CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > Software User Forums > OpenFOAM > OpenFOAM Pre-Processing

killed "snappyHexMesh"

Register Blogs Community New Posts Updated Threads Search

Like Tree1Likes
  • 1 Post By alberto

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   April 7, 2012, 23:21
Default killed "snappyHexMesh"
  #1
New Member
 
hs
Join Date: Mar 2012
Posts: 22
Rep Power: 14
parkh32 is on a distinguished road
hi all

I'v run the snappyHexMesh and got the problem, Killed..

Anyone can help me, please ?

thanks//
hs

~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~

$ snappyHexMesh


// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
Create time

Create mesh for time = 0

Read mesh in = 3.84 s

Overall mesh bounding box : (-25 -6 -0.7) (5 6 0.4)
Relative tolerance : 1e-06
Absolute matching distance : 3.23297e-05

Reading refinement surfaces.
Read refinement surfaces in = 0.05 s

Reading refinement shells.
Refinement level 1 for all cells inside box1
Refinement level 2 for all cells inside box2
Refinement level 2 for all cells inside box3
Read refinement shells in = 0 s

Setting refinement level of surface to be consistent with shells.
Checked shell refinement in = 0 s

Reading features.
Read features in = 0 s


Determining initial surface intersections
-----------------------------------------

Edge intersection testing:
Number of edges : 1228620
Number of edges to retest : 1228620
Number of intersected edges : 11643
Calculated surface intersections in = 4.15 s

Initial mesh : cells:396000 faces:1228620 points:437052
Cells per refinement level:
0 396000

Adding patches for surface regions
----------------------------------

Patch Type Region
----- ---- ------
hull:

4 wall hull_CreatedbyGmsh

Added patches in = 0.07 s

Selecting decompositionMethod simple

Refinement phase
----------------

Found point (-2 0 0) in cell 269929 on processor 0

Surface refinement iteration 0
------------------------------

Marked for refinement due to surface intersection : 15305 cells.
Determined cells to refine in = 1.35 s
Selected for refinement : 15305 cells (out of 396000)
Edge intersection testing:
Number of edges : 1585770
Number of edges to retest : 459084
Number of intersected edges : 46521
Refined mesh in = 4.77 s
After refinement surface refinement iteration 0 : cells:503135 faces:1585770 points:580318
Cells per refinement level:
0 380695
1 122440

Surface refinement iteration 1
------------------------------

Marked for refinement due to surface intersection : 62292 cells.
Determined cells to refine in = 0.12 s
Selected for refinement : 67930 cells (out of 503135)
Edge intersection testing:
Number of edges : 3154578
Number of edges to retest : 2023445
Number of intersected edges : 185977
Refined mesh in = 11.89 s
After refinement surface refinement iteration 1 : cells:978645 faces:3154578 points:1198876
Cells per refinement level:
0 374987
1 105882
2 497776

Surface refinement iteration 2
------------------------------

Marked for refinement due to surface intersection : 327 cells.
Determined cells to refine in = 0.31 s
Selected for refinement : 379 cells (out of 978645)
Edge intersection testing:
Number of edges : 3163407
Number of edges to retest : 28843
Number of intersected edges : 186257
Refined mesh in = 8.79 s
After refinement surface refinement iteration 2 : cells:981298 faces:3163407 points:1202428
Cells per refinement level:
0 374935
1 105971
2 500392

Surface refinement iteration 3
------------------------------

Marked for refinement due to surface intersection : 13 cells.
Determined cells to refine in = 0.3 s
Selected for refinement : 15 cells (out of 981298)
Edge intersection testing:
Number of edges : 3163755
Number of edges to retest : 1287
Number of intersected edges : 186262
Refined mesh in = 8.44 s
After refinement surface refinement iteration 3 : cells:981403 faces:3163755 points:1202566
Cells per refinement level:
0 374933
1 105974
2 500496

Surface refinement iteration 4
------------------------------

Marked for refinement due to surface intersection : 1 cells.
Determined cells to refine in = 0.31 s
Selected for refinement : 2 cells (out of 981403)
Edge intersection testing:
Number of edges : 3163803
Number of edges to retest : 167
Number of intersected edges : 186262
Refined mesh in = 8.32 s
After refinement surface refinement iteration 4 : cells:981417 faces:3163803 points:1202586
Cells per refinement level:
0 374932
1 105981
2 500504

Surface refinement iteration 5
------------------------------

Marked for refinement due to surface intersection : 0 cells.
Determined cells to refine in = 0.25 s
Selected for refinement : 0 cells (out of 981417)
Stopping refining since too few cells selected.


Removing mesh beyond surface intersections
------------------------------------------

Found point (-2 0 0) in cell 562633 in global region 0 out of 1 regions.
Keeping all cells in region 0 containing point (-2 0 0)
Selected for keeping : 981417 cells.
Edge intersection testing:
Number of edges : 3163803
Number of edges to retest : 0
Number of intersected edges : 186262

Shell refinement iteration 0
----------------------------

Marked for refinement due to refinement shells : 304456 cells.
Determined cells to refine in = 10.17 s
Selected for internal refinement : 327315 cells (out of 981417)
Killed

~~~~~~~~~~~~~~~~~~~~~
parkh32 is offline   Reply With Quote

Old   April 8, 2012, 17:53
Default
  #2
Senior Member
 
Alberto Passalacqua
Join Date: Mar 2009
Location: Ames, Iowa, United States
Posts: 1,912
Rep Power: 36
alberto will become famous soon enoughalberto will become famous soon enough
Probably you have "ulimit" set to a smaller value for the process memory than what snappyHexMesh would want to use for your case. If that happens, the system will kill the snappyHexMesh process.
charlliemarshalll likes this.
__________________
Alberto Passalacqua

GeekoCFD - A free distribution based on openSUSE 64 bit with CFD tools, including OpenFOAM. Available as in both physical and virtual formats (current status: http://albertopassalacqua.com/?p=1541)
OpenQBMM - An open-source implementation of quadrature-based moment methods.

To obtain more accurate answers, please specify the version of OpenFOAM you are using.
alberto is offline   Reply With Quote

Old   April 8, 2012, 18:12
Default
  #3
New Member
 
hs
Join Date: Mar 2012
Posts: 22
Rep Power: 14
parkh32 is on a distinguished road
thank you for your reply.

hs//
parkh32 is offline   Reply With Quote

Reply


Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

BB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Trackbacks are Off
Pingbacks are On
Refbacks are On


Similar Threads
Thread Thread Starter Forum Replies Last Post
parallel fluent runs being killed at partitioing Ben Aga FLUENT 3 June 8, 2012 11:40
[snappyHexMesh] snappy hangs while layer generation bastil OpenFOAM Meshing & Mesh Conversion 3 October 29, 2010 08:19
[ICEM CFD] Child killed: segmentation violation vmlxb6 ANSYS Meshing & Geometry 0 September 2, 2010 08:07
Solver killed sega OpenFOAM Running, Solving & CFD 4 June 2, 2008 18:33
Killed by signal 8 after first timestep matthias OpenFOAM Running, Solving & CFD 0 December 9, 2005 09:06


All times are GMT -4. The time now is 15:02.