|
[Sponsors] |
April 4, 2002, 21:02 |
gambit mesh problem
|
#1 |
Guest
Posts: n/a
|
Hi,everyone I want to calculate the flow field around an airfoil.I use the far-field Boundary Conditions so the airfoil is put in the middle of a square domain. I want to make dense meshes near the airfoil and thin meshes far away the airfoil. How should I do in FLUENT 5.5? Thanks for any response!
|
|
April 7, 2002, 18:28 |
Re: gambit mesh problem
|
#2 |
Guest
Posts: n/a
|
Well that problem seems familiar to me. I would recommend you to have a semicircular domain with the arc of circle at the front. This would give you the best mesh. Also use boundary layer near the airfoil surface to capture velocity and pressure distribution correctly. You could also try meshing with successive ratios to achieve that.
|
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
[GAMBIT] Problem with mesh in Gambit | giuseppemerlini | ANSYS Meshing & Geometry | 12 | November 10, 2014 01:04 |
Gambit - meshing over airfoil wrapping (?) problem | JFDC | FLUENT | 1 | July 11, 2011 05:59 |
[Gmsh] gmshToFoam problem: not the same mesh in Gmsh vs. paraview | zhernadi | OpenFOAM Meshing & Mesh Conversion | 8 | July 7, 2011 02:28 |
Convergence moving mesh | lr103476 | OpenFOAM Running, Solving & CFD | 30 | November 19, 2007 14:09 |
Problem for making mesh in GAMBIT | chlim | FLUENT | 0 | July 8, 2005 18:23 |