|March 14, 2011, 04:32||
Creating Hex Boundary Layer Mesh and Unstructured everywhere else
Join Date: Nov 2010
Posts: 7Rep Power: 8
I am studying wing tip blowing and I am trying to produce a structured mesh on my wing and on the boundary layer, whilst having an unstructured mesh around the wing.
I have tried different methods to obtain this but I am not getting what I want out of Ansys Mesher. I have used a combination of Multizone, Inflation and Face Sizing (on the wing).
I also need a fine mesh on the wing tip as this is where my UDF will be hooked onto.
If anyone has any suggestions for me, I would very much appreciate it.
Problem Info: 8m Wing,
(12m Height, 13m Width, 10m Length from TE) Domain,
NACA0012 Aerofoil (1m Chord)
EDIT: Sorry I forgot to add a screenshot.
However, my problem has now changed. I now do not need a boundary layer mesh as I will be modelling with inviscid solver. So by using the inviscid solver, this will remove wave and viscous drag, and leave only the lift-induced drag being calculated.
But, I need to create a structured mesh over the geometry and the domain. I also need very fine cell sizes on the wing tip as this is where my UDF will be applied to.
Info: I am studying the effects of wing tip blowing as a means to reduce the lift-induced drag on the wing.
Last edited by NLao; March 15, 2011 at 16:01. Reason: Forgot to add screenshots
|ansys, mesher, wing, wing tip|
|Thread||Thread Starter||Forum||Replies||Last Post|
|3D Hybrid Mesh Errors||DarrenC||ANSYS Meshing & Geometry||11||August 5, 2013 06:42|
|Boundary Layer Mesh in GAMBIT||Jane Wilkinson||FLUENT||2||December 4, 2006 10:36|
|Errors in Gambit for boundary layer mesh||Mike Spears||FLUENT||0||June 23, 2005 11:34|
|Boundary layer for unstructured mesh||Hunter Hsu||FLUENT||0||September 4, 2002 10:53|
|immersed boundary method with unstructured mesh||x.zhang||Main CFD Forum||0||August 25, 2002 21:57|