Oasys LS-DYNA Environment 8.1 VOLUME 3 ... - Oasys Software

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Oasys LS-DYNA Environment: User Guide (Version 8.1) List of first LS-DYNA input deck: *KEYWORD *TITLE BILLET FORGE $ $================================ CONTROL CARDS ================================ $ *CONTROL_TERMINATION $ [1] Termination time [2] Termination Cycle [3] Minimum timestep scale factor $ [4] % Energy change for termination [5] % Mass change for termination $ 1 ][ 2 ][ 3 ][ 4 ][ 5 ] 1.500E-03 0 .000E+00 .000E+00 .000E+00 *CONTROL_SHELL $ [1] Shell warpage angle [2] Automatic sorting of triangles [3] Hughes-Liu $ update option [4] Shell thickness change option [5] Shell theory [6] Warping $ stiffness [7] Plane stress plasticity option $ 1 ][ 2 ][ 3 ][ 4 ][ 5 ][ 6 ][ 7 ] .000E+00 0 0 0 0 0 0 *CONTROL_CONTACT $ [1] Interface penalty scale factor [2] Rigid wall penalty scale factor $ [3] Initial penetration check [4] Shell thickness in type 3,5,10 contacts [5] $ Penalty stiffness option [6] Consider shell thickness change (single surface $ contact) [7] Automatic reorientation of interface segments $ 1 ][ 2 ][ 3 ][ 4 ][ 5 ][ 6 ][ 7 ] .000E+00 .000E+00 0 0 1 0 0 $ [1] Storage per contact surface [2] Storage per user defined friction $ [3] Timesteps between bucket searches [4] Intermittent searching [5] Search $ multiplier [6] Shell thickness logic [7] Timstep override for eroding contacts $ 1 ][ 2 ][ 3 ][ 4 ][ 5 ][ 6 ][ 7 ] 0 0 0 0 .000E+00 *CONTROL_ENERGY $ [1] Compute hourglass energy [2] Compute stonewall energy dissipation $ [3] Compute sliding interface energy [4] Compute Rayleigh energy dissipation $ 1 ][ 2 ][ 3 ][ 4 ] 0 0 0 0 *CONTROL_DAMPING $ [1] No cycles between convergence checks [2] DR convergence tolerance [3] DR $ damping factor [4] DR Optional termination time [5] Scale factor for DR time $ step [6] Automatic control for DR option [7] Convergence tolerance for $ automatic DR [8] DR flag for stress initialization $ 1 ][ 2 ][ 3 ][ 4 ][ 5 ][ 6 ][ 7 ][ 8 ] 0 .000E+00 .000E+00 .000E+00 .000E+00 0 .000E+00 0 *CONTROL_OUTPUT $ [1] Print suppression during input phase [2] Print suppression for echo file $ [3] Update beam reference nodes [4] Average accelerations from velocities $ [5] Output interval for interface file [6] Print all element initial timestep $ [7] Number of cycles between output to otf file $ 1 ][ 2 ][ 3 ][ 4 ][ 5 ][ 6 ][ 7 ] 0 0 0 0 .000E+00 0 0 *CONTROL_TIMESTEP $ [1] Initial timestep size [2] Scale factor for computed timestep [3] Basis of $ timestep size calculation [4] Minimum timestep for shell elements [5] Timestep $ size for mass scaled solution [6] Load curve number that limits time step $ [7] Erode solids and shells when minimum timestep reached $ 1 ][ 2 ][ 3 ][ 4 ][ 5 ][ 6 ][ 7 ] .000E+00 .000E+00 0 .000E+00 1.200E-07 0 0 0 $ $================================ DATABASE CARDS =============================== $ *DATABASE_RCFORC 7.333E-06 *DATABASE_BINARY_D3PLOT 7.333E-05 0 1 *DATABASE_BINARY_XTFILE *DATABASE_BINARY_D3THDT 2.200E-02 0 *DATABASE_BINARY_D3DUMP 0 *DATABASE_BINARY_RUNRSF 0 *DATABASE_BINARY_INTFOR 7.333E-05 0 *DATABASE_EXTENT_BINARY 0 0 0 0 0 0 0 0 0 0 0 $ $============================ MATERIAL PROPERTIES ============================== $ Page A.128
Oasys LS-DYNA Environment: User Guide (Version 8.1) *MAT_PIECEWISE_LINEAR_PLASTICITY $ Material 1 : BILLET - ALUMINUM 1 2.500E-04 1.000E+07 .3300 .000E+00 .000E+00 .000E+00 .000E+00 .000E+00 .000E+00 .0 .0 .000E+00 5.000E-03 1.000E-02 5.000E-02 1.000E-01 2.000E-01 7.000E-01 4.000E+00 4.785E+03 6.505E+03 7.423E+03 1.063E+04 1.254E+04 1.482E+04 2.010E+04 3.081E+04 $------------------------------------------------------------------------------- *MAT_RIGID $ Material 2 : PRESS - ALUMINUM 2 2.500E-04 1.000E+07 .3300 .0 .0 .0 -1.0 .0 110111.0 .000E+00 .000E+00 .000E+00 .000E+00 .000E+00 .000E+00 $ $============================= SECTION PROPERTIES ============================== $ *SECTION_SOLID $ Section 1 : BILLET - ALUMINUM 1 0 $------------------------------------------------------------------------------- *SECTION_SHELL $ Section 2 : PRESS - ALUMINUM 2 0 .00000 .0 .0 .0 0 1.000E-02 1.000E-02 1.000E-02 1.000E-02 .000E+00 $ $============================== PART DEFINITIONS =============================== $ *PART BILLET - ALUMINUM 1 1 1 0 0 0 $------------------------------------------------------------------------------- *PART PRESS - ALUMINUM 2 2 2 0 0 0 $ $=================================== NODES ===================================== $ *NODE $ ID X COORDINATE Y COORDINATE Z COORDINATE TRANS ROT 1 .00000000E+00 .00000000E+00 .00000000E+00 0 0 ... 5755 .10646980E+01 .90907520E+00 .11260000E+01 0 0 $ $================================== ELEMENTS =================================== $ *ELEMENT_SOLID $ ID PART NODE 1 NODE 2 NODE 3 NODE 4 NODE 5 NODE 6 NODE 7 NODE 8 1 1 1 2 11 10 82 83 92 91 ... 4576 1 5309 5310 3645 3636 5381 5382 3726 3717 *ELEMENT_SHELL $ ID PART NODE 1 NODE 2 NODE 3 NODE 4 1 2 5383 5394 5395 5384 ... 340 2 5754 5624 5635 5755 $ $============================ BOUNDARY CONDITIONS ============================== $ *BOUNDARY_SPC_NODE $ NODE COORD-SYS X-TRANS Y-TRANS Z-TRANS X-ROT Y-ROT Z-ROT 1 1 1 1 1 1 1 1 ... 5319 1 0 1 0 1 0 1 *DEFINE_COORDINATE_SYSTEM 1 .0 .0 .0 1.0 .0 .0 .0 1.0 .0 *BOUNDARY_PRESCRIBED_MOTION_RIGID $ PART ID DOF TYPE CURVE ID FACTOR VECT ID 2 3 0 1 1.000E+00 0 .000E+00 $ $================================= CONSTRAINTS ================================= $ $ $================================= RIGID WALLS ================================= $ $ $============================== INITIAL CONDITIONS ============================= $ $ $============================== CONTACT SURFACES =============================== $ *CONTACT_NODES_TO_SURFACE_TITLE Page A.129
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