Shell 2
A beam twisted 90 degrees about its length is constrained on on e edge and has a point load prescribed normal to the opposite end of the beam.
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Shell 2
A beam twisted 90 degrees about its length is constrained on on e edge and has a point load prescribed normal to the opposite end of the beam.
*CONTROL_SHELL Twisted Cantilever Beam LS-DYNA Manual Section: *CONTROL_SHELL Example: Twisted Cantilever Beam Filename: control_shell.beam-twist.k Description: A beam twisted 90 degrees about its length is constrained on on e edge and has a point load prescribed normal to the opposite end of the beam. Model: The beam measures 12.00 * 1.10 * 0.32 cubic inches. A concentrated load is applied to one node on the end in the x-direction and the other node on the end in the z-direction. Input: This model uses the Hughes-Liu five through the thickness integration points (*CONTROL_SHELL, *SECTI ON_SHELL). The element has the shell normal update calculation performed at each nodal fiber every cycle (*CONTROL_SHELL). Note: This is another example that will not work correctly with the B-T shell formulation (unless warping stiffness is added). Results: The beam oscillates about a neutral amplitude. Reference: Belytschko, Wang and Chiang.
*CONTROL_OUTPUT *CONTROL_SHELL *CONTROL_TERMINATION *DATABASE_BINARY_D3PLOT *DATABASE_BINARY_D3THDT *DATABASE_BNDOUT *DATABASE_EXTENT_BINARY *DATABASE_GLSTAT *DATABASE_HISTORY_NODE *DATABASE_NODOUT *DEFINE_CURVE *ELEMENT_SHELL *END *KEYWORD *LOAD_NODE_POINT *MAT_ELASTIC *NODE *PART *SECTION_SHELL *TITLE
*KEYWORD *TITLE Twisted Beam $ $ LSTC Example $ $ Last Modified: September 15, 1997 $ $ Units: lbf-s2/in, in, s, lbf, psi, lbf-in $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $$$$ Control Ouput $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $...>....1....>....2....>....3....>....4....>....5....>....6....>....7....>....8 $ *CONTROL_TERMINATION $ endtim endcyc dtmin endneg endmas 0.018 $ *CONTROL_OUTPUT $ npopt neecho nrefup iaccop opifs ipnint ikedit 0 0 0 0 2 1000 $ *CONTROL_SHELL $ wrpang itrist irnxx istupd theory bwc miter -2 1 $ $ *DATABASE_EXTENT_BINARY $ neiph neips maxint strflg sigflg epsflg rltflg engflg 4 $ cmpflg ieverp beamip $ *DATABASE_BINARY_D3PLOT $ dt lcdt 0.001 $ *DATABASE_BINARY_D3THDT $ dt lcdt 0.0001 $ *DATABASE_BNDOUT $ dt 0.0001 $ *DATABASE_GLSTAT $ dt 0.0001 $ *DATABASE_NODOUT $ dt 0.0001 $ *DATABASE_HISTORY_NODE $ id1 id2 id3 id4 id5 id6 id7 id8 37 $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $$$$ Loading $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $$$$ Load node 37, 38, 39 with 0.1667 lbs in both x and y direction. $ $...>....1....>....2....>....3....>....4....>....5....>....6....>....7....>....8 $ *LOAD_NODE_POINT $ nid dof lcid sf cid m1 m2 m3 37 1 1 1.667E-01 38 1 1 1.667E-01 39 1 1 1.667E-01 37 2 1 1.667E-01 38 2 1 1.667E-01 39 2 1 1.667E-01 $ *DEFINE_CURVE $ lcid sidr scla sclo offa offo 1 $ a o 0.000E+00 1.000E+00 1.000E+03 1.000E+00 $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $$$$ Define Parts and Materials $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $...>....1....>....2....>....3....>....4....>....5....>....6....>....7....>....8 $ *PART $ pid sid mid eosid hgid adpopt Twisted Beam 1 1 1 $ $ *MAT_ELASTIC $ mid ro e pr da db 1 2.00e-4 29.00e+6 0.330 $ $ *SECTION_SHELL $ sid elform shrf nip propt qr/irid icomp 1 0 4 0 $ t1 t2 t3 t4 nloc 0.320 0.320 0.320 0.320 $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $$$$ Define Nodes and Elements $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $$$$ Nodes 1, 2, 3 have fixed boundary conditions. $ $ *END