*Heading static test of shell to solid coupling ** Job name: xshell2solid_s8r_c3d10_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 15, -0.5, 0., 1. 16, -0.3331328, 0.125, 0.439443 17, -0.3331328, 0., 1.439443 18, -0.3331328, 0.125, 1.439443 19, -0.5, 0., 2. 20, -0.5, 0.125, 1. 21, -0.5, 0., 0. 22, -0.5, -0.125, 1. 23, -0.3331328, 0., 0.439443 24, -0.1668672, -0.125, 0.439443 25, -0.1668672, -0.125, 1.439443 26, 0., 0., 0.8788859 27, -0.08313281, 0., 1.439443 28, -0.25, -0.125, 2. 29, -0.25, 0., 2. 30, 0.08313281, -0.125, 1.439443 31, -0.25, 0.125, 0. 32, -0.08313281, 0.125, 0.439443 33, -0.08313281, 0., 0.439443 34, 0., 0., 0. 35, -0.25, 0., 0. 36, 0.25, -0.125, 2. 37, 0.5, 0., 2. 38, 0.25, 0., 2. 39, 0.3331328, 0., 1.439443 40, 0.3331328, -0.125, 1.439443 41, -0.08313281, 0.125, 1.439443 42, 0., 0., 2. 43, -0.25, 0.125, 2. 44, 0.1668672, 0.125, 0.439443 45, 0.1668672, 0.125, 1.439443 46, 0.5, 0.125, 1. 47, 0.3331328, 0., 0.439443 48, 0.5, 0., 1. 49, 0.5, 0., 0. 50, 0.3331328, -0.125, 0.439443 51, 0.25, 0., 0. 52, 0.08313281, -0.125, 0.439443 53, 0.25, -0.125, 0. 54, 0.5, -0.125, 1. 55, -0.25, -0.125, 0. 56, 0.25, 0.125, 0. 57, 0.25, 0.125, 2. *Element, type=C3D10I 1, 3, 14, 1, 4, 17, 16, 15, 19, 18, 20 2, 3, 2, 1, 14, 22, 21, 15, 17, 23, 16 3, 3, 2, 14, 13, 22, 23, 17, 25, 24, 26 4, 3, 10, 14, 4, 28, 27, 17, 19, 29, 18 5, 3, 14, 10, 13, 17, 27, 28, 25, 26, 30 6, 12, 14, 1, 9, 32, 16, 31, 34, 33, 35 7, 10, 7, 6, 13, 38, 37, 36, 30, 39, 40 8, 10, 14, 4, 11, 27, 18, 29, 42, 41, 43 9, 8, 7, 14, 13, 46, 45, 44, 47, 39, 26 10, 8, 5, 7, 13, 49, 48, 46, 47, 50, 39 11, 8, 13, 9, 5, 47, 52, 51, 49, 50, 53 12, 6, 7, 5, 13, 37, 48, 54, 40, 39, 50 13, 1, 9, 14, 2, 35, 33, 16, 21, 55, 23 14, 14, 13, 2, 9, 26, 24, 23, 33, 52, 55 15, 9, 13, 8, 14, 52, 47, 51, 33, 26, 44 16, 9, 14, 8, 12, 33, 44, 51, 34, 32, 56 17, 14, 10, 7, 11, 27, 38, 45, 41, 42, 57 18, 14, 7, 10, 13, 45, 38, 27, 26, 39, 30 ** 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. 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, 6, 7, 10, 11, 19, 28, 29, 36, 37, 38, 42, 43, 57 *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=_G11a, internal, instance=Part-2-1 27, 31 *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, 19, 28, 29, 36, 37, 38, 42, 43, 57 *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, 19, 28, 29, 36, 37, 38, 42, 43, 57 *Elset, elset=_G19, internal, instance=Part-1-1 4, 7, 8, 17 *Nset, nset=_G20, internal, instance=Part-2-1 2, 3, 6, 27, 31 *Elset, elset=_G20, internal, instance=Part-2-1 4, 5 *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 bend - perturbation *Static ** ** BOUNDARY CONDITIONS ** ** Name: BC-1 Type: Displacement/Rotation *Boundary _G9, 1, 1 _G9, 2, 2 _G9, 3, 3 ** ** LOADS ** ** Name: Load-1 Type: Concentrated force *Cload _G10, 2, -3.75 _G11, 2, -7.5 _G11a, 2, -15. ** ** 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, perturbation pull - perturbation *Static ** ** BOUNDARY CONDITIONS ** ** Name: BC-2 Type: Displacement/Rotation *Boundary _G18, 1, 1 _G18, 2, 2 _G18, 3, 3 ** ** LOADS ** ** Name: Load-3 Type: Concentrated force *Cload _G10, 1, 3.75 _G11, 1, 7.5 _G11a, 1, 15. ** ** 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 *End Step ** ---------------------------------------------------------------- ** ** STEP: Step-3 ** *Step, name=Step-3, nlgeom bend - nonlinear *Static 0.25, 1., 1e-05, 1. ** ** BOUNDARY CONDITIONS ** ** Name: BC-3 Type: Displacement/Rotation *Boundary _G19, 1, 1 _G19, 2, 2 _G19, 3, 3 ** ** LOADS ** ** Name: Load-5 Type: Concentrated force *Cload _G10, 2, -3.75 _G11, 2, -7.5 _G11a, 2, -15. ** ** 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-4 ** *Step, name=Step-4, nlgeom pull - nonlinear *Static 0.25, 1., 1e-05, 1. ** ** LOADS ** *Cload, Op = new _G10, 1, 3.75 _G11, 1, 7.5 _G11a, 1, 15. ** Name: Load-5 Type: Concentrated force ** ** 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-5 ** *Step, name=Step-5, nlgeom unload *Static 1., 1., 1e-05, 1. ** ** LOADS ** ** Name: Load-7 Type: Concentrated force *Cload, op=NEW ** Name: Load-8 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 ** ---------------------------------------------------------------- ** ** STEP: Step-6 ** *Step, name=Step-6, nlgeom rigid rotation *Static 0.04, 1., 1e-05, 1. ** ** BOUNDARY CONDITIONS ** ** Name: BC-3 Type: Displacement/Rotation *Boundary, op=NEW ** Name: BC-4 Type: Displacement/Rotation *Boundary, op=NEW _G20, 1, 1 _G20, 2, 2 _G20, 3, 3 _G20, 6, 6, -1.5708 ** ** OUTPUT REQUESTS ** *Restart, write, frequency=1 ** ** FIELD OUTPUT: F-Output-2 ** *Output, field *Node Output U, *Element Output S, ** ** HISTORY OUTPUT: H-Output-2 ** *Output, history, variable=PRESELECT *End Step