|
[Sponsors] |
April 3, 2013, 07:32 |
Asymmetric Aerofoil C-Grid
|
#1 |
New Member
Kurt Cuschieri
Join Date: Mar 2013
Posts: 7
Rep Power: 13 |
Dear all,
I've been working on constructing a C-grid for my Selig S3024 aerofoil but I've been trying to deal with the same problem for a while now. As you can see from the attached images, I've applied mapped meshing to the two square sections and edge sizing bias on all lines, with the semi-circular curve retaining the default no-bias but fixed number of divisions. The top quarter-circle has a good mesh, but the bottom quarter is horrible and I've been trying all sorts of methods and combinations but it just doesn't seem to want to mesh as the top quarter. Can anyone help me with this please? It's urgent! Thanks a lot in advance! |
|
April 3, 2013, 08:56 |
|
#2 |
Super Moderator
Ghazlani M. Ali
Join Date: May 2011
Location: Tokyo, Japan
Posts: 1,385
Blog Entries: 23
Rep Power: 29 |
I see a lot of people having just the same problem. Most of them follow the tutorial available in Cornell university.
Sorry i can't help with this one, if you have time, consider doing it in icem... |
|
April 3, 2013, 09:03 |
|
#3 |
Senior Member
|
If you can, upload the geometry file
|
|
April 3, 2013, 09:22 |
|
#4 |
New Member
Kurt Cuschieri
Join Date: Mar 2013
Posts: 7
Rep Power: 13 |
You may download my geometry file from this dropbox link:
https://www.dropbox.com/s/8j8zmzomnquvjj8/FFF.agdb I have been following a number of tutorials, now I'm going through this one - https://confluence.cornell.edu/displ...ometryinGAMBIT though that is using GAMBIT and I'm not. Thanks for your replies! |
|
April 3, 2013, 10:00 |
|
#5 |
New Member
Kurt Cuschieri
Join Date: Mar 2013
Posts: 7
Rep Power: 13 |
I also followed this tutorial:
https://confluence.cornell.edu/displ...Airfoil+-+Mesh to the letter but I'm getting an error saying that the mesh could not be generated due to poor quality elements or incorrect input. I am using the sweep tool to sweep the mesh on the surface shown across a thickness of 0.05m and I am also getting an error saying that I should change the element size parameters. |
|
April 3, 2013, 23:44 |
|
#6 |
Senior Member
|
I guess edges were not matching in the region where mesh is not mapped
https://dl.dropbox.com/u/68746918/as...caerofoil.wbpz |
|
April 4, 2013, 03:25 |
|
#7 |
New Member
Kurt Cuschieri
Join Date: Mar 2013
Posts: 7
Rep Power: 13 |
Hello Far,
Thanks for your reply! But unfortunately my version of the program is older so I cannot open the file you've attached. Could you kindly explain what the problem was? I've switched from 3D to 2D and so I'm not experiencing the problem anymore. Thanks once again Kurt |
|
April 4, 2013, 09:01 |
|
#8 |
Senior Member
|
Tried in v14.5, but will probably work in your version as well. Skip the step about Mapped faces. Instead just set your edge sizes and insert a Method, choose Multizone, selecting all bodies, with the following settings:
|
|
April 4, 2013, 09:56 |
|
#9 |
New Member
Kurt Cuschieri
Join Date: Mar 2013
Posts: 7
Rep Power: 13 |
that looks awesome!
Thanks so much for your help, much appreciated |
|
November 15, 2014, 19:54 |
ICEM tutorials
|
#11 |
Member
Radwanma
Join Date: Oct 2014
Posts: 30
Rep Power: 12 |
Hi all,
I will be thankful if you give me tutorials in ICEM mesh. Thanks |
|
November 16, 2014, 17:15 |
ICEM mesh
|
#12 |
Member
Radwanma
Join Date: Oct 2014
Posts: 30
Rep Power: 12 |
Dear All,
Do you have tutorials in ICEM aerofoil meshing? Many thanks in advance |
|
November 27, 2014, 22:11 |
|
#13 |
New Member
siddharth hans
Join Date: Sep 2014
Posts: 4
Rep Power: 12 |
guys, i am facing a similar problem for a flat bottom airfoil 2D ansys meshing.As you can see from the attached images, I've applied mapped meshing to the two square sections and edge sizing bias on all lines, with the semi-circular curve retaining the default no-bias but fixed number of divisions. i am able to map the right square portions successfully but the left half seems to go haywire for every tried combination.
any help is hugely appreciated! thanks in advance. sid |
|
November 29, 2014, 13:25 |
|
#14 |
New Member
siddharth hans
Join Date: Sep 2014
Posts: 4
Rep Power: 12 |
Got it figured out! Edge sizing is the word.
|
|
April 24, 2016, 19:52 |
|
#15 |
New Member
Anonymous
Join Date: Apr 2016
Posts: 8
Rep Power: 10 |
Sorry to bump up this old thread, but I am having trouble similar to those mentioned in here. What changes did you make to your Edge sizing, hans.siddharth (if you can still recall)?
|
|
Tags |
aerofoil, ansys, grid, meshing |
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
MapFields to New Grid For Extreme Grid Deformations due to Body Motion | albcem | OpenFOAM | 0 | May 5, 2009 15:17 |
Grid Adaptation | Suresh | FLUENT | 0 | October 15, 2003 14:18 |
GRID TO GRID INTERPOLATION in FLUENT | calogero | FLUENT | 3 | June 4, 2003 09:32 |
Combustion Convergence problems | Art Stretton | Phoenics | 5 | April 2, 2002 06:59 |
Troubles modelling flow through a grid | Hans Klaufus | CFX | 1 | June 28, 2000 17:43 |