 |
 |
 |
|
|
|
[Sponsors] | ||||
November 28, 2019, 09:11
|
fluent adapting mesh for shock problem
|
#1 |
|
New Member
Shin Huihoon
Join Date: Jul 2019
Posts: 1
Rep Power: 0  |
I'm a Fluent beginner.
i have a problem in analysis on supersonic. i will using adapting mesh in my problem and i studied fluent tutorial about adapting mesh. in tutorial, they suggest me to select a gradient of static pressure, then in the normalization, select scale and 0.3 for coarsening and 0.7 for refinement. But I wonder why it should be 0.3 and 0.7. Does Fluent just be set with those numbers for solving all kinds of coarsening and refinement for shock problem? Or is there any rule for finding numbers? |
|
|
|
|
 |
| Tags |
| adapting mesh, fluent, mesh, shock, supersonic |
|
|
Similar Threads
|
||||
| Thread | Thread Starter | Forum | Replies | Last Post |
| hybrid mesh created by pointwise fails mesh check in fluent due to left-handed faces | Hamid.de | Pointwise & Gridgen | 4 | November 9, 2016 12:20 |
| FLUENT adding mesh nodes problem when importing 3D mesh from ICEM | guxin7005 | FLUENT | 2 | June 27, 2016 22:41 |
| Moving mesh | Niklas Wikstrom (Wikstrom) | OpenFOAM Running, Solving & CFD | 122 | June 15, 2014 07:20 |
| Adapting the Mesh in Fluent | edongliang | Main CFD Forum | 0 | January 12, 2013 04:52 |
| fluent add additional zones for the mesh file | SSL | FLUENT | 2 | January 26, 2008 12:55 |
Linear Mode
