*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