*Heading
** traction loading for axisymmetric shells
*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.,           1.
      2,    0.1423148,    0.9898214
      3,    0.2817326,     0.959493
      4,     0.415415,     0.909632
      5,    0.5406408,    0.8412535
      6,    0.6548607,    0.7557496
      7,    0.7557496,    0.6548607
      8,    0.8412535,    0.5406408
      9,     0.909632,     0.415415
     10,     0.959493,    0.2817326
     11,    0.9898214,    0.1423148
     12,           1.,           0.
     13,   0.07133918,    0.9974521
     14,    0.2125653,    0.9771469
     15,    0.3494642,    0.9369497
     16,     0.479249,     0.877679
     17,    0.5992777,    0.8005412
     18,    0.7071068,    0.7071068
     19,    0.8005412,    0.5992777
     20,     0.877679,     0.479249
     21,    0.9369497,    0.3494642
     22,    0.9771469,    0.2125653
     23,    0.9974521,   0.07133918
*Element, type=SAX2
 1,  1, 13,  2
 2,  2, 14,  3
 3,  3, 15,  4
 4,  4, 16,  5
 5,  5, 17,  6
 6,  6, 18,  7
 7,  7, 19,  8
 8,  8, 20,  9
 9,  9, 21, 10
10, 10, 22, 11
11, 11, 23, 12
** Region: (Section-1:Picked)
*Elset, elset=_PickedSet2, internal, generate
  1,  11,   1
** Section: Section-1
*Shell Section, elset=_PickedSet2, material=Material-1
0.2, 5
*End Instance
**  
*Instance, name=Part-1-2, part=Part-1
          0.,         1.32,           0.
*Node
      1,           0.,           1.
      2,    0.1423148,    0.9898214
      3,    0.2817326,     0.959493
      4,     0.415415,     0.909632
      5,    0.5406408,    0.8412535
      6,    0.6548607,    0.7557496
      7,    0.7557496,    0.6548607
      8,    0.8412535,    0.5406408
      9,     0.909632,     0.415415
     10,     0.959493,    0.2817326
     11,    0.9898214,    0.1423148
     12,           1.,           0.
*Element, type=SAX1
 1,  1,  2
 2,  2,  3
 3,  3,  4
 4,  4,  5
 5,  5,  6
 6,  6,  7
 7,  7,  8
 8,  8,  9
 9,  9, 10
10, 10, 11
11, 11, 12
** Region: (Section-1:Picked)
*Elset, elset=_PickedSet2, internal, generate
  1,  11,   1
** Section: Section-1
*Shell Section, elset=_PickedSet2, material=Material-1
0.2, 5
*End Instance
**  
*Nset, nset=_PickedSet6, internal, instance=Part-1-1
 12,
*Nset, nset=_PickedSet6, internal, instance=Part-1-2
 12,
*Elset, elset=_Surf-1_SNEG, internal, instance=Part-1-1, generate
  1,  11,   1
*Elset, elset=_Surf-1_SNEG, internal, instance=Part-1-2, generate
  1,  11,   1
*Surface, type=ELEMENT, name=Surf-1
_Surf-1_SNEG, SNEG
*End Assembly
** 
** MATERIALS
** 
*Material, name=Material-1
*Density
 0.0001,
*Elastic
1000., 0.3
** ----------------------------------------------------------------
** 
** STEP: Step-1
** 
*Step, name=Step-1, nlgeom=YES, unsymm=YES
*Static
0.1, 1., 1e-05, 1.
*Controls, parameters=field
 1.0E-6, 
** 
** BOUNDARY CONDITIONS
** 
** Name: BC-1 Type: Displacement/Rotation
*Boundary
_PickedSet6, 2, 2
_PickedSet6, 6, 6
** 
** LOADS
** 
** Name: Load-1   Type: Surface traction
*Dsload
Surf-1, TRVEC, 50., 0.707107, 0.707107, 0.
** 
** OUTPUT REQUESTS
** 
** 
** FIELD OUTPUT: F-Output-1
** 
*Output, field
*Node output
u,rf
*End Step