*Heading
** traction loading for axisymmetric element.
*Preprint, echo=NO, model=NO, history=NO, contact=NO
**
** PARTS
**
*Part, name=Part-1
*End Part
**
** ASSEMBLY
**
*Assembly, name=Assembly
**
*Instance, name=Part-1-1, part=Part-1
*Node
1, 0., 0.5
2, 0., -0.5
3, 1., -0.5
4, 1., 0.5
5, 0., 0.
6, 0.5, -0.5
7, 1., 0.
8, 0.5, 0.5
9, 0.5, 0.05618608
10, 0.5, -0.221907
11, 0.75, -0.25
12, 0.75, 0.02809304
13, 0.25, 0.02809304
14, 0.25, -0.25
15, 0., -0.25
16, 0.25, -0.5
17, 0.75, -0.5
18, 1., -0.25
19, 0.75, 0.278093
20, 0.75, 0.5
21, 0.5, 0.278093
22, 0.25, 0.278093
23, 0., 0.25
24, 1., 0.25
25, 0.25, 0.5
*Element, type=CAX6M
1, 9, 6, 7, 10, 11, 12
2, 9, 5, 6, 13, 14, 10
3, 5, 2, 6, 15, 16, 14
4, 6, 3, 7, 17, 18, 11
5, 9, 4, 8, 19, 20, 21
6, 9, 1, 5, 22, 23, 13
7, 9, 7, 4, 12, 24, 19
8, 9, 8, 1, 21, 25, 22
** Region: (Section-1:Picked)
*Elset, elset=_PickedSet2, internal, generate
1, 8, 1
** Section: Section-1
*Solid Section, elset=_PickedSet2, material=Material-1
1.,
*End Instance
**
*Instance, name=Part-1-1-1-2, part=Part-1
0., 2., 0.
*Node
1, 0., 0.5
2, 0., 0.
3, 0., -0.5
4, 0.5, 0.5
5, 0.5, 0.
6, 0.5, -0.5
7, 1., 0.5
8, 1., 0.
9, 1., -0.5
*Element, type=CAX4R
1, 1, 2, 5, 4
2, 2, 3, 6, 5
3, 4, 5, 8, 7
4, 5, 6, 9, 8
** Region: (Section-1:Picked)
*Elset, elset=_PickedSet2, internal, generate
1, 4, 1
** Section: Section-1
*Solid Section, elset=_PickedSet2, material=Material-1
1.,
*End Instance
**
*Instance, name=Part-1-1-1-3, part=Part-1
0., 4., 0.
*Node
1, 0., 0.5
2, 0., -0.5
3, 1., -0.5
4, 1., 0.5
5, 0., 0.
6, 0.5, -0.5
7, 1., 0.
8, 0.5, 0.5
9, 0.5, 0.05618608
*Element, type=CAX3
1, 9, 6, 7
2, 9, 5, 6
3, 5, 2, 6
4, 6, 3, 7
5, 9, 4, 8
6, 9, 1, 5
7, 9, 7, 4
8, 9, 8, 1
** Region: (Section-1:Picked)
*Elset, elset=_PickedSet2, internal, generate
1, 8, 1
** Section: Section-1
*Solid Section, elset=_PickedSet2, material=Material-1
1.,
*End Instance
*Nset, nset=boun, instance=Part-1-1
2, 3, 6, 16, 17
*Nset, nset=boun, instance=Part-1-1-1-2, generate
3, 9, 3
*Nset, nset=boun, instance=Part-1-1-1-3
2, 3, 6
*Elset, elset=boun, instance=Part-1-1
3, 4
*Elset, elset=boun, instance=Part-1-1-1-2
2, 4
*Elset, elset=boun, instance=Part-1-1-1-3
3, 4
*Elset, elset=_Surf-1_S2, internal, instance=Part-1-1-1-3
5, 8
*Surface, type=ELEMENT, name=Surf-1
_Surf-1_S2, S2
*Elset, elset=_Surf-2_S3, internal, instance=Part-1-1-1-2
3, 4
*Surface, type=ELEMENT, name=Surf-2
_Surf-2_S3, S3
*Elset, elset=_Surf-3_S2, internal, instance=Part-1-1
4, 7
*Surface, type=ELEMENT, name=Surf-3
_Surf-3_S2, S2
*End Assembly
*Amplitude, name=Amp-1
0., 0., 1., 1.
**
** MATERIALS
**
*Material, name=Material-1
*Density
0.0001,
*Elastic
1000., 0.3
** ----------------------------------------------------------------
**
** STEP: Step-1
**
*Step, name=Step-1
*Dynamic, Explicit
, 1.
*Bulk Viscosity
0.06, 1.2
**
** BOUNDARY CONDITIONS
**
** Name: BC-1 Type: Displacement/Rotation
*Boundary
boun, 2, 2
**
** LOADS
**
** Name: Load-1 Type: Surface traction
*Dsload, amplitude=Amp-1
Surf-1, TRVEC, 1., 0., -1., 0.
** Name: Load-2 Type: Surface traction
*Dsload, amplitude=Amp-1
Surf-2, TRVEC, 1.414, 0.707107, 0.707107, 0.
** Name: Load-3 Type: Surface traction
*Dsload, amplitude=Amp-1
Surf-3, TRSHR, 1., 0.707107, 0.707107, 0.
**
** OUTPUT REQUESTS
**
**
** FIELD OUTPUT: F-Output-1
**
*Output, field, number=6
*Element output
TRNOR,TRSHR
*Node output
U,RF
*End Step