*Heading dynamic test of shell to solid coupling ** Job name: xshell2solid_dyn_s8r_c3d8_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., 0.125, 0. 6, 0., -0.125, 0. 7, 0., 0.125, 2. 8, 0., -0.125, 2. 9, 0.5, 0.125, 0. 10, 0.5, -0.125, 0. 11, 0.5, 0.125, 2. 12, 0.5, -0.125, 2. *Element, type=C3D8 1, 5, 6, 8, 7, 1, 2, 4, 3 2, 9, 10, 12, 11, 5, 6, 8, 7 ** Region: (Section-1:Picked) *Elset, elset=_I1, internal 1, 2 ** 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. 16, 1., 0., 0. 17, 2., 0.25, 0. 18, 1., 0.5, 0. 19, 0., 0.25, 0. 20, 3., 0., 0. 21, 4., 0.25, 0. 22, 3., 0.5, 0. 23, 5., 0., 0. 24, 6., 0.25, 0. 25, 5., 0.5, 0. 26, 7., 0., 0. 27, 8., 0.25, 0. 28, 7., 0.5, 0. 29, 6., -0.25, 0. 30, 7., -0.5, 0. 31, 8., -0.25, 0. 32, 4., -0.25, 0. 33, 5., -0.5, 0. 34, 2., -0.25, 0. 35, 3., -0.5, 0. 36, 0., -0.25, 0. 37, 1., -0.5, 0. *Element, type=S8R 1, 1, 7, 12, 4, 16, 17, 18, 19 2, 7, 8, 11, 12, 20, 21, 22, 17 3, 8, 9, 10, 11, 23, 24, 25, 21 4, 9, 2, 3, 10, 26, 27, 28, 24 5, 2, 9, 15, 6, 26, 29, 30, 31 6, 9, 8, 14, 15, 23, 32, 33, 29 7, 8, 7, 13, 14, 20, 34, 35, 32 8, 7, 1, 5, 13, 16, 36, 37, 34 ** 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, 7, 8, 11, 12 *Elset, elset=_G9, internal, instance=Part-1-1 1, 2 *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, 7, 8, 11, 12 *Elset, elset=_G18, internal, instance=Part-1-1 1, 2 *Nset, nset=_G19, internal, instance=Part-1-1 3, 4, 7, 8, 11, 12 *Elset, elset=_G19, internal, instance=Part-1-1 1, 2 *Nset, nset=_G20, internal, instance=Part-2-1 2, 3, 6, 27, 31 *Nset, nset=_G21, internal, instance=Part-1-1 4, 8, 12 *Elset, elset=_G20, internal, instance=Part-2-1 4, 5 *Elset, elset=_Surf-1_S3, internal, instance=Part-1-1 1, 2 *Surface, type=ELEMENT, name=Surf-1 _Surf-1_S3, S3 *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 *Controls,Parameters=field ,0.0, *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