|
[Sponsors] |
February 12, 2010, 06:19 |
wing body tutorials, problem
|
#1 |
New Member
zhao xin
Join Date: Feb 2010
Location: Goteborg
Posts: 28
Rep Power: 16 |
Hi, guys,
I got a trouble when doing the tutorials of ICEM, the wing body, hexa mesh. I followed the instructions and steps carefully. But the result I got is different from the mesh size that the tutorial shows. I got 40 millions nodes and hexas, after I set the surface mesh parameters as, maximum size to 300, height to 300 and height ratio to 1. This lead me can't even see the grid in the pre-mesh. on the same edge, I got 3332 nodes, and tutorial shows only 115. Hope somebody can help me with this rokie problem. Thank you! |
|
February 14, 2010, 19:05 |
not sure...
|
#2 |
Senior Member
Simon Pereira
Join Date: Mar 2009
Location: Ann Arbor, MI
Posts: 2,663
Blog Entries: 1
Rep Power: 47 |
I am not sure what went wrong... perhaps you had something set finer than you thought. If you post the files (*.tin and *.blk), I could take a quick look.
In the mean time, you can fix the edge distribution manually Use the middle icon to adjust edge distribution, select the edge and change the number of nodes to 115. Simon |
|
February 18, 2010, 06:08 |
|
#3 | |
New Member
zhao xin
Join Date: Feb 2010
Location: Goteborg
Posts: 28
Rep Power: 16 |
Quote:
Thank you for your information and sorry for this late reply. I solved the problem by changing the number of nodes on the edge manually. But I still don't know why the default number of nodes get that high. Because there is something wrong with my computer, the file lost. I will mesh it again and if the problem remains, I will post it to you and hope you can make a quick look. Thank you ^_^ Xin |
||
February 23, 2010, 11:04 |
|
#4 |
Senior Member
Emanuele
Join Date: Mar 2009
Posts: 110
Rep Power: 17 |
OT Where can i found wing body tutorial?!?! Thanks FOUND IT (Help section of software)
Last edited by nuovodna; February 23, 2010 at 11:08. Reason: Solved |
|
March 9, 2010, 16:40 |
|
#5 | |
New Member
Conrad Lee
Join Date: Mar 2010
Posts: 1
Rep Power: 0 |
Quote:
Thanks, Conrad Lee |
||
March 16, 2010, 09:19 |
|
#6 |
Member
User_CFD
Join Date: Mar 2010
Posts: 48
Rep Power: 16 |
I have an error as, how fix it, everybody?
A minor internal error has occurred. You may continue to work but if problems arise they may be related to this error. Try using the check/fix function to fix the problem The following message was designed to aid developers fix the problem: failed to allocate space for 140393388 nodes of 32 bytes each |
|
March 16, 2010, 14:52 |
Too many nodes, check edge params.
|
#7 |
Senior Member
Simon Pereira
Join Date: Mar 2009
Location: Ann Arbor, MI
Posts: 2,663
Blog Entries: 1
Rep Power: 47 |
lehoang_mai
Your mesh is just too big (too many, 140 million, nodes) for your machine... Chances are that something went wrong when you setup the sizes and things are really much finer than you think... In the model tree, right click on edges and turn on the option for bunching... I am pretty sure you will find some edges with way too many nodes. Then use Blocking tab to adjust the edge parameters for those edges to have fewer nodes... If you really did need 140 million nodes, then perhaps you should get a bigger 64 bit machine. Simon |
|
May 2, 2010, 17:12 |
|
#8 |
Member
User_CFD
Join Date: Mar 2010
Posts: 48
Rep Power: 16 |
Thanks Simon!
|
|
March 22, 2011, 02:05 |
|
#9 |
New Member
Join Date: Oct 2010
Location: USA
Posts: 18
Rep Power: 16 |
I ran into the same problem, but I was able to considerably reduce the number of nodes by manually changing the number of nodes through bunching. Thanks Simon that really helped me out!
Tony |
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
Can't get good results on ahmed body research | Michael | Main CFD Forum | 8 | September 17, 2008 14:55 |
Laminar wing profiles and drag | gregorv | OpenFOAM Running, Solving & CFD | 4 | December 4, 2007 14:25 |
Simulate flow field of moving body by dynamic meshes | luckyluke | OpenFOAM Running, Solving & CFD | 5 | January 10, 2006 05:37 |
Periodic flow boundary condition problem | sudha | FLUENT | 3 | April 28, 2004 09:40 |
Problem about 3D blunt body high Re simulation | David | FLUENT | 0 | September 27, 2002 11:59 |