|
[Sponsors] |
[ICEM] A mesh generation for aero acoustic computation |
|
LinkBack | Thread Tools | Search this Thread | Display Modes |
April 17, 2010, 13:18 |
|
#7 |
Senior Member
Simon Pereira
Join Date: Mar 2009
Location: Ann Arbor, MI
Posts: 2,663
Blog Entries: 1
Rep Power: 47 |
Nope, these are all different methods... What matters is how the mesh is generated. The methods that work with the Density boxes all rely on top down meshing with a back ground grid... On the other hand, Hexa relies on a blocking structure that lets you mesh it any way you like... You can refine blocks in hexa or use blocking strategies (such as Ogrid) to refine the mesh...
The method closest to what you had seen in Gambit is the Patch Independent surface meshing with "quad" or "quad dominant". This method will accept density zones or sizing function in the same way (and for the same reasons) as they worked in Gambit... Other methods, such as ICEM CFD Hexa, may be able to give a much higher quality mesh, but require a bit more practice and effort due to the higher level of user interaction. Have you tried the ICEM CFD Hexa tutorials? Simon |
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
[ICEM] Generating Mesh for STL Car in Windtunnel Simulation | tommymoose | ANSYS Meshing & Geometry | 48 | April 15, 2013 04:24 |
Mesh generation software is needed | H.Dou | Main CFD Forum | 12 | May 4, 2011 15:20 |
ICEM - incomplete mesh generation | ralph | CFX | 0 | June 23, 2008 23:35 |
Convergence moving mesh | lr103476 | OpenFOAM Running, Solving & CFD | 30 | November 19, 2007 14:09 |
3-d elliptic generation mesh | Gang Sun | Main CFD Forum | 5 | September 16, 1998 00:24 |