I usually consider something at about AR = 10~20 as acceptable. And depends on the local flow velocity so for something of high subsonic it would be better to keep it below 10.
|
|
|
||
![]() |
| Thread Tools | Search this Thread |
| Display Modes | |
|
|
Similar Threads
|
||||
| Thread | Thread Starter | Forum | Replies | Last Post |
| Automobile aero ground boundary layer OR simpleFoam/GAMG and high aspect ratio cells | kyle | OpenFOAM Running, Solving & CFD | 4 | January 4, 2011 12:17 |
| [GAMBIT] Viscous layer elements aspect ratio | siw | ANSYS Meshing & Geometry | 0 | September 29, 2009 06:10 |
| CREATION OF BOUNDARY LAYER | Jibran Haider | FLUENT | 3 | August 1, 2008 01:33 |
| GAMBIT problem with 3D Boundary Layer when meshing | Anthony Haroutunian | FLUENT | 2 | March 26, 2008 03:02 |
| New topic on same subject - Flow around race car | Tudor Miron | CFX | 15 | April 2, 2004 07:18 |