|March 8, 2011, 22:44||
Improve meshing non symmetrical airfoil
Join Date: Sep 2010
Posts: 20Rep Power: 7
Hi, I am trying to improve my mesh using GAMBIT (Basically because it is the mesh generator I have). I have seen mesh that are refined only on the airfoil, i would like to know how do the do it! because i have tried everything and i only got errors and a mesh so big that has so many elements that results impractical.
I attached some pictures so if you have any ideas it would be nice. I can use icem but i really donīt know how to use it.
I need a y+=1.
Itīs not a symmetrical airfoil, so i am stock and i do not know what yo do, any help would be nice
|March 9, 2011, 03:25||
Join Date: Mar 2009
Posts: 3,135Rep Power: 32
If you want a refined mesh only on airfoil, then you need to mesh your domain with tri (or quad-pave) with a size function.
y+ will be managed with a Boundary Layer.
In memory of my friend Hervé: CFD engineer & freerider
|Thread||Thread Starter||Forum||Replies||Last Post|
|Problem Meshing Airfoil||erodv||OpenFOAM||12||January 11, 2012 18:46|
|Airfoil Meshing Scheme in Gambit||J. Weiler||FLUENT||6||October 2, 2011 15:41|
|[Other] Ansys meshing airfoil and / or compressor blades||baw192||ANSYS Meshing & Geometry||8||September 23, 2011 00:43|
|Oscillating Airfoil - Dynamic meshing or user-defined velocity profile.||DarrenC||Main CFD Forum||5||July 19, 2010 22:33|
|[GAMBIT] Meshing airfoil using .dat file problem||creggie||ANSYS Meshing & Geometry||10||June 27, 2010 19:24|