*Heading static test of shell to solid coupling ** Job name: xshell2solid_dyn_s4r_c3d4_std Model name: Model-1 ** ** PARTS ** *Part, name=Part-1 *End Part *Part, name=Part-2 *End Part ** ** ASSEMBLY ** *Assembly, name=Assembly ** *Instance, name=Part-1-1, part=Part-1 0., -3.06151588455594e-17, -2.22044604925031e-16 0., -3.06151588455594e-17, -2.22044604925031e-16, 0., -1., -2.22044604925031e-16, 90. *Node 1, -0.5, 0.125, 0. 2, -0.5, -0.125, 0. 3, -0.5, -0.125, 2. 4, -0.5, 0.125, 2. 5, 0.5, -0.125, 0. 6, 0.5, -0.125, 2. 7, 0.5, 0.125, 2. 8, 0.5, 0.125, 0. 9, 0., -0.125, 0. 10, 0., -0.125, 2. 11, 0., 0.125, 2. 12, 0., 0.125, 0. 13, 0.1662656, -0.125, 0.8788859 14, -0.1662656, 0.125, 0.8788859 *Element, type=C3D4 1, 3, 14, 1, 4 2, 3, 2, 1, 14 3, 3, 2, 14, 13 4, 3, 10, 14, 4 5, 3, 14, 10, 13 6, 12, 14, 1, 9 7, 10, 7, 6, 13 8, 10, 14, 4, 11 9, 8, 7, 14, 13 10, 8, 5, 7, 13 11, 8, 13, 9, 5 12, 6, 7, 5, 13 13, 1, 9, 14, 2 14, 14, 13, 2, 9 15, 9, 13, 8, 14 16, 9, 14, 8, 12 17, 14, 10, 7, 11 18, 14, 7, 10, 13 ** Region: (Section-1:Picked) *Elset, elset=_I1, internal, generate 1, 18, 1 ** Section: Section-1 *Solid Section, elset=_I1, material=Material-1 1., *End Instance ** *Instance, name=Part-2-1, part=Part-2 0., 0., 0. 0., 0., 0., 1., 0., 0., 90. *Node 1, 0., 0., 0. 2, 8., 0., 0. 3, 8., 0.5, 0. 4, 0., 0.5, 0. 5, 0., -0.5, 0. 6, 8., -0.5, 0. 7, 2., 0., 0. 8, 4., 0., 0. 9, 6., 0., 0. 10, 6., 0.5, 0. 11, 4., 0.5, 0. 12, 2., 0.5, 0. 13, 2., -0.5, 0. 14, 4., -0.5, 0. 15, 6., -0.5, 0. *Element, type=S4R 1, 1, 7, 12, 4 2, 7, 8, 11, 12 3, 8, 9, 10, 11 4, 9, 2, 3, 10 5, 2, 9, 15, 6 6, 9, 8, 14, 15 7, 8, 7, 13, 14 8, 7, 1, 5, 13 ** Region: (Section-2:Picked) *Elset, elset=_I1, internal, generate 1, 8, 1 ** Section: Section-2 *Shell Section, elset=_I1, material=Material-1 0.25, 3 *End Instance *Nset, nset=_G9, internal, instance=Part-1-1 3, 4, 6, 7, 10, 11 *Elset, elset=_G9, internal, instance=Part-1-1 4, 7, 8, 17 *Nset, nset=_G10, internal, instance=Part-2-1 3, 6 *Nset, nset=_G11, internal, instance=Part-2-1 2, *Nset, nset=_G12, internal, instance=Part-2-1 3, 6 *Nset, nset=_G13, internal, instance=Part-2-1 2, *Nset, nset=_G14, internal, instance=Part-2-1 3, 6 *Nset, nset=_G15, internal, instance=Part-2-1 2, *Nset, nset=_G16, internal, instance=Part-2-1 3, 6 *Nset, nset=_G17, internal, instance=Part-2-1 2, *Nset, nset=_G18, internal, instance=Part-1-1 3, 4, 6, 7, 10, 11 *Elset, elset=_G18, internal, instance=Part-1-1 4, 7, 8, 17 *Nset, nset=_G19, internal, instance=Part-1-1 3, 4, 6, 7, 10, 11 *Elset, elset=_G19, internal, instance=Part-1-1 4, 7, 8, 17 *Nset, nset=_G20, internal, instance=Part-2-1 2, 3, 6 *Elset, elset=_G20, internal, instance=Part-2-1 4, 5 *Nset, nset=_G21, internal, instance=Part-1-1 3, 6, 10 *Elset, elset=_Surf-1_S4, internal, instance=Part-1-1, generate 6, 16, 5 *Elset, elset=_Surf-1_S2, internal, instance=Part-1-1 13, *Surface, type=ELEMENT, name=Surf-1 _Surf-1_S4, S4 _Surf-1_S2, S2 *Elset, elset=_Surf-2_E4, internal, instance=Part-2-1 1, *Elset, elset=_Surf-2_E2, internal, instance=Part-2-1 8, *Surface, type=ELEMENT, name=Surf-2 _Surf-2_E4, E4 _Surf-2_E2, E2 ** Constraint: Constraint-1 *Shell to solid coupling, constraint name=Constraint-1 Surf-2, Surf-1 *End Assembly ** ** MATERIALS ** *Material, name=Material-1 *Density 1700., *Elastic 3e+07, 0.3 ** ---------------------------------------------------------------- ** ** STEP: Step-1 ** *Step, name=Step-1, perturbation frequency analysis *Frequency, eigensolver = lanczos 4, , ** ** BOUNDARY CONDITIONS ** ** Name: BC-1 Type: Displacement/Rotation *Boundary _G10, 1, 6 _G11, 1, 6 ** ** OUTPUT REQUESTS ** *Restart, write, frequency=0 ** ** FIELD OUTPUT: F-Output-1 ** *Output, field *Node Output U, *Element Output S, ** ** HISTORY OUTPUT: H-Output-1 ** *Output, history, variable=PRESELECT *El Print, freq=999999 *Node Print, freq=999999 *End Step ** ---------------------------------------------------------------- ** ** STEP: Step-2 ** *Step, name=Step-2, nlgeom bend - nonlinear *Static 0.25, 1., 1e-05, 1. ** ** BOUNDARY CONDITIONS ** ** Name: BC-3 Type: Displacement/Rotation *Boundary _G14, 1, 6 _G15, 1, 6 ** ** LOADS ** ** Name: Load-5 Type: Concentrated force *Cload _G21, 2, -60. ** ** OUTPUT REQUESTS ** *Restart, write, frequency=0 ** ** FIELD OUTPUT: F-Output-2 ** *Output, field *Node Output U, *Element Output S, ** ** HISTORY OUTPUT: H-Output-2 ** *Output, history, variable=PRESELECT *End Step ** ---------------------------------------------------------------- ** ** STEP: Step-3 ** *Step, name=Step-3, nlgeom dynamic analysis *Dynamic, haftol=3e4 0.1, 20.,,2. ** ** LOADS ** ** Name: Load-5 Type: Concentrated force *Cload, op=NEW ** ** OUTPUT REQUESTS ** *Restart, write, frequency=0 ** ** FIELD OUTPUT: F-Output-2 ** *Output, field *Node Output U, *Element Output S, ** ** HISTORY OUTPUT: H-Output-2 ** *Output, history, variable=PRESELECT *End Step