Zigmhount
Mechanical
- Apr 6, 2009
- 16
Hi all,
I'm currently testing the "skinning" of a 3D-finite elemente model to reduce the amount of data for a fatigue analysis (mentionned at the end of thread727-232206).
I modelled a complex (cast) part with Tet10 (10-nodes tetrahedal) volume elements, then meshed the surfaces with Tria6 (6-nodes surface elements) shell elements and merged the nodes of solid and surface meshes (including midside nodes).
The shell elements have a thickness of 0,001mm and the same material property as the volume elements.
I then compare the nodal output in solid and shell elements (unaveraged maximum value of strain and stress).
The max principal stress/strain distribution is the same in both solid and shell meshes, however the max stress value in the skin is slightly inferior to the max value at the corner of the solid elements (up to 1%, depending on mesh fineness)... Which one should I trust??...
Thanks for your help!
Simon
I'm currently testing the "skinning" of a 3D-finite elemente model to reduce the amount of data for a fatigue analysis (mentionned at the end of thread727-232206).
I modelled a complex (cast) part with Tet10 (10-nodes tetrahedal) volume elements, then meshed the surfaces with Tria6 (6-nodes surface elements) shell elements and merged the nodes of solid and surface meshes (including midside nodes).
The shell elements have a thickness of 0,001mm and the same material property as the volume elements.
I then compare the nodal output in solid and shell elements (unaveraged maximum value of strain and stress).
The max principal stress/strain distribution is the same in both solid and shell meshes, however the max stress value in the skin is slightly inferior to the max value at the corner of the solid elements (up to 1%, depending on mesh fineness)... Which one should I trust??...
Thanks for your help!
Simon