CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > Special Topics > Mesh Generation & Pre-Processing

skewFaces Errors after snappyHexMesh

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   January 18, 2017, 10:14
Default skewFaces Errors after snappyHexMesh
  #1
New Member
 
Kryss
Join Date: Dec 2016
Posts: 9
Rep Power: 9
totalBeginner is on a distinguished road
Hey guys,
I have included a .stl-File and want to create a mash. So I used surfaceFeatureExtract, BlockMesh and snappyHexMesh. When I tryed "checkMesh", the answer was:

Create time

Create polyMesh for time = 0

Time = 0

Mesh stats
points: 3585719
faces: 10022446
internal faces: 9352200
cells: 3221166
faces per cell: 6.01479
boundary patches: 7
point zones: 0
face zones: 0
cell zones: 0

Overall number of cells of each type:
hexahedra: 2987288
prisms: 161904
wedges: 0
pyramids: 0
tet wedges: 0
tetrahedra: 0
polyhedra: 71974
Breakdown of polyhedra by number of faces:
faces number of cells
5 464
6 3624
9 65770
12 2112
15 4

Checking topology...
Boundary definition OK.
Cell to face addressing OK.
Point usage OK.
Upper triangular ordering OK.
Face vertices OK.
Number of regions: 1 (OK).

Checking patch topology for multiply connected surfaces...
Patch Faces Points Surface topology
inlet 1040 1134 ok (non-closed singly connected)
outlet 1040 1134 ok (non-closed singly connected)
front 23600 23976 ok (non-closed singly connected)
back 23600 23976 ok (non-closed singly connected)
bottom 3835 4144 ok (non-closed singly connected)
atmosphere 3835 4144 ok (non-closed singly connected)
Kanal 613296 613514 ok (closed singly connected)

Checking geometry...
Overall domain bounding box (-16 -0.5 -9.5) (43 2.2 6.5)
Mesh (non-empty, non-wedge) directions (1 1 1)
Mesh (non-empty) directions (1 1 1)
Boundary openness (-1.16337e-19 -3.50034e-14 4.62428e-15) OK.
Max cell openness = 5.91374e-16 OK.
Max aspect ratio = 5.79441 OK.
Minimum face area = 7.73338e-05. Maximum face area = 0.0435317. Face area magnitudes OK.
Min volume = 3.26601e-05. Max volume = 0.00872124. Total volume = 2543.98. Cell volumes OK.
Mesh non-orthogonality Max: 56.7907 average: 8.29633
Non-orthogonality check OK.
Face pyramids OK.
***Max skewness = 7.71711, 16 highly skew faces detected which may impair the quality of the results
<<Writing 16 skew faces to set skewFaces
Coupled point location match (average 0) OK.

Failed 1 mesh checks.

End



Do you have any idea what to do? I've tried foamToVTK to show me the problems in paraView, but it seems that my whole stl-Geometry is the problem...
Thank you!
Attached Images
File Type: jpg parafoamfoto.jpg (110.8 KB, 14 views)
totalBeginner is offline   Reply With Quote

Old   January 19, 2017, 07:21
Default
  #2
Member
 
power
Join Date: Jun 2014
Posts: 86
Rep Power: 12
enginpower is on a distinguished road
I state I'm a beginner too, so I can't answer with a solution.

But because I want to learn, and maybe this will be useful to also who can help you too, I'd want to know how did you create the stl file, what are your snappyHexMeshDict and the blockMeshDict files.
Thanks

Last edited by enginpower; January 19, 2017 at 07:23. Reason: grammar checks
enginpower is offline   Reply With Quote

Reply

Tags
mesh 3d, shm, skewfaces


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
Building OpenFOAM1.7.0 from source ata OpenFOAM Installation 46 March 6, 2022 14:21
How to write k and epsilon before the abnormal end xiuying OpenFOAM Running, Solving & CFD 8 August 27, 2013 16:33
Upgraded from Karmic Koala 9.10 to Lucid Lynx10.04.3 bookie56 OpenFOAM Installation 8 August 13, 2011 05:03
IcoFoam parallel woes msrinath80 OpenFOAM Running, Solving & CFD 9 July 22, 2007 03:58
Could anybody help me see this error and give help liugx212 OpenFOAM Running, Solving & CFD 3 January 4, 2006 19:07


All times are GMT -4. The time now is 23:31.