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      Date: 04/13/2026      Time: 10:54:43  
      ___________________________________________________ 
     |                                                   |
     |  LS-DYNA, A Program for Nonlinear Dynamic         |
     |  Analysis of Structures in Three Dimensions       |
     |  Date    : 03/10/2022    Time: 06:59:30           |
     |  Version : smp d R13                              |
     |  Revision: R13.1-138-g8429c8a10f                  |
     |                                                   |
     |  Features enabled in this version:                |
     |    Shared Memory Parallel                         |
     |    CESE CHEMISTRY EM ICFD STOCHASTIC_PARTICLES    |
     |    FFTW (multi-dimensional FFTW Library)          |
     |    ARPACK (nonsymmetric eigensolver library)      |
     |    ANSYSLIC enabled                               |
     |                                                   |
     |  Licensed to: IFSTTAR Bron - - -- 1083027         |
     |  Issued by  : abby.merz_03122025                  |
     |  Commercial license                               |
     |                                                   |
     |  Platform   : WINDOWS X64                         |
     |  OS Level   : Windows 7/8/10 & Srv 2016/2019 com  |
     |  Compiler   : Intel Fortran XE 2019 MSVC++ 2019   |
     |  Hostname   : fbro-23-060                         |
     |  Precision  : Double precision (I8R8)             |
     |                                                   |
     |  Unauthorized use infringes Ansys Inc. copyrights |
     |___________________________________________________|


 Command line options: i=D:\Marc\Programmation\ls_toolbox\ls_toolbox\Example/Beam_3D_mesh_example_model.k 
                       ncpu=31 
                       memory=415m

 Input file: D:\Marc\Programmation\ls_toolbox\ls_toolbox\Example/Beam_3D_mesh_example_model.k

 The native file format       : 64-bit small endian
 Memory size from command line:   415000000

 ********  notice  ********  notice  ********  notice  ********
 *                                                            *
 * This is the LS-DYNA Finite Element code.                   *
 *                                                            *
 * Neither LST nor the authors assume any responsibility for  *
 * the validity, accuracy, or applicability of any results    *
 * obtained from this system. Users must verify their own     *
 * results.                                                   *
 *                                                            *
 * LST endeavors to make the LS-DYNA code as complete,        *
 * accurate and easy to use as possible.                      *
 * Suggestions and comments are welcomed.  Please report any  *
 * errors encountered in either the documentation or results  *
 * immediately to LST through your site focus.                *
 *                                                            *
 * Copyright (C) 1990-2022                                    *
 * by Ansys, Inc.                                             *
 * All rights reserved                                        *
 *                                                            *
 ********  notice  ********  notice  ********  notice  ********

 Beginning of keyword reader                                   04/13/26 10:54:43


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total # of *LOAD_BODY_Y............................       0
total # of *LOAD_BODY_Z............................       0
total # of *LOAD_BRODE.............................       0
total # of *LOAD_BLAST.............................       0
total # of *LOAD_BLAST_CLEARING....................       0
total # of *LOAD_BLAST_ENHANCED....................       0
total # of *LOAD_BLAST_SEGMENT.....................       0
total # of *LOAD_BLAST_SEGMENT_SET.................       0
total # of *LOAD_DENSITY_DEPTH.....................       0
total # of *LOAD_GRAVITY_PART......................       0
total # of *LOAD_HEAT_CONTROLLER...................       0
total # of *LOAD_HEAT_EXOTHERMIC_REACTION..........       0
total # of *LOAD_HEAT_GENERATION_SET...............       0
total # of *LOAD_HEAT_GENERATION_SOLID.............       0
total # of *LOAD_HEAT_GENERATION_SET_SHELL.........       0
total # of *LOAD_HEAT_GENERATION_SHELL.............       0
total # of *LOAD_MOVING_PRESSURE...................       0
total # of *LOAD_NODE..............................       0
total # of *LOAD_NODE_SET..........................       0
total # of *LOAD_NSG...............................       0
total # of *LOAD_PYRO_ACTUATOR.....................       0
total # of *LOAD_REMOVE_PART ......................       0
total # of *LOAD_SEGMENT...........................       0
total # of *LOAD_SEGMENT_FSILNK....................       0
total # of *LOAD_SEGMENT_NONUNIFORM................       0
total # of *LOAD_SEGMENT_SET.......................       0
total # of *LOAD_SEGMENT_SET_NONUNIFORM............       0
total # of *LOAD_SEISMIC_SSI_AUX...................       0
total # of *LOAD_SEISMIC_SSI_NODE..................       0
total # of *LOAD_SEISMIC_SSI_SET...................       0
total # of *LOAD_SEISMIC_SSI_POINT.................       0
total # of *LOAD_SEISMIC_SSI_DECONV................       0
total # of *LOAD_SHELL.............................       0
total # of *LOAD_SHELL_SET.........................       0
total # of *LOAD_STIFFEN_PART .....................       0
total # of *LOAD_SUPERPLASTIC_FORMING..............       0
total # of *LOAD_SURFACE_STRESS....................       0
total # of *LOAD_THERMAL_option_ELEMENT............       0
total # of *LOAD_THERMAL_option_NODE...............       0
total # of *LOAD_THERMAL_option....................       0
total # of *LOAD_THERMAL_LOAD_CURVE................       0
total # of *LOAD_THERMAL_TOPAZ ....................       0
total # of *LOAD_THERMAL_VARIABLE_SHELL_option.....       0
total # of *LOAD_THERMAL_VARIABLE_BEAM _option.....       0
total # of *LOAD_VIBRO_ACOUSTIC....................       0
total # of *LOAD_VOLUME_LOSS ......................       0
total # of *LSO_DOMAIN.............................       0
total # of *LSO_ID_SET.............................       0
total # of *LSO_POINT_SET..........................       0
total # of *LSO_REGION.............................       0
total # of *LSO_TIME_SEQUENCE......................       0
total # of *LSO_VARIABLE_GROUP.....................       0
total # of *MAT_option.............................       1
total # of *MAT_THERMAL_option.....................       0
total # of *MAT_NONLOCAL...........................       0
total # of *MESH_BL................................       0
total # of *MESH_BL_SYM............................       0
total # of *MESH_EMBEDSHELL........................       0
total # of *MESH_EMBEDSHELL........................       0
total # of *MESH_IMM_ELEMENT.......................       0
total # of *MESH_IMM_NODE..........................       0
total # of *MESH_NODE..............................       0
total # of *MESH_SIZE..............................       0
total # of *MESH_SIZE_SHAPE........................       0
total # of *MESH_SURFACE_ELEMENT...................       0
total # of *MESH_SURFACE_NODE......................       0
total # of *MESH_VOLUME............................       0
total # of *MESH_VOLUME_ELEMENT....................       0
total # of *MESH_VOLUME_NODE.......................       0
total # of *MESH_VOLUME_PART.......................       0
total # of *NODE...................................     160
total # of *NODE_MERGE.............................       0
total # of *NODE_MERGE_TOLERANCE...................       0
total # of *PART_option card.......................       1
total # of *PART_ANNEAL_option.....................       0
total # of *PARTICLE_GENERAL.......................       0
total # of *RIGIDWALL_option.......................       0
total # of *SECTION_option.........................       1
total # of *SENSOR_CONTROL.........................       0
total # of *SENSOR_DEFINE .........................       0
total # of *SENSOR_SWITCH .........................       0
total # of *SET_2D_SEGMENT.........................       0
total # of *SET_BEAM...............................       0
total # of *SET_BOX ...............................       0
total # of *SET_DISCRETE...........................       0
total # of *SET_MODE...............................       0
total # of *SET_NODE_option........................       2
total # of *SET_PART...............................       0
total # of *SET_POINT..............................       0
total # of *SET_SEGMENT............................       0
total # of *SET_SHELL_option.......................       0
total # of *SET_SOLID..............................       0
total # of *SET_TSHELL.............................       0
total # of *STOCHASTIC_SPRAY_PARTICLES.............       0
total # of *STOCHASTIC_TBX_PARTICLES...............       0
total # of *TERMINATION_BODY.......................       0
total # of *TERMINATION_DELETED_SHELLS.............       0
total # of *TERMINATION_DELETED_SOLIDS.............       0
total # of *TERMINATION_NODE.......................       0
total # of *TERMINATION_CONTACT....................       0
total # of *TITLE..................................       0
total # of *USER_INTERFACE_CONTROL.................       0
total # of *USER_INTERFACE_FRICTION................       0
total # of *USER_INTERFACE_FORCES..................       0
total # of *USER_INTERFACE_CONDUCTIVITY............       0
total # of *USER_LOAD..............................       0
total # of *USER_MATERIAL_VENDOR...................       0
total # of *USER_MATERIAL_LICENSE..................       0
total # of *USER_NONLOCAL_SEARCH...................       0
total # of *USER_PARAMETER.........................       0
total # of *CHANGE_BOUNDARY_CONDITIONS.............       0
total # of *CHANGE_CONTACT_SMALL_PENETRATION.......       0
total # of *CHANGE_RIGID_BODY_CONSTRAINTS..........       0
total # of *CHANGE_RIGID_BODY_INERTIA..............       0
total # of *CHANGE_THERMAL_PARAMETERS..............       0
total # of *CHANGE_VELOCITY_ZERO...................       0
total # of *CHANGE_VELOCITY_RIGID_BODY.............       0
total # of *DELETE_ALECPL..........................       0
total # of *DELETE_CONTACT.........................       0
total # of *DELETE_CONTACT_2DAUTO..................       0
total # of *DELETE_FSI.............................       0
total # of *DELETE_ENTITY..........................       0
total # of *DELETE_ELEMENT_SOLID...................       0
total # of *DELETE_ELEMENT_BEAM....................       0
total # of *DELETE_ELEMENT_SHELL...................       0
total # of *DELETE_ELEMENT_TSHELL..................       0
total # of *DELETE_PART............................       0
total # of *RIGID_DEFORMABLE_CONTROL...............       0
total # of *RIGID_DEFORMABLE_D2R...................       0
total # of *RIGID_DEFORMABLE_R2D...................       0
total # of *STRESS_INITIALIZATION..................       0

 Memory required to process keyword     :     224878  
 Additional dynamic memory required     :    2056663  


 LS-DYNA will perform a structural only analysis 



                                                                         
            code input version =1993
            formats            =mlarg



    IMPLICIT CONTROL CARD 1.  General Data

    implicit/explicit switching flag ..............       1
          eq.0: explicit analysis                       
          eq.1: implicit analysis                       
          eq.2: explicit, then seamless springback      
          eq.4: implicit with automatic implicit/explicit switching
          eq.5: implicit with automatic implicit/explicit switching
                with mandatory implicit finish                     
          eq.6: explicit with intermittent eigenvalues  
          eq.-n: load curve n gives flag vs. time       

    initial time step for implicit solution .......    0.5000E+00
          lt.0: absolute value is time step,             
                negative principal stresses eliminated in
                geometric (initial stress) stiffness     

    element formulation after switching ...........       2
          eq.1: switch to fully integrated element      
          eq.2: retain element formulation              

    number of steps for nonlinear springback ......       1

    geometric (initial stress) stiffness flag .....       2
          lt.0: absolute value is part set for apply    
          eq.1: include                                 
          eq.2: ignore                                  

    consistent tangential stiffness flag ..........       0
          eq.0: do not use                              
          eq.1: use                                     

    displacement termination tolerance 1 ..........    0.0000E+00
          eq.0: use time based termination (default)    

    displacement termination tolerance 2 ..........    0.0000E+00
          eq.0: use time based termination (default)    

    zero out velocities when switching to implicit       0
          eq.0: keep velocities (default)    
          eq.1: zero velocities 



    IMPLICIT CONTROL CARD 2.  Solution

    solution method ...............................      12
          eq.-1:linear, multiple loading w/same stiffness
          eq.1: linear                               
          eq.2: nonlinear, BFGS updates              
          eq.3: nonlinear, Broydens updates          
          eq.4: nonlinear, DFP updates               
          eq.5: nonlinear, Davidon updates           
          eq.6: nonlinear, BFGS updates+arclength    
          eq.7: nonlinear, Broydens updates+arclength
          eq.8: nonlinear, DFP updates+arclength     
          eq.9: nonlinear, Davidon updates+arclength 
          eq.12:nonlinear, (experimental), BFGS updates 
                           with optional arclength

    iteration limit per reformation ...............      11

    reformation limit per step ....................      15
          lt.0 implicit will declare convergence after 
               |maxref| matrix reformations

    displacement convergence tolerance ............    0.1000E-02
          lt.0 -(curve ID) defining tolerance w.r.t. time

    energy convergence tolerance ..................    0.1000E-01
          lt.0 -(curve ID) defining tolerance w.r.t. time

    residual convergence tolerance ................    0.1000E+11
          lt.0 -(curve ID) defining tolerance w.r.t. time

    line search convergence tolerance .............    0.9000E+00

    absolute convergence tolerance ................    0.1000E-09

    displacement norm .............................       2
          eq.1: increment vs. total this step           
          eq.2: increment vs. total whole simulation    

    divergence flag ...............................       1
          eq.1: reform stiffness if residual grows      
          eq.2: ignore growing residual                 

    initial stiffness interval ....................       1
          eq.1: form new stiffness each step            
          eq.n: new stiffness every n steps             

    nonlinear solver print flag ...................       0
          eq.0: defaults to same as 1                   
          eq.1: print iteration info to screen, files   
          eq.2: extra iteration info to d3hsp and messag
          eq.3: all iteration info to d3hsp and messag  


    IMPLICIT CONTROL CARD 2a.  Solution

    convergence norms .............................       2
          lt.0: defaults to 4 but scales rotations      
                with characteristic length              
          eq.1: use translational and rotational DOFs   
          eq.2: use only translational DOFs             
          eq.4: use translational plus rotational DOFs  

    d3iter control ................................       0
          eq.0: use sense switch control (default)      
          eq.n: write d3iter database every time step   
                but rewind every n-th time step         

    line search method ............................       4
          eq.1: based on translational dofs (default)   
          eq.2: based on residual function              
          eq.3: based on translational+rotational dofs  

    line search direction .........................       2
          eq.1: traditional form (ls970 and earlier)    
          eq.2: search only independent dofs (default)  
          eq.3: adaptive line search (experimental)     
          eq.4: curved line search (experimental)       

    experimental line search parameters ...........
          curvature factor 0-straight,1-full curved    0.0000E+00
          radius of influence (curved search)          0.0000E+00
          adaptive line search weight (0. to 1.)       0.0000E+00
          init. step reduction (0. to 1.,adaptive)     0.0000E+00
    contact penetration check .....................       0
          eq.0: no checking (default)                   
          eq.1: check for contact penetration           



    IMPLICIT CONTROL CARD 2b.  Joints              

    implicit treatment for spherical joint ........       0
          eq.1: constraint formulation (DEFAULT)
          eq.2: penalty formulation  

    implicit treatment for revolute joint .........       0
          eq.1: constraint formulation (DEFAULT)
          eq.2: penalty formulation  

    implicit treatment for cylindrical joint ......       0
          eq.1: constraint formulation (DEFAULT)
          eq.2: penalty formulation  



    IMPLICIT CONTROL CARD 3.  Linear Solver

    linear equation solver ........................      7
          eq. 2: sparse direct with dynamic memory       
          eq. 6: BCSLIB-EXT double - auto out-of-core    
          eq.10: iterative, best method available        
          eq.11: iterative, Conjugate Gradient           
          eq.12: iterative, C.G. with Jacobi             
          eq.13: iterative, C.G. with Inc. Choleski      
          eq.14: iterative, Lanczos                      
          eq.15: iterative, Lanczos with Jacobi          
          eq.16: iterative, Lanczos with Inc. Choleski   
          eq.22: iterative, C.G. with Diagonal Precond   
          eq.23: iterative, C.G. with Sym GS Precond     
          eq.24: iterative, C.G. with SSOR Precond       
          eq.25: iterative, C.G. with ILDLT Precond      
          eq.26: iterative, C.G. with ILDLT w/extra fill 
          eq.30: Mumps                                   
          eq.90: User Supplied Linear Equation Solver    

    linear solver print flag ......................      0
          eq.0: no printing                             
          eq.1: small amount of summary statistics      
          eq.2: additional statistics                   
          eq.3: debug level recommended only for problem-debugging

    negative eigenvalue option ....................      2
          eq.1: retry step if negative eigenvalue       
          eq.2: ignore negative eigenvalues             

    sparse ordering option ........................      0
          eq.0: ordering chosen by LS-DYNA              
          eq.1: order with Multiple Minimum Degree      
          eq.2: order with METIS                        

    Drilling Rotation Constraint Method ...........      4
          eq.1: add additional stiffness                
          eq.3: no constraint method                    
          eq.4: add force and stiffness                 

    Drilling Rotation Constraint Parameter ........    1.0000E+00

    AUTOSPC Control Switch ........................      1
          eq.1: AUTOSPC On                              
          eq.2: AUTOSPC Off                             

    AUTOSPC Tolerance .............................    1.0000E-08

    Matrix Assembly Method ........................      2
          eq.2: Use LCPACK (default)                    
          eq.3: Use LCPACK w/nonsymmetric               

    Matrix Dumping Flag ...........................      0

    User requested number of Metis executions .....      0
    Matrix Reordering Reuse Parameter .............    0.0000E+00



    IMPLICIT CONTROL CARD 4.  Auto Time Step Control

    time step control method ......................       1
          eq.0: fixed (constant) time step size         
          eq.1: variable automatic time step size       
          eq.2: variable automatic time step size with  
                max step limited by thermal time step   
          lt.0: time step size specified by load curve  

    target iteration count ........................      11

    iteration window ..............................       5

    minimum allowable step size ...................    0.5000E-03

    maximum allowable step size ...................    0.5000E+01
          eq.0: max. allowed step size is 10*initial step size
          gt.0: maximum allowed step size                 
          lt.0: -(curve ID) for max. allowed step size    

    time interval to run explicit when switching       0.0000E+00
          lt.0: -(curve ID) for time interval             

    no. of failed steps before switching ..........       1

    min. no. of explicit steps after switching ....       0

    artificial stabilization flag .................       2
          eq.1: on  ('springback' analysis DEFAULT)      
          eq.2: off ('standard' analysis DEFAULT)        

    scale factor for artificial stabilization .....    0.1000E+01

    start time for artificial stabilization .......    0.0000E+00
          eq.0.0: immediately                            

    end time for artificial stabilization .........    0.0000E+00
          eq.0.0: termination time



    IMPLICIT CONTROL CARD 5.  Dynamic and Eigenvalue

    implicit dynamic flag .........................       0
          eq.0: implicit static
          eq.1: implicit dynamic
          eq.2: modal superposition (eigenvalue analysis)
          eq.3: modal superposition using d3eigv file    

    first  Newmark parameter (default=.50) ........    0.0000E+00

    second Newmark parameter (default=.25) ........    0.0000E+00

    number of eigenvalues to extract ..............       0
          lt.0: -(curve ID) for intermittent extraction   

    eigenvalue frequency shift ....................    0.0000E+00

    number of constraint modes to extract .........       0

    number of attachment modes to extract .........       0

    number of eigen      modes to extract .........       0

    buckling mode flag ............................       0
          eq.0: compute eigenvalues
          eq.1: compute buckling modes

    buckling eigenmethod ..........................       1
          eq.1: Lanczos (default)
          eq.2: Power Method (reqd for inertia relief)

    inertia relief computation flag ...............       0
          eq.0: do not perform inertia relief computation
          eq.1: perform inertia relief computation impl/expl
          eq.2: perform inertia relief computation impl only

    inertia relief mode threshold .................    0.0000E+00

    Eigenvector Dumping Flag ......................       0

    Modal Stress Recovering Scaling Parameter .....    0.1000E-02

    Accuracy Control for output to file eigout ....       0
          eq.0: use default of e15.6
          ge.1: use e25.16

    Flag for optional eigenvalue control card .....       0
          eq.0: no card - use defaults
          ge.1: next cards specifies additional parameters

    Optional time integration parameter for composite
    time integration scheme .......................    0.0000E+00
          eq. 0: no composite scheme
          gt. 0: value is alpha in Bathe scheme
          gt.-1: value is alpha in HHT scheme
          le.-1: absolute value is number of sets in FRD scheme,
                 details reported elsewhere


    IMPLICIT CONTROL CARD 6.  Arc Length            

    node controlling arc length method ............       0
          eq.0: generalized arc length method

    direction controlling arc length method .......       0

    arc length size  ..............................    0.0000E+00
          eq.0: chosen from initial stepsize

    arc length formulation ........................       1
          eq.1: Crisfield (generalized arc length only)
          eq.2: Ramm 
          eq.3: Modified Crisfield
                (used with nonlinear solution method 12 only)

    arc length damping option .....................       2
          eq.1: on
          eq.2: off

    psi, influence of load/time parameter in
    predictor step.................................    0.0000E+00

    alpha, influence of predictor step on
    cylindrical center in corrector steps..........    0.0000E+00

    time when arclength is first initiated.........    0.0000E+00


    IMPLICIT Residual Vector Controls

    on/off flag ...................................       0
          eq.0: Implicit Residual Vector off (DEFAULT)
          eq.0: Implicit Residual Vector active


    IMPLICIT FRF Controls

    on/off flag ...................................       0
          eq.0: Implicit FRF off (DEFAULT)
          eq.0: Implicit FRF active


 c o n t r o l   i n f o r m a t i o n

    CONTROL CARD 1. Model Size-General

    number of materials or property sets...........       1

    number of nodal+scalar points..................     160

    number of merged nodal points..................       0

    number of solid elements.......................      81

    number of beam elements........................       0

    number of shell elements.......................       0

    number of thick shell elements.................       0

    number of user defined material subroutines....       0

    number of material groups tied to solids.......       0

    number of tracer particles.....................       0

    number of super elements.......................       0

    number of solid tetrahedrons with 10 nodes.....       0

    number of quadratic shell elements.............       0

    number of shells with extra degrees of freedom.       0

    number of solids with extra degrees of freedom.       0

    number of user defined sections................       0

    activate sensor capability (inactive=0)........       0

    number of user defined solid element types.....       0

    number of solid interpolation elements.........       0

    number of user defined shell element types.....       0

    number of shell interpolation elements.........       0

    number of constrained nodes for interpolation..       0

    consistent mass matrix for user-def elements...       0

    number of shell nurbs patches..................       0

    number of solid nurbs patches..................       0

    number of tree branches........................       0


    CONTROL CARD 2. Model Size-Boundary Conditions

    number of spc nodes............................      16

    number of spc coordinates......................       0

    number of velocity cards.......................      16

    number of non-reflecting boundary segments.....       0

    number of b. c. cards..........................       0

    number of b. c. cards with failure.............       0

    number of box definition for b. c. card........       0

    number of nodes/interface for cyclic symmetry..       0

    number of rigid bodies with attachment nodes...       0


    CONTROL CARD 3. Model Size-Loading

    number of load curves..........................       1

    number of nodes for load curve functions.......       0

    number of curves for entities..................       0

    number of concentrated load cards..............       0

    number of pressure load cards..................       0

    number of expansion pressure load cards........       0

    number of nonuniform pressure loads-4 nodes....       0

    number of nonuniform pressure loads-6 nodes....       0

    number of nonuniform pressure loads-8 nodes....       0

    number of generalized body force sets..........       0

    number of beam pressure card definitions.......       0

    number of detonation points....................       0

    number of zones for momentum deposition........       0

    number of points in density vs. depth curve....       0

    number of outflow boundary segments............       0

    number of load curve feedback sets.............       0

    number of pressure load sets with masks........       0

    number of spray systems .......................       0

    number of initial stress by cross-sections sets       0

    number of pressure load sets...................       0

    number of ground motion definitions............       0

    number of ground motions specified at nodes....       0

    number of ground motions specified at points...       0

    number of ground motions specified in bin file.       0

    number of segsets with specified ground motion.       0

    number of soil-structure interfaces for output.       0

    number of aero-acoustic load cards.............       0

    number of delayed curve........................       0

    number of pid controller.......................       0


    CONTROL CARD 4. Model Size-Constraints and Contact

    number of rigid wall definitions...............       0

    number of number of contact definitions........       0

    number of number of guided cable contacts......       0

    number of shell-solid interfaces...............       0

    number of tie-breaking slide lines.............       0

    number of blocks of tied nodes with fracture ..       0

    number of tied nodal pairs for linking.........       0

    number of constraint cards.....................       0

    number of linear constraint equations..........       0

    number of 1d slidelines........................       0

    number of adaptive constraints.................       0

    number of ALE smoothing constraints............       0

    number of 2d slidelines........................       0

    number of 2d automatic contacts................       0

    number of part IDs for interior contact........       0

    number of beam release sets....................       0

    max. number of nodes in any beam release set...       0


    CONTROL CARD 5. Model Size-Rigid Body Parameters

    number of rigid body constraint sets...........       0

    number of rigid body merge cards...............       0

    number of joint constraints....................       0

    number of joint failure definitions............       0

    number of joint user force definitions.........       0

    number of extra node blocks....................       0

    number of rigid body inertia definitions.......       0

    number of geometric contact entities...........       0

    number of joint stiffness definitions..........       0

    number of rigid body stoppers..................       0

    joint formulation for rigid bodies.............       0
          eq.0:  penalty                                 
          eq.1:  lagrange multiplier                     

    generalized stiffness angle update ............       3
          eq.0:  incremental formulation                 
          eq.1:  total formulation                       

    number of flexible bodies......................       0
          lt.0:  stress recovery active                  

    number of relative damping definitions.........       0

    flag for reading rigid surface contact input...       0
          eq.0:  no rigid surface contact                 
          eq.1:  read rigid surface input                

    number of Hybrid III dummies ..................       0

    number of Hybrid III joint modifications ......       0

    number of interpolation constraints ...........       0

    flag for metalforming fast rigid bodies........       0
          eq.0:  full rigid body treatment               
          eq.1:  fast rigid body treatment               

    number of prescribed rigid body orientations          0


    CONTROL CARD 6. Model Size-Discrete Elements & Seat Belts

    number of spring-damper material types.........       0

    number of local coordinate systems.............       0

    number of discrete springs and dampers.........       0

    number of lumped masses........................       0

    number of parts with added mass................       0

    number of nodes with mass matrix...............       0

    number of seat belt materials..................       0

    number of seat belt elements...................       0

    number of 2d seat belt elements................       0

    number of slip rings...........................       0

    number of retractors...........................       0

    number of sensors..............................       0

    number of pretensioners........................       0

    number of accelerometers.......................       0

    number of discrete rotary inertias.............       0

    number of SPH particles........................       0

    number of groups of SPH particles..............       0


    CONTROL CARD 7. Model Size-Output Control

    number of cross section definitions............       0

    number of nodal groups for resultant forces....       0

    number of interface segments for linking.......       0

    max. number of segments defining rigid wall....       0

    number of power spectrum density databases.....       0


    CONTROL CARD 8. Computation Options-Termination

    termination time...............................    0.3000E+02

    termination cycle..............................       0

    reduction factor for minimum time step (TSMIN).    0.0000E+00

    percent change in energy ratio for termination.    0.0000E+00

    percent change in total mass for termination...    0.1000E+09

    number of nodes for displacement termination...       0

    number of rigid bodies for disp. termination...       0

    number of conditions for contact termination...       0

    number of conditions for ldcurve termination...       0

    ID of sensor_switch  for sensor  termination... 0


    CONTROL CARD 8a. Computation Options-Start      

    start time.....................................    0.0000E+00


    CONTROL CARD 9. Computation Options-Time Step Size 

    initial time step size.........................    0.0000E+00

    time step scale factor.........................    0.9000E+00
          lt.0:  -curve bumber for time step scale factor

    time step size calculation for 4-node shells...       0
          eq.0:  based on longest element side          
          eq.1:  based on longest element diagonal      
          eq.2:  based on bar wave speed max side       
          eq.3:  based on optimal time step size        
                 estimator                              

    shell element minimum time step assignment.....    0.0000E+00

    time step size for mass scaled solution, dt2ms.    0.0000E+00
          lt.0:  minimum time step size permitted       

    load curve number for maximum timestep.........       0

    erosion/termination flag for element dt < TSMIN       0
        beam elements..............................    not active
        shell elements.............................    not active
        solid and tshell elements..................    not active

    solid element time step calculation option, IHDO      0
          eq.0:  default method
          eq.1:  method to improve time step continuity

    option part set ID for eroding solids..........       0
          eq.0:  all solids and thick shells are checked
                 if ERODE=1 and TSMIN>0 or if TSMIN<0
          gt.0:  solids within part set are checked      

    limit mass scaling to the first time step......       0
          eq.0:  no                                      
          eq.1:  yes                                     

    scale factor on initial dt to determine dt2ms..    0.0000E+00

    load curve ID for mass scaling ................       0

    flag for selective mass scaling................       0
          eq.0:  off                                     
          eq.1:  on                                      
          eq.2:  on for part subset                      

    consistent constraint logical switch...........       F

    flag for part set for erosion .................       0
          eq.0:  no                                      
          eq.1:  yes                                     

    flag for accounting for rotations in sms.......    0.0000E+00
          eq.0.:  off (default)                           
          gt.0.:  on                                      
    implicit_explicit_hybrid part set..............       0

    fraction of added mass contributing to gravity.    0.0000E+00

    consistent mass scaling (0=off, 1=on)..........       0

    user defined average nodal rotational mass ....    0.0000E+00

    IGA element time step calculation option, IGADO      0
          eq.0: default method - conservative 
          eq.1: account for inner-patch continuity 




    CONTROL CARD 10. Computation Options-Loading

    x-ground acceleration..........................       0
          eq.0:  no                                      
          eq.1:  yes                                     

    y-ground acceleration..........................       0
          eq.0:  no                                      
          eq.1:  yes                                     

    z-ground acceleration..........................       0
          eq.0:  no                                      
          eq.1:  yes                                     

    x-angular velocity.............................       0
          eq.0:  no                                      
          eq.1:  yes                                     

    y-angular velocity.............................       0
          eq.0:  no                                      
          eq.1:  yes                                     

    z-angular velocity.............................       0
          eq.0:  no                                      
          eq.1:  yes                                     

    number of materials receiving body forces......       0
          eq.0:  all                                     
          eq.n:  subset of n materials                   

    flag for user defined loading subroutine.......       0
          lt.0:  magnitude=# of input constants          
          eq.0:  no                                      
          eq.1:  yes, but no additional input            

    explosive initiation option....................       0
          eq.0:  lighting times based on distance        
          eq.1:  lighting times include geometric        
                 effects for wave shapers, etc.          

    sub-sea structural analysis option.............       0
          eq.0:  off                                     
          eq.1:  on with 1 point integration             
          eq.4:  on with 4 point integration             
    contact pressure calculation option............       0
          eq.0:  off (default)                           
          eq.1:  on                                      
    # of user defined loading set..................       0


    CONTROL CARD 11. Computation Options-Input Control

    initialization of velocities...................       0
          eq.0: velocities are initialized to zero       
          eq.1: initial velocities are read in           
          eq.2: all velocities have same input value     
          eq.3: as 2 but exempted nodes are defined      
          eq.4: box option                               
          eq.5: generation with arbitrary numbering      
          eq.6: rotational and translational via IDs     
          eq.7: option 6 but applied during calculation  

    time to apply initial velocites (option 7).....    0.0000E+00

    arbitrary node and element numbering flag .....       1

    constitute, eqs-of-state, cross-section option.       0
          eq.0:  off                                     
          eq.1:  separate input is required for each     

    specified nodal coordinate format..............    e20.0

    flag for thermodynamic control volume input....       0

    overpressure option (eq.0 no,  eq.1 yes).......       0

    number of part (de) activation sensors.........       0

    number of rigid body initial velocity sets.....       0

    jacobian tolerance for type 16 tetrahedron.....    0.0000E+00

    flag to check for NaN in force/moment arrays...       0

    load curve accuracy flag.......................       0

    cycles between evaluation of curve functions...       1

    no-copy option for history variables...........       0


    CONTROL CARD 12. Computation Options-Elements  

    warped shell angle in deg. for error message...    0.2000E+02

    iterative plane stress plasticity for shells...       1
          eq.1:  vectorized with three iterates         
          eq.2:  nonvectorized iterations as needed     
          eq.3:  noniterative radial return             

    Calculation option for F for solid elements....       0
          eq.0:  default, explicit=1, implicit=2        
          eq.1:  integrate incrementally                
          eq.2:  compute directly                       

    flag for automatic sorting ....................       0
          eq. 1:  on for triangular shells              
          eq.11:  on for triangular shells and solids   
          eq.10:  on for solids (tets and pentas)       

    formulation for sorted degenerate tet/pent.....       0
          eq. 0:  no sorting required(default)           
          eq. 1:  type 10 tet & type 15 pent             
          eq. 2:  type 10 tet, 1pt pent to type 15 pent, 
                  fully intg pent to type 115 pent       
          eq. 3:  same as 1 & switch elem in messag file 
          eq. 4:  same as 2 & switch elem in messag file 

    formulation for sorted trianglar shells .......       0
          eq. 0:  no sorting required(default)           
          eq. 1:  C0 triangle, type  4                   
          eq. 2:  DKT triangle type 17                   

    hughes-liu normal computation options..........      -1
          eq.-2: unique nodal fibers                    
          eq.-1: compute normals each cycle
          eq.0 : default set to -1     
          eq.1 : compute on restart
          eq.n : compute on restart + each nth cycle     

    consistent tangent for type 13 solid...........       0
          eq.0 : no, recommended for nonlinear implicit 
          eq.1 : yes, may improve linear response       

    choice of type 13 solid implementation.........       0
          eq.0 : efficient version (default)            
          eq.1 : slower but more accurate version       

    thickness modification for membrane strains....       0
          eq.0:  no                                     
          eq.1:  4-node shell only                      
          eq.2:  8-node thick shell types 1 & 2         
          eq.3:  update both 4 & 8 node thickness       
          eq.4:  same as option 1 but the elastic       
                 strains are neglected                  

    shell part set ID (pids) for thickness update.  0
          lt.0: exclude pids if update option is active  
          eq.0: include  all if update option is active  
          gt.0: include pids if update option is active  

    shell part set ID where type 4 update applies   0

    shell formulation basis........................ 2
          eq.   1: hughes-liu                            
          eq.   2: belytschko-tsay                       
          eq.   3: bciz                                  
          eq.   4: c0-triangular element                 
          eq.   5: membrane element                      
          eq.   6: s/r hughes-liu                        
          eq.   7: s/r co-rotational hughes-liu          
          eq.   8: belytschko-leviathan shell            
          eq.   9: fully integrated membrane             
          eq.  10: belytschko-wong-chiang                
          eq.  11: fast hughes-liu                       
          eq.  12: 2d plane stress                       
          eq.  13: 2d plane strain                       
          eq.  14: 2d axisymmetric  (area wgt)           
          eq.  15: 2d axisymmetric  (volume wgt)         
          eq.  16: fully integrated element              
          eq.  17: dkt element                           
          eq.  18: dkq-dkt linear element                
          eq.  20: assumed strain linear element         
          eq.  21: assumed strain linear element(5DOF)   
          eq.  22: linear shear panel element(3DOF)      
          eq.  23: 8-node quadratic quadrilateral shell  
          eq.  24: 6-node quadratic triangular shell     
          eq.  25: belytschko-tsay with                  
                   thickness stretch                     
          eq.  26: fully integrated element with         
                   thickness stretch                     
          eq.  27: c0-triangular element with            
                   thickness stretch                     
          eq.  29: cohesive element for shell            
                   edge-to-edge connections              
          eq. -29: cohesive element with midlayer        
                   coordinate system for pure shear      
          eq.  31: 2-d 1-pt. eulerian n-s                
          eq.  32: 2-d 4-pt. eulerian n-s                
          eq.  33: 2-d cvfem eulerian n-s                
          eq.  41: meshfree shell local projection       
          eq.  42: meshfree shell global projection      
          eq.  43: meshfree plane strain                 
          eq.  44: meshfree axisymmetric solid           
          eq.  46: cohesive element compatible with 2d   
                   plane stress, plane strain, or        
                   area-weighted axisymmetric elements   
          eq.  47: cohesive element compatible with 2d   
                   volume-weighted axisymmetric elements 
          eq.  98: interpolation shell element           
          eq.  99: elastic vibration element             
          eq. 201: isogeometric nurbs element            
          ge.1000: user defined (generalized) shell      

    # of user specified beam integration rules.....       0
    max number of integration points reqd (beams) .       0
    # of user specified shell integration rules....       0
    max number of integration points reqd (shells).       0
    warping stiffness for Belytschko-Tsay shells...       2
          eq.1:  Belytschko-Wong-Chiang modification    
          eq.2:  original Belytschko-Tsay               

    projection method for warping stiffness........       0
          eq.0:  drill                                   
          eq.1:  full                                    

    reference configuration .......................       0
          eq. 0:  no                                      
          eq. 1:  yes, active for all airbags             
          eq. 2:  yes, reference geometry Dt              
          eq.10:  yes, active for foam elements           
          eq.11:  options 1 and 10 active                 
          eq.12:  options 2 and 10 active                 

    contact reference configuration ...............       0
          eq. 0:  no                                      
          eq. n:  n number of reference nodes             

    invariant node numbering ......................       2
          eq.-4  on for both shell and solid elements   
                 except triangular shells               
          eq.-2  on for shell elements except           
                 triangular shells                      
          eq. 1  off (default)                          
          eq. 2  on for all shell elements              
          eq. 3  on for solid elements with             
                 anisotropic material                   
          eq. 4  on for all shell elements and solid    
                 elements with anisotropic material     

    activation time for reference geometry ........    0.0000E+00

    scale factor for shell rotary mass ............    0.1000E+01
    scale factor for shell rotary added mass ......    0.1000E+01

    integration for shell through thickness .......       0
          eq.0:  Gauss                                   
          eq.1:  Lobatto                                 

    use laminated shell theory for material .......       0
    types 22, 54, 55, and 76:                      
          eq.0:  no                                      
          eq.1:  yes for thin shell material types       
                 22, 54, 55, or 76                       
          eq.3:  yes for all thin shell anisotropic      
                 materials or mixed materials            
          eq.4:  yes for all thick shell anisotropic     
                 materials or mixed materials            
          eq.5:  yes for thick and thin shells           

    number of annealed parts .......................       0

    number of new part IDs for COMPOSITE option.....       0

    flag for shell offset vectors .................       0
          eq. 0:  off                                   
          eq. 1:  on                                    

    flag to reduce time step for shell offsets ....       0
          eq. 0:  reduction depending on offset         
          eq. 1:  no reduction                          

    flag for offset shell contact surface .........       0
          eq. 0:  off                                   
          eq. 1:  on                                    
          eq. 2:  on, but use contact thickness         

    number of point constraints between shells ....       0

    flag for input of beam orientation vectors ....       0

    flag for input of beam offset vectors .........       0

    flag for input of beam warpage scalar nodes....       0

    flag for 12-node shell for thermal ............       0

    local shell coordinate system in type 6 shell..       1
          eq. 0:  uniform local coordinate system       
          eq. 1:  variable local coordinate system      

    Jacobian check on 1 point shells...............       0
          eq. 0:  off                                   
          eq. 1:  on -delete distorted element          
          eq. 2:  on -terminate                         
          eq. n:  terminate when n elements are deleted 

    Jacobian check on 4 point shells...............       0
          eq. 0:  off                                   
          eq. 1:  on -delete distorted element          
          eq. 2:  on -terminate                         
          eq. n:  terminate when n elements are deleted 

    part set ID for Jacobian checks................ 0

    keep contact segment related to failed shell...       0
          eq. 0:  off                                   
          eq. 1:  on                                    
    delete free-free shells in Jacobian checks.....       0
          eq. 0:  off                                   
          eq. 1:  on                                    

    part set ID for drill constraint force ........ 0
    scale factor for drill constraint force .......  0.00000000E+00
    method for drill constraint force .............       0
          eq. 0:  generalized drill strain, node based  
          eq. 1:  spin tensor, element based            

    w mode deletion angle in degrees ..............    0.0000E+00

    stretch ratio deletion (l/l0) .................    0.0000E+00

    flag for error exit in case of unwanted        
    interpolation of inital stresses ..............       0

    number of shell  part IDs for termination......       0
          eq. 0:  inactive                              
          gt. 0:  # part IDs where # failed are defined 

    number of solid  part IDs for termination......       0
          eq. 0:  inactive                              
          gt. 0:  # part IDs where # failed are defined 

    integration rule for quadratic tetrahedrons....       4
          eq. 4:  4 point integration formula           
          eq. 5:  5 point integration formula           

    integration rule for quadratic shells..........       3
          eq. 2:  2x2 integration in plane              
          eq. 3:  3x3 integration in plane              

    stress output for solid element spotwelds......       0
          eq. 1:  global (default)                      
          eq. 2:  local                                 

    # of solid elements with death times...........       0

    # of beam  elements with death times...........       0

    # of shell elements with death times...........       0

    # of thick shell elements with death times.....       0

    # of box definitions for element deletion......       0

    # of parts to be annealed......................       0

    flag for input of elbow extra scalar nodes.....       0

    flag for material stochastic variations........       0

    number of tailor welded blanks ................       0

    number of heat affected zone property sets.....       0

    flag for loading segments with file option.....       0

    flag for loading segments FSI link file........       0


    number of solid elements with initial stress ..       0

    number of sph   elements with initial stress ..       0

    number of beam  elements with initial stress ..       0

    number of shell elements with initial stress ..       0

    number of shell elements with initial strain ..       0

    number of iga-shell elms with initial stress ..       0

    number of iga-shell elms with initial strain ..       0

    number of iga-solid elms with initial stress ..       0

    number of iga-solid elms with initial strain ..       0

    maximum number of tensor data .................       0

    maximum number of history variables ...........       0

    no. of thick shell elems with initial stress ..       0

    number of solid elements with initial strain ..       0

    number of solid elements with initial dof......       0

    number of nodes with initial geometry..........       0

    write nodes with initial geometry..............       0
        = 0: do not write nodes
        = 1: write nodes

    number of discrete element spheres.............       0

    flag for initial transverse shear stresses ....       0
        = 0: keep transverse shear stresses (default)
        = 1: set transverse shear stresses to zero

    psid for shells with local initial stresses ...       0

    number of of thick shells with inital strain...       0

    cohesive element flag ICOH = [LK] = K+10*L ....       0
        K = 0: do not delete after neighbor failed
        K = 1: delete after neighbor failed
        L = 0: default time step estimate
        L = 1: most conservative (smallest) 
               time step estimate
        L = 2: intermediate time step estimate

    flag for SPR2/SPR3 initial radius of influence        0
          eq.0:  silently increased to find enough nodes 
          eq.1:  same as .eq.0 but write warning         
          eq.2:  error termination if too small          


    CONTROL CARD 13. Computation Options-Materials

    hourglass formulation..........................       0
          eq.0   LS-DYNA versions 940 and after         
          eq.1   LS-DYNA versions 936 and before        

    hourglass models                              
          eq.1: standard viscous form                  
          eq.2: flanagan-belytschko viscous form       
                1pt volume integration for solids      
          eq.3: flanagan-belytschko viscous form       
                exact volume integration for solids    
          eq.4: flanagan-belytschko stiffness form     
                1pt volume integration for solids      
          eq.5: flanagan-belytschko stiffness form     
                exact volume integration for solids    
          eq.6: bindeman-belytschko stiffness form     
                for 2d and 3d solid elements only      
          eq.9: puso stiffness form for 3d solid       
                elements only                          

    hourglass model (default)......................       0

    hourglass coefficient (default)................    0.0000E+00

    bulk viscosity type (default)..................       0
          eq.-2: standard +types 2,4,10,16,17 shells+IE 
          eq.-1: standard +types 2,4,10,16,17 shells    
          eq.+1: standard                               

    quadratic bulk viscosity coefficient...........    0.0000E+00

    linear bulk viscosity coefficient..............    0.0000E+00

    bulk viscosity type for beams..................       0
          eq.+1: standard  
          eq.+2: standard + IE 

    bulk viscosity for thick shells................       0
          eq.0:  off (default)
          gt.0:  on (forms 5, 6, and 7)

    flag for rayleigh damping input................       0
          eq.0:  off (default)                          
          eq.1:  on                                     

    flag for rigid/deformable material switching...       1
          eq.1:  off (default)                          
          eq.2:  on                                     
          eq.3:  on and automatic switching             

    thermal effects option.........................       0
          eq.0:  no thermal effects                      
          eq.n:  nodal temps scaled by load ftn -n-      
          eq.-1: coupled thermal mechanical analysis     
          eq.-2: temperature data input option 2         
          eq.-3: thermal solution                        
          eq.-4: Read binary temperature file            
          eq.-5: Read d3plot file                        
          eq.-6: Read LSDA file                          
          eq.-9998: user defined load set temp. input    
          eq.-9999: temperature data input option 1      

    thermal curve ID used for dynamic relaxation... 0

    super plastic forming input option.............       0
          eq.0:  skip input                              
          eq.1:  read superplastic input section         

    objective stress update for large Dt...........       1
          eq.0:  off (default)                           
          eq.1:  on globally                             
          eq.2:  on for part subset                      

    default contact parameters input option........       0
          eq.0:  no                                      
          eq.1:  yes                                     

    number of reinforcement cards for mat 84&85....       0

    output interval for aea_crack database.........    0.0000E+00

    number of non local materials..................       0

    neighbours arrays oversized of (%).............       0

    number of parts defined for adaptive failure...       0

    number of elements with specified temperature..       0

    number of parts with spotweld rupture stress...       0

    number of parts with spotweld rupture parametr.       0

    number of spotweld lists.......................       0

    number of rows of opt=10 spot weld failure data       0

    implicit accuracy option to turn on strong     
    objectivity in various features (elements,     
    contacts, constraints, etc.....................       0
          eq.0:  no                                      
          eq.1:  yes                                     

    flag for MAT_ADD_EROSION failure switching ....       0
          eq.0:  on (default)                            
          eq.1:  off globally                            

    flag for MAT_USER treatment ...................       0
          eq.0:  warning if default umat is used         
          eq.1:  error termination if default umat is used


    CONTROL CARD 14. Computation Options-Damping

    load curve specifying system damping...........       0
          eq.-1: system damping by material             
          eq. n: load curve n defines system damping    

    optional constant for system damping...........    0.0000E+00

    system damping scale factor for x-translation..    0.1000E+01

    system damping scale factor for y-translation..    0.1000E+01

    system damping scale factor for z-translation..    0.1000E+01

    system damping scale factor for x-rotation.....    0.1000E+01

    system damping scale factor for y-rotation.....    0.1000E+01

    system damping scale factor for z-rotation.....    0.1000E+01

    stress initialization flag ....................       0
          eq.-1:  dynamic relaxation (debug option)       
          eq.0:   off                                     
          eq.1:   dynamic relaxation                      
          eq.2:   deformed geometry                       
          eq.3:   dynamic relaxation with part set ID     
          eq.5:   initialize implicitly                   
          eq.-999:off-not activated by load curves        

    convergence check interval (dynamic relaxation)     250

    convergence tolerance for dynamic relaxation...    0.1000E-02

    dynamic relaxation factor......................    0.9950E+00

    termination time for dynamic relaxation........    0.0000E+00
          eq.0.0:  convergence terminates relaxation     
          gt.0.0:  termination at specified time         
                   unless convergence is attained        

    scale factor for dyn relax time step...........    0.9000E+00

    automatic determination of dr factors..........       0
          eq.0:  off (default)                          
          eq.1:  on                                     

    convergence tolerance for above option.........    0.0000E+00

    active part set ID for dynamic relaxation ..... 0



    CONTROL CARD 15. Computation Options-Contact

    scale factor for contact interface penalties...    0.1000E+00

    scale factor for rigid wall penalties..........    0.0000E+00

    flag to activate MADYMO contact coupling.......       0
          eq.0:  inactive                              
          eq.1:  active                                

    track initial penetrations in auto contacts....       0
          eq.0:  no, move node to contact surface      
          eq.1:  yes, initial penetrations remain      

    ignore initial separations in tied contacts....       0
          eq.0:  no, eliminate gaps most accurate      
          eq.1:  yes, may lock rotations               

    contact initial penetration check option.......       1
          eq.1:  off (default)                           
          eq.2:  on                                      

    thickness considered in type 3, 5 or 10 contact       0
          eq.0:  off                                     
          eq.1:  on, but rigid bodies excluded           
          eq.2:  on, rigid bodies are included           

    penalty stiffness option.......................       0
          eq.1:  minimum master/slave value             
          eq.2:  master segment stiffness (old way)     
          eq.3:  slave node stiffness                   
          eq.4:  slave node area/mass weighted          
          eq.5:  like 4 but k proportional to 1/thick   

    thickness changes considered in contact........       0
          eq.0:  no for type 4, 13, and a13 contact      
                 except for segment based contact (SOFT=2),
          eq.1:  yes                                     
          eq.2:  no in any segment based conatct (SOFT=2)

    automatic reorientation option.................       1
          eq.1:  on for automatic contact definitions   
          eq.2:  on                                     
          eq.3:  off                                    

    memory allocation-user contact surface control        0
          gt.0:  memory per interface passed to user    

    memory allocation-user contact surface frict...       0
          gt.0:  memory per interface passed to user    

    number of time steps between contact searching.       0
          eq.0:  LS-DYNA chooses value                  

    intermittent searching in type 3 contact.......       0
          eq.0:  off (default)                           
          eq.1:  on                                      

    release factor for extra searching option......    0.4000E+01

    treatment of nodes in eroding contact..........       0
          eq.0:  delete from calculation                
          eq.1:  keep nodes of eroded solids            
          eq.2:  keep nodes of eroded solids & shells   

    calculation of frictional sliding energy.......       0
          eq.0:  do not calculate                       
          eq.1:  calculate                              

    shell thickness in single surface contact......       0
          eq.0:  use characteristic shell dimension     
          eq.1:  use actual shell thickness             

    time step size override for eroding contact....       0
          eq.0:  contact time size may control dt        
          eq.1:  contact is not considered for dt        

    number of automatic positioning definitions....       0

    print slave node/segment in spotweld contact...       0
          eq.0:  no                                      
          eq.1:  yes, in D3HSP file                     

    option for unconstrained spotweld node/face....       0
          eq.0:  ignore                                 
          eq.1:  terminate                              
          eq.2:  delete weld and continue               

    delete spotweld if tied to failed shell........       0
          eq.0:  no                                     
          ge.1:  yes                                    

    number of friction table definitions...........       0

    read in friction table for automatic contacts..       0
          eq.0:  no                                     
          ne.0:  number of part pair defined for table  

    include sliding energy density in d3plot.......       0
          eq.0:  no                                     
          eq.1:  yes                                    

    read in spotweld failure table.................       0
          eq.0:  no                                     
          ne.0:  number of part pair defined for table  

    contact thickness scaling option for welds.....    0.0000E+00
          eq.0.0: inactive                              
          gt.0.0: scale factor on thickness             

    beam spotweld radius scale factor for thinning.    0.0000E+00
          eq.0.0: inactive                              
          gt.0.0: scale factor on radius                

    read in smooth contact flags...................       0
          eq.0:  no
          eq.1:  yes
          Warning: in Shared Memory Program smooth option only 
          available for Forming type  contact

    flag for eliminating faces on symmetry planes..       0
          eq.0:  use all faces                          
          eq.1:  delete faces from contact              

    spotweld tension scaling load curve............       0
    spotweld compression scaling load curve........       0
    spotweld direction scaling table.(tension).....       0
    spotweld direction scaling table (shear)  .....       0
          eq.0:  table for tension scaling is used      
    spotweld print flag (on=1).....................       0

    number of contact volume definitions...........       0

    flag to use one way node to surface erosion....       0

    flag for implicit rigidwall gap stiffness......       1

          eq.1:  add initial gap stiffness              
          eq.2:  do not add gap stiffness               

    death time for gap stiffness...................    0.5000E+00

    penalty scale factor for rigid walls...........    0.1000E+01

    flag for covariant contact formulation.........       0

          eq.0:  covariant formulation not used         
          eq.1:  covariant formulation used             

    flag for offsetting thick thermal contact      
    surfaces in the thermal contacts...............       0

          eq.0:  no offset, if thickness is not included
                 contact will act on shell mid-surface  
          eq.1:  offsets are applied so that contact    
                 always act on the shell outer surfaces 

    flag for shell segment edge shape..............       0
          eq.0:  shell edges assumed round (default)    
          eq.1:  shell edges assumed square             

    segment based contact PSTIFF option............       0
          eq.0:  use the material density (default)     
          eq.1:  use nodal masses                       

    flag for consistent thermal contact algorithm..       1
          lt.0:  conduction evenly distributed (pre-R4) 
          eq.1:  conduction weighted by shape functions,
                 reduced integration (default)          
          eq.2:  conduction weighted by shape functions,
                 full integration                       

    flag for optional tied interface update .......       0
          eq.0:  integrate accelerations for v and u    
          eq.1:  differentiate u to obtain v and a      

    flag for overlapping force transducers.........       0
          eq.0:  forces applied to first found (faster) 
          eq.1:  forces applied to all transducers      

    scale factor for contact interface mass scaling    0.0000E+00
    shell thickness scale factor for rigidwall ....    0.0000E+00
    flag of contact involving isogeometric ele ....       0
          eq.0:  interp. node vs. interp. facet         
          eq.1:  interp. node vs. isogeometric element  
    print out penetration info for mortar contact..       0
    scale factor for contact pressure on thickness
    shells.........................................    0.1000E+01
    convert spc on mat_rigid and                   
    constrained_nodal_rigid_body to bpm for        
    output to bndout...............................       0
          eq.0: do not convert                          
          eq.1: convert                                 
    output contact penetrations to d3plot          
    and sleout.....................................       0
          eq.0: no output                               
          ge.1: output absolute penetrations            
          ge.2: output relative penetrations            


    CONTROL CARD 16. Computation Options-Parallel

    number of cpus for parallel computations.......      31

    parallel right hand side assembly..............       0
          eq.0:  on  (default)                          
          eq.1:  off                                    

    flag for automatic subcycling..................       0
          eq.0:  off (default)                          
          eq.1:  on                                     

    number of part IDs for mass scaled subcycling..       0

    flag for repeatability in parallel solution....       2
          eq.1:  on  (ordered RHS summation-slower)     
          eq.2:  off (default)                          

    use memory to parallelize repeatability option.       0
          eq.0:  off                                    
          eq.1:  on                                     
    maximum time step factor for subcycling........       0


    CONTROL CARD 17. Computation Options-Coupling

    length conversion factor coupling..............    0.1000E+01

    time conversion factor coupling................    0.1000E+01

    force conversion factor coupling...............    0.1000E+01

    material repositioning flag....................       0
          eq.0:  off                                    
          eq.1:  input data defines repositioning       
          eq.2:  no repositioning of defined nodes      

    Flag to flip X-coordinates.....................       0

    Flag to flip Y-coordinates.....................       0

    Flag to flip Z-coordinates.....................       0

    Idle time for LS-DYNA..........................    0.0000E+00

    Implicit coupling for springback...............       0
          eq.0:  off (default)                          
          eq.1:  on                                     
          eq.2:  seamless springback                    

          eq.12: seamless springback                    

    DYNAIN output format...........................       0
          eq. 0:  ascii                                 
          eq. 1:  binary                                
          eq. 2:  ascii and binary                      
          eq.10:  ascii (large)                         
          eq.11:  binary (large internal ASCII)         
          eq.12:  ascii and binary (large)              

    Mismatched acoustic coupling input flag........       0
          eq.0:  off                                    
          eq.1:  on                                     

    Two sided acoustic coupling input flag.........       0
          eq.0:  off                                    
          eq.1:  on                                     

    Coupling with USA..............................       0
          eq.0:  off (default)                          
          eq.1:  on                                     

    Number of steps for CAL3D/MADYMO3D subcycling..       1

    Number of MCOL coupled rigid bodies............       0

    Number of vehicles to be initialized...........       0

    Coupling with CFD..............................       0
          eq.0:  off (default)                           
          eq.1:  FAST3D                                  
          eq.2:  boundary element method                 


    CONTROL CARD 18. Computation Options-Output Control

    printout of node, element, velocity input data.       0
          eq.0:  on                                      
          eq.1:  off                                     

    time zero printout of element time step size...       0
          eq.0:  no printout                             
          eq.1:  print dt for each element at t=0        

    problem status report interval in printer file.     100

    number of cycles between restart dumps.........99999999

    number of cycles between running restart dumps.99999999

    number of files to rewrite running restart ....       1

    printout of force types to bndout file.........
          eq.0:  on                                      
          eq.1:  off                                     
                nodal force groups.................       0
                concentrated nodal forces..........       0
                pressure boundary conditions.......       0
                disp/vel/acc nodal BC..............       0


    node and element printout suppression..........       0
          eq.1:  nodal data is not echoed                
          eq.2:  element data is not echoed              
          eq.3:  node and element data is not echoed     

    debug information in messag file option........       0
          eq.0:  no                                      
          eq.1:  yes                                     

    update of beam reference nodes.................       0
          eq.0:  off                                     
          eq.1:  on-unique reference nodes required      

    averaged acceleration-print/time history files.       0
          eq.0:  no average (default)                   
          eq.1:  averaged between output intervals      
          eq.2:  user defined filtering                 

    output interval for interface file.............    0.5000E-01

    default print flag for the RBDOUT/MATSUM files        0
          eq.0: RBDOUT and MATSUM       
          eq.1: RBDOUT only             
          eq.2: MATSUM only             
          eq.3: no output               

    include eroded and lumped mass in MATSUM ......       0
          eq.0:  no                                     
          eq.1:  yes                                    

    include 10-node connectivities in D3PLOT ......       2
          eq.1:  yes                                     
          eq.2:  no                                      

    write spring forward database at termination...       0
          eq.0:  no                                      
          eq.1:  include all deformable nodes            
          eq.2:  include nodes of material subset        

    d3plot and d3thdt binary output format.........       0
          eq.0 default                                   
          eq.1 32ieee                                    

    flush output file interval.....................    5000

    output interval for d3part database............    0.0000E+00

    interval via load curve for part database......       0

    number of part blocks..........................       0

    number of solids output to part database ......       0

    number of beams  output to part database ......       0

    number of shells output to part database ......       0

    number of thick shells output to part database.       0

    Maximum number of messages.....................       0

    Print flag for digitized curve data............       0

    Print info. of 1d belt created for 2d belt.....       0

    ELOUT shell output coordinate system flag......       0

          eq.0 default                                  
          eq.1 local element coordinate system          
          eq.2 global coordinate sytstem                
    number of parts removed from d3plot ...........       0

    number of levels of timing at termination .....       2

    max frequency of element failure summaries.....       1

    shell element stress extrapolation.............       0

          eq.0 default: no extrapolation
          eq.1 extrapolate stress for linear materials only
          eq.2 extrapolate stress if plastic strain is zero
          eq.3 extrapolate stress always
          eq.4 extrapolate all history variables

    solid element stress extrapolation.............       0

          eq.0 default: no extrapolation
          eq.1 extrapolate stress for linear materials only
          eq.2 extrapolate stress if plastic strain is zero
          eq.3 extrapolate stress always
          eq.4 extrapolate all history variables

    phase change output control....................       0
          eq.0 default: no messag

          eq.1 write out element ID at time of phase change
    DEM density output control.....................       0
          eq.0 default: no messag
          eq.1 write out density data

    quadratic solid element output.................       0
          eq.0:  default to lower order output only      
          eq.1:  write out connectivies for geometry     
                 no extra integration data written       
          eq.2:  write out connectivies for geometry +   
                 extra integration points                

    cubic solid element output.....................       0
          eq.0:  default to lower order output only      
          eq.1:  write out connectivies for geometry     
                 no extra integration data written       
          eq.2:  write out connectivies for geometry +   
                 extra integration points                

    names of history variables listed per part.....       0
          eq.0:  no                                      
          eq.1:  in d3hsp                                
          eq.2:  in d3hsp and in file hisnames.xml       

    results output for deleted elements ...........       0
          eq.0 default: off
          eq.1 on



    CONTROL CARD 19. Computation Options-Output Energy

    hourglass energy calculation...................       0
          eq.1:  off (default)                          
          eq.2:  on                                     

    rigid wall energy calculations.................       1
          eq.1:  off (default)                          
          eq.2:  on                                     

    contact energy calculation.....................       2
          eq.1:  off                                    
          eq.2:  on                                     

    flag for rayleigh damping energy calculations..       0
          eq.1:  off (default)                          
          eq.2:  on                                     

    flag for reference geometry energy calculations       0
          eq.1:  off                                    
          eq.2:  on (default)                           

    material energy details .......................       0
          eq.1:  off (default)                          
          eq.2:  on                                     

    flag for material energy in D3THDT file........       2
          eq.1:  off                                    
          eq.2:  on  (default)                          


    CONTROL CARD 20. Computation Options-LS-POST Database

    time step between dumps of complete state data.    0.5000E+00

    output interval for interface force database...    0.5000E+00

    time step between dumps of time history data...    0.0000E+00

    number of nodal printout blocks................       0

    number of solid element printout blocks........       0

    number of beam element printout blocks.........       0

    number of discrete element printout blocks.....       0

    number of seatbelt element printout blocks.....       0

    number of shell element printout blocks........       0

    number of thick shell element printout blocks..       0

    load curve-interval between state data dumps...       0

    behavior of state data dump curve..............       1
          eq.1:  load curve value added to current time 
          eq.2:  plot time T=current t+curve at T       
          eq.3:  plot at each ordinate point            

    load curve-interval between force data dumps...       0

    load curve-interval between history data dumps.       0

    flag, user output into shell resultant vector..       0
          eq.1:  off (default)                          
          eq.2:  on, user subroutine is called           

    number of subsystems for SSSTAT file ..........       0

    behavior of intfor data curve..................       1
          eq.1:  load curve value added to current time 
          eq.2:  plot time T=current t+curve at T       
          eq.3:  plot at each ordinate point            


    CONTROL CARD 21. Computation Options LS-POST Database

    flag to write ls-post database during dyn rel..       0
          eq.0:  no database write (default)            
          eq.1:  write database at convergence check    
          eq.n:  write database at nth check            

    number of extra history variables for solids...       0

    number of integration points output/solid .....       1

    number of extra history var/int.pt for shells..       0

    number of integration points output/shell .....       3
          lt.0:  also output 4 points in plane          

    flag for including strain tensor in database...       1
       STRFLG[NML] = L + M*10 + N*100
            eq.0:  exclude (default)                    
          L.eq.1: Write strain tensor data to d3plot & elout
          M.EQ.1: Write plastic strain data to d3plot   
          N.EQ.1: Write thermal strain data to d3plot   

    flag for including stress tensor in database...       1
          eq.1:  include (default)                      
          eq.2:  exclude for shells, include for solids 
          eq.3:  exclude for shells and solids          

    flag for including effective plastic strain....       1
          eq.1:  include (default)                      
          eq.2:  exclude for shells, include for solids 
          eq.3:  exclude for shells and solids          

    flag for including shell resultants............       1
          eq.1:  include (default)                      
          eq.2:  exclude                                

    flag for including shell energy and thickness..       1
          eq.1:  include (default)                      
          eq.2:  exclude                                

    every state is written to a separate file......       0
          eq.0:  off (default)                          
          eq.1:  only one state per plotfile            

    composite material stress output ..............       0
          eq.-1:  same as 1, but fiber stress and strain
                  are engineering measured in material  
                  34                                    
          eq. 0:  global                                
          eq. 1:  local                                 
          eq. 2:  local, additional information         
                  output in place of shell resultants   

    number of integration points output/beam ......       0

    data compression to eliminate rigid body data..       1
    nodal velocities, and nodal accelerations      
          eq.1:  off                                    
          eq.2:  on -rigid bodies                       
          eq.3:  off-rigid bodies-on nodal data         
          eq.4:  on -rigid bodies-on nodal data         

    output shell element hourglass energy..........       1
          eq.1:  off                                    
          eq.2:  on                                     

    output shell element dt, mass, added mass......       2
          eq.1:  off                                    
          eq.2:  output dt                              
          eq.3:  output mass                            

    peak pressure flag.............................       0
          eq.1:  on                                     

    filter parameter...............................    0.1000E+01

    flag for solid element additional output.......       0
          eq.1:  output 3 additional variables          
          eq.2:  output 5 additional variables          
          eq.4:  output 7 additional variables          

    flag for scaled mass output to the d3plot file.       0
          eq.1:  output mass increment                  
          eq.2:  output percentage increase             

    flag for thermal data..........................       1
          eq.0 or 1: output temperature                 
          eq.2: output temperature and flux             
          eq.3: output temp, flux, and thick shell temps

    flag for including stress tensor at int. point        0
          eq.0:  exclude (default)                      
          eq.1:  include stress (solid and shells)      

    flag for including stress tensor at nodes .....       0
          eq.0:  exclude (default)                      
          eq.1:  include local stress (solid and shell) 
          eq.2:  include global stress (solid and shell)

    flag for including strain tensor at int. point        0
          eq.0:  exclude (default)                      
          eq.1:  include strains (solid and shells)     

    flag for including strain tensor at nodes .....       0
          eq.0:  exclude (default)                      
          eq.1:  include local strain (solid and shell) 
          eq.2:  include global strain (solid and shell)
    output interval for blast force database.......    0.0000E+00
          lt.0:  interval specified by load curve       


    CONTROL CARD 22. Computation Options-ASCII Output I

    output interval for cross section forces.......    0.0000E+00
    output interval for rigid wall forces .........    0.0000E+00
    output interval for nodal print blocks.........    0.5000E+00
    output interval for element print blocks.......    0.5000E+00
    output interval for global statistics .........    0.5000E+00
    output interval for subsystem statistics ......    0.0000E+00
    output interval for discrete elements..........    0.0000E+00
    output interval for material summaries.........    0.0000E+00
    output interval for nodal interface forces.....    0.0000E+00
    output mass properties in subsystem statistics.             0
    output mass properties in global statistics....             0
    additional history variables output-solids.....             0
    additional history variables output-shells.....             0
    additional history variables output-tshells....             0
    additional history variables output-beams......             0



    CONTROL CARD 23. Computation Options-ASCII Output II

    output interval for resultant interface forces.    0.0000E+00
    output interval for smug nodal data............    0.0000E+00
    output interval for sp constraint forces.......    0.5000E+00
    output interval for nodal constraint forces....    0.0000E+00
    output interval for airbag statistics..........    0.0000E+00
    output interval for avs filter.................    0.0000E+00
    output interval for nodal force groups.........    0.0000E+00
    output interval for b.c. forces and energy ....    0.5000E+00



    CONTROL CARD 24. Computation Options-ASCII Output III

    output interval for rigid body data............    0.0000E+00
    output interval for geometric contact entities.    0.0000E+00
    output interval for mpgs  database.............    0.0000E+00
    output interval for movie database.............    0.0000E+00
    output interval for interface energies.........    0.0000E+00
    output interval for seatbelt response..........    0.0000E+00
    output interval for joint forces...............    0.0000E+00
    output interval for tracer particles...........    0.0000E+00
    output interval for discrete beam data.........    0.0000E+00
    output type for discrete beam data ............       0
    curve id for discrete beam data ...............       0
    option for ascii output time for discrete beam.       0

    output interval for pulley element data........    0.0000E+00
    output type for pulley element data ...........       0
    curve id for pulley element data ..............       0
    option for ascii output time for pulley element       0

    output interval for bearing element data........    0.0000E+00
    output type for bearing element data ...........       1
    curve id for bearing element data ..............       0
    option for ascii output time for bearing .......       0

    output interval for des mass flow data..........    0.0000E+00
    output type for des mass flow data .............       1
    curve id for des mass flow data ................       0
    option for ascii output time for des mass flow..       0

    output interval for curvout ....................    0.0000E+00
    output type for curvout ........................       1
    curve id for curvout ...........................       0
    option for ascii output time for curvout .......       0

    output interval for SPH mass flow data..........    0.0000E+00
    output type for SPH mass flow data .............       1
    curve id for SPH mass flow data ................       0
    option for ascii output time for SPH mass flow..       0



    CONTROL CARD 25. CONTROL_ALE 1st card

    Default continuum treatment....................       0
         eq.-1: Improved Advection
         ne.-1: Default advection (Legacy)
    Number of cycles between rezones...............       0

    Advection formulation..........................       0
         eq.1: Donor Cell + HIS
         eq.2: Van Leer + HIS (default)

    Relaxation factor 1 (simple average)...........   -0.1000E+01

    Relaxation factor 2 (volume weighting).........    0.0000E+00

    Relaxation factor 3 (isoparametric)............    0.0000E+00

    Relaxation factor 4 (equipotential)............    0.0000E+00

    Relaxation factor 5 (equilibrium)..............    0.0000E+00


    CONTROL CARD 26. CONTROL_ALE 2nd card

    time to begin rezoning.........................    0.0000E+00

    time to end rezoning...........................    0.0000E+00

    SALE advection factor..........................    0.0000E+00

    Void factor....................................    0.1000E-05

    Pressure equilibrium...........................       0
         eq.0: Off
         eq.1: On

    Automatic euler boundary condition flag........    0.0000E+00
         eq.0: Off.
         eq.1: On with stick condition.
         eq.2: On with slip condition.

    Reference pressure.............................    0.0000E+00

    Node set excluded from EBC (see NSIDEBC).......       0


    CONTROL CARD 26. CONTROL_ALE 3rd card

    Number of cycles between ALE coupling..........       1

    Number of cycles between ALE bucket sort.......      50

    A flag to control mass scaling for ALE parts...       0

    A flag to control pressure locking pattern.....    0.0000E+00

    BEAMIN flag....................................       0

    Reference pressure by ALE group..see load curve       0

    Max. pressure difference to cancel nodal forces    0.0000E+00

    Dynamic viscous time step factor (DTMU)........    0.0000E+00


    CONTROL CARD 26. CONTROL_ALE 4th card

    Flag to optimize the coupling MPP..............       0

    Flag to include ALE in the dynamic relaxation..       0

    Number of ALE groups allowed to flow in.......:       0
         ALE group:


    CONTROL CARD 26. Other ALE parameters

    Number of multi-material Euler groups..........       0

    number of void materials.......................       0

    Number of non-interacting Euler materials......       0

    Number of parts considered in ALE convection...       0

    Number of ALE Multi-material group switching...       0

    Number of ALE mixing length....................       0

    Number of ALE coupling to nodes ...............       0

    Number of ALE essential boundaries ............       0

    Number of ALE tracer particles ................       0

    Output interval for euler statistics...........    0.0000E+00


    CPM output format..............................      11
         eq.11: Version 3 (full output)
         eq.21: Version 4 (full output)
         eq.22:           (coordinates)
         eq.23:           (summary)
    # of CPM airbag interaction....................       0

    # of cycle for CPM repartition.................       5
    CPM time step control..........................       0
         eq.0: no control
         eq.1: set CPM timestep size as 1 usec
    CPM check bag and chamber connectivity.........       0
         eq.0: no
         eq.1: yes (error termination if detected)
    CPM rebalancing option.........................       0
         eq.0: no
         eq.1: yes
    Scale factor of force decay constant...........    0.1000E+01
    Adjust energy due to rigid body motion.........       0
         eq.0: no (default)
         eq.1: yes



    PG output format...............................      11
         eq.11: Version 3 (full output)
         eq.21: Version 4 (full output)
         eq.22:           (coordinates)
         eq.23:           (summary)
    # of PG airbag interaction.....................       0

    # of cycle for PG repartition..................       5
    PG time step control...........................       0
         eq.0: no control
         eq.1: set PG timestep size as 1 usec


    CONTROL CARD 37. SPH 1st card 

    Sort frequency.................................       0

    Box activation.................................       0

    First option...................................    0.0000E+00

    Space dimension................................       0

    Memory allocation for neighbors MEMORY.........       0
           allocation type:........................ DYNAMIC

    Particle approximation.........................       0
         eq.0: Standard gather form (Lacome-Vila 1998)
         eq.1: Renormalization (Ben Moussa-Vila 1998)
         eq.2: Symmetric formulation (Benz 1989)         
         eq.3: Symmetric renormalization (Libersky 1993) 
         eq.4: Elliptic smoothing length                 
         eq.5: Fluid formulation                         
         eq.6: Renormalized fluid formulation            
         eq.7: Total Lagrangian formulation              
         eq.8: Renormalized Total Lagrangian formulation 
         eq.9: Adaptive SPH formulation                  
         eq.10: Renormalized adaptive SPH formulation    
         eq.12: Moving least-squares based formulation   
         eq.13: Implicit incompressible formulation      
         eq.15: Enhanced fluid formulation               
         eq.16: Renormalized enhanced fluid formulation  

    Start time of SPH analysis.....................    0.0000E+00

    Maximum velocity...............................    0.0000E+00

    Contact definition between SPH parts...........       0
         eq.0: Approximation is computed
         eq.1: Approximation is not computed

    Time derivative for smoothing length...........       0
    Initial smooth length computation option.......       0
    Display options for SPH particles..............       0
    Erosion control option for SPH particles.......       0
    Contact treatment for deactivated particles....       0
         eq.0: Contact remains active
         eq.1: Contact becomes inactive

    Artificial viscosity for SPH particles.........       0
         eq.0: Monaghan type bulk viscosity (change
                   to bulk coefficents recommended)
         eq.1: Solid elements type bulk viscosity
    Thickness option for contact...................       0
    Total MLS stabilization flag...................       0
    SPH Pressure smoothing parameter...............       0



    CONTROL CARD 50. EFG 

    ispline .......................................       0

    idila..........................................       0

    inint..........................................       0

    iefgs..........................................       0

    intfs..........................................       0
 
 *** Warning 20471 (STR+471)
     Hourglass formulation for part # 1
     has been switched to type 6 since other
     formulations do not have a stiffness matrix.



 p a r t   d e f i n i t i o n s

 material type                         
     eq.1   isotropic                  
     eq.2   orthotropic                
     eq.3   elastoplastic ( von mises )
     eq.4   thermo-elastic-plastic     
     eq.5   soil and crushable foam model   
     eq.6   viscoelastic model         
     eq.7   blatz-ko finite elastic rubber  
     eq.8   high explosive model       
     eq.9   null material              
     eq.10  hydrodynamic - elastic-plastic  
     eq.11  steinberg - guinan model   
     eq.12  isotropic elastic-plastic  
     eq.13  elastic-plastic with failure    
     eq.14  crushable foam with failure    
     eq.15  johnson/cook plasticity model  
     eq.16  pseudo tensor geological model  
     eq.17  elastoplastic with fracture
     eq.18  power law isotropic plasticity  
     eq.19  strainrate sensitive plasticity 
     eq.20  rigid material             
     eq.21  thermal orthotropic(12 constants)
     eq.22  composite material damage model 
     eq.23  thermal orthotropic(12 curves)  
     eq.24  piecewise linear plasticity     
     eq.25  soil cap model by taylor        
     eq.26  crushable metallic honeycomb    
     eq.27  hyperelastic mooney-rivlin      
     eq.28  shell/beam resultant plasticity 
     eq.29  beam resultant force limited    
     eq.30  shape-memory alloy              
     eq.31  frazer-nash rubber model        
     eq.32  safety glass                    
     eq.33  barlat's anisotropic plasticity
     eq.34  fabric                          
     eq.35  elastoplastic (green-naghdi rate)
     eq.36  barlat's 3-parameter plasticity
     eq.36E extended barlat plasticity      
     eq.37  anisotropic plasticity model    
     eq.38  blatz-ko finite elastic foam    
     eq.39  fld anisotropic plasticity      
     eq.40  nonlinear orthotropic elastic   
     eq.41-50  user material models         
     eq.51  bammann plasticity model        
     eq.52  sandia damage model             
     eq.53  crushable cellular foam         
     eq.54  composite damage model(hashin)  
     eq.55  composite damage model(tsai-wu) 
     eq.57  low density urethane foam       
     eq.58  laminated composite fabric      
     eq.59  composite failure               
     eq.60  viscous glass model model       
     eq.61  maxwell/kelvin viscoelastic     
     eq.62  viscous foam model              
     eq.63  crushable foam model            
     eq.64  rate sensitive powerlaw plasticity
     eq.65  modified armstrong-zerrilli model 
     eq.66  elastic resultant beams           
     eq.67  nonlinear elastic via load curves 
     eq.68  plastic resultant via load curves 
     eq.69  sid impact dummy damper           
     eq.70  hydraulic/gas damper              
     eq.71  cable                             
     eq.72  k & c concrete damage             
     eq.73  low density viscous foam          
     eq.74  elastic spring discrete beam      
     eq.75  bilkhu/dubois crushable foam      
     eq.76  linear viscoelastic               
     eq.77  general hyperelastic/ogden        
     eq.78  soil/concrete                     
     eq.79  hysteretic soil                   
     eq.80  ramberg-osgood                    
     eq.81  plastic damage model              
     eq.82  plastic orthotropic damage model  
     eq.83  fu-chang rate sensitive foam model
     eq.84  reinforced concrete (aea winfrith, 1990)
     eq.86  orthotropic viscoelastic             
     eq.87  cellular viscoelastic rubber         
     eq.88  material threshold stress (mts)      
     eq.89  plasticity polymer                   
     eq.90  acoustic media                       
     eq.91  hyperelastic soft tissue             
     eq.92  visco-hyperelastic soft tissue       
     eq.93  elastic 6-dof spring                 
     eq.94  inelastic spring discrete beam       
     eq.95  inelastic 6-dof spring               
     eq.96  brittle damage                       
     eq.97  general joint discrete beam          
     eq.98  simplified johnson cook              
     eq.99  simplified johnson cook with damage  
     eq.100 spotweld material                    
     eq.101 ge rate sensitive plasticity         
     eq.102 inverse hyperbolic sine              
     eq.103 viscoplastic model (ntnu, 1996)      
     eq.104 damage model 1 (ntnu, 1997)          
     eq.105 damage model 2 (ntnu, 1997)          
     eq.106 elastic viscoplastic thermal         
     eq.107 modified johnson cook                
     eq.108 orthotropic elastic plastic          
     eq.110 johnson/holmquist ceramics           
     eq.111 johnson/holmquist concrete           
     eq.112 finite elastic strain plasticity     
     eq.113 trip for austenitic stainless        
     eq.114 layered piecewise linear plasticity  
     eq.115 unified creep                        
     eq.116 composite lay up                     
     eq.117 composite matrix                     
     eq.118 composite direct                     
     eq.119 general nonlinear 6dof discrete beam 
     eq.120 gurson                               
     eq.121 general nonlinear 1dof discrete beam 
     eq.122 hill 3r                              
     eq.123 modified piecewise linear plasticity 
     eq.124 compression-tension plasticity       
     eq.125 yoshida kinematic plasticity model   
     eq.126 crushable metallic honeycomb         
     eq.127 arruda-boyce hyper-viscoelastic      
     eq.128 heart tissue                         
     eq.129 lung hyper-viscoelastic              
     eq.130 special orthotropic                  
     eq.131 tno isotropic smeared crack model    
     eq.132 tno orthotropic smeared crack model  
     eq.133 barlat yld2000                       
     eq.135 wtm/stm                              
     eq.136 orthotropic vegter model             
     eq.137 anisotropic ito-goya model           
     eq.139 modified resultant beam force limited
     eq.140 vacuum                               
     eq.141 rate sensitive polymer               
     eq.142 transversly isotropic crushable foam 
     eq.143 aptek orthotropic wood               
     eq.144 pitzer crushable foam                
     eq.145 continuous surface cap with damage   
     eq.146 1dof generalized spring              
     eq.147 fhwa soil                            
     eq.148 gas mixture                          
     eq.150 cfd - constant properties            
     eq.152 hyperbolic tangent thermal           
     eq.153 damage model 3                       
     eq.154 deshpande fleck foam model           
     eq.155 compression-tension eos model        
     eq.156 muscle model                         
     eq.157 anisotropic elastic plastic          
     eq.158 rate sensitive composite fabric      
     eq.159 continuous surface cap               
     eq.161 composite msc                        
     eq.162 composite dmg msc                    
     eq.163 modified crushable foam              
     eq.164 brain linear viscoelastic            
     eq.165 plastic nonlinear kinematic          
     eq.166 moment curvature beam                
     eq.167 mccormick                            
     eq.168 polymer                              
     eq.169 arup adhesive                        
     eq.170 resultant anisotropic                
     eq.171 steel concentric brace               
     eq.172 concrete ec2                         
     eq.173 mohr couloumb                        
     eq.174 rc beam                              
     eq.176 quasilinear viscoelastic             
     eq.177 hill foam                            
     eq.178 viscoelastic hill foam               
     eq.179 low density synthetic foam           
     eq.180 low density synthetic foam ortho     
     eq.181 simplified rubber model              
     eq.182 viscoelastic plastic model           
     eq.187 semi-analytical model for polymers   
     eq.188 thermo elastic viscoplastic creep    
     eq.189 anisotropic thermo elastic           
     eq.190 barlat 3-parameter fld plasticity    
     eq.191 seismic beam                         
     eq.192 soil brick                           
     eq.193 drucker prager                       
     eq.194 rc shear wall                        
     eq.195 concrete beam                        
     eq.196 general spring discrete beam         
     eq.197 seismic isolator                     
     eq.198 jointed rock                         
     eq.199 barlat yld2004                       
     eq.202 steel EC3                            
     eq.203 hysteretic reinforcement             
     eq.205 discrete beam surface contact        
     eq.206 Park Ang beam                        
     eq.208 bolt beam                            
     eq.213 composite tab. plast. damage v1.3.5  
     eq.214 dry fabric                           
     eq.215 4A micromec                          
     eq.219 codam2                               
     eq.220 rigid material discrete particles    
     eq.221 orthotropic simplified damage        
     eq.222 genoa material for laminates         
     eq.223 orthotropic advanced damage          
     eq.224 tabulated johnson cook               
     eq.225 viscoplastic mixed hardening         
     eq.230 elastic pml                          
     eq.231 acoustic pml                         
     eq.232 biot hysteretic                      
     eq.233 cazacu barlat                        
     eq.234 viscoelastic loose fabric            
     eq.235 micromechanics dry fabric            
     eq.236 silicon carbid coating on RCC        
     eq.237 hysteretic pml                       
     eq.242 barlat yld2000 Yoshida hardening     
     eq.243 hill 90                              
     eq.244 ultra high strength steel            
     eq.248 press hardening steel bmw model      
     eq.249 reinforced thermoplastic             
     eq.250 aedm (working name)                  
     eq.251 tailored properties                  
     eq.252 toughened adhesive polymer           
     eq.255 piecewise linear plastic thermal     
     eq.256 amorphous solids finite stain        
     eq.258 non quadratic with failure           
     eq.260 Stoughton non-associated flow        
     eq.261 laminated fracture daimler pinho     
     eq.262 laminated fracture daimler camanho   
     eq.263 Lou-Yoon                             
     eq.264 tabulated johnson cook ortho plastic 
     eq.265 constrained spr                      
     eq.266 tissue dispersed                     
     eq.267 eight chain rubber                   
     eq.269 bergstrom-boyce rubber model         
     eq.270 computational welding mechanics model
     eq.271 powder compaction model              
     eq.272 RHT concrete                         
     eq.273 CDPM concrete                        
     eq.274 paper                                
     eq.275 smooth viscoelastic viscoplastic     
     eq.279 cohesive paper                       
     eq.291 energy based shape memory alloy      
     eq.295 anisotropic hyperelastic             
     eq.300 implicit SPH fluid                   
     eq.301 implicit SPH structure               
     eq.326 cohesive gasket                      
 equation-of-state types              
     eq.1   linear polynomial         
     eq.2   jwl high explosive        
     eq.3   sack tuesday high explosive    
     eq.4   gruneisen                 
     eq.5   ratio of polynomials      
     eq.6   linear polynomial with source  
     eq.7   initiation and reaction in he  
     eq.8   compaction                
     eq.9   tabulated                 
     eq.11  tensor pore collapse      
     eq.14  jwlb high explosive       
     eq.15  one-dimensional gasket    
     eq.16  mie-gruneisen with p-alpha
 hourglass models                                    
     eq.1   viscous                                  
     eq.2   flanagan-belytschko viscous form         
     eq.3   full flanagan-belytschko viscous form    
            (constant stress solid elements)         
     eq.4   flanagan-belytschko stiffness form       
     eq.5   full flanagan-belytschko stiffness form  
     eq.6   bindeman-belytschko stiffness form       
            (solid 2d and 3d elements)               
     eq.7   linear total strain stiffness form       
            (solid 2d and 3d elements)               
     eq.9   puso stiffness form (solid 3d elements)  
     eq.10  cosserat total strain stiffness form     
            (solid 3d elements)                      
 bulk viscosity models                
     eq.1   standard                  
 defaults                                  
     hourglass model.(thin shells).........    4
     hourglass model.(bricks)..............    6
     hourglass model.(thick shells)........    2
     hourglass coefficient................. 1.00000E-01
     bulk viscosity type...................    1
     quadratic bulk viscosity coefficient.. 1.50000E+00
     linear bulk viscosity coefficient..... 6.00000E-02

 ***********************************************************************


 boxsolid                                                                

 part     id ..................... 1
 section  id ..................... 1
 material id ..................... 1
 section  title .................. 
                                                                                 
 material title .................. 
                                                                                 
           material type ..............     1     
           equation-of-state type .....     0
           hourglass type .............     6
           bulk viscosity type ........     1
     density .......................... = 1.00000E+03
     hourglass coefficient ............ = 1.00000E-01
     quadratic bulk viscosity ......... = 1.50000E+00
     linear bulk viscosity ............ = 6.00000E-02
     element type ..................... =    0
          eq.0: 4, 6, 8, 10-node solid element
          eq.1: 2-node beam or truss or 2D shell element
          eq.2: 3, 4-node membrane/shell or 2D continuum element
          eq.3: 8-node thick shell element 
          eq.4: SPH element 
     flag for bulk viscosity in shells. =    0
     flag for rbdout/matsum  output ... =    0
          eq.0: rbdout and matsum       
          eq.1: rbdout only             
          eq.2: matsum only             
          eq.3: no output               
     static coefficient of friction ... = 0.00000E+00
     kinetic coefficient of friction... = 0.00000E+00
     exponential decay coefficient .... = 0.00000E+00
     viscous friction coefficient ..... = 0.00000E+00
     optional contact thickness ....... = 0.00000E+00
     optional thickness scale factor... = 0.00000E+00
     local penalty scale factor........ = 0.00000E+00
     optional beam to beam cparm8...... =           0
     flag for adaptive remeshing ...... =           0
          eq.0: inactive                    
          eq.1: h-adaptive only             
          eq.2: r-adaptive only             
     relative offset of cohesive            
     reference surface .................= 0.00000E+00
     gasket element thickness ..........= 0.00000E+00
     rayleigh damping coefficient...... = 0.00000E+00
     hourglass damping coefficient..... = 0.00000E+00
     e ................................ = 1.00000E+06
     vnu .............................. = 4.99900E-01
     for belytschko-schwer beam only     
     ga, axial damping factor ......... = 0.00000E+00
     gb, bending damping factor ....... = 0.00000E+00
     solid  formulation ............... =    1
         eq.-18: 8  point integration-3dof/node 
                 incompatible modes (C3D8I)     
          eq.-2: 8  point integration-3dof/node 
                 for poor aspect ratio elements 
          eq.-1: 8  point integration-3dof/node 
                 for poor aspect ratio elements 
                 (efficient variant of -2 but   
                 prone to some hourglassing)    
          eq. 1: 1  point integration           
          eq. 2: 8  point integration-3dof/node 
          eq. 3: 14 point integration-6dof/node 
          eq. 4: 5  point tetrahedron-6dof/node 
          eq. 5: 1  point ale                   
          eq. 6: 1  point eulerian              
          eq. 7: 1  point eulerian ambient      
          eq. 8: 1  point acoustic              
          eq. 9: 1  point corotational          
          eq.10: 1  point tetrahedron           
          eq.11: multi-material eulerian        
          eq.12: eulerian with void             
          eq.13: nodal pressure tetrahedron     
          eq.14: 8  point acoustic              
          eq.15: 2  point pentahedron           
         eq.115: 1  point pentahedron           
          eq.16: 10-node quadratic tetrahedron  
          eq.17: 10-node composite tetrahedron  
          eq.18: linear static element          
          eq.19: 8-node 2x2 cohesive            
          eq.20: 8-node 2x2 cohesive with offsets for shells
          eq.21: 6-node 1x1 cohesive            
          eq.22: 6-node 1x1 cohesive with offsets for shells
          eq.23: 20-node quadratic hexahedron  
          eq.41: efg 3d                         
          eq.42: efg 3d for 4-noded background  
          eq.43: mesh-free enriched finite element 
          eq.46: CE/SE Eulerian compressible N-S
          eq.47: smoothed particle Galerkin method 
          eq.99: elastic vibration element      
     corotational local coord. ........ =    0
          eq. 0: not requested                  
          eq. 1: requested                      








 n o d a l   p o i n t   c o o r d i n a t e s 
   node ID   trnbc          x-ord          y-ord          z-ord   rotbc
         1     0.0     0.0000E+00     0.0000E+00     0.0000E+00     0.0
         2     0.0     0.3333E+02     0.0000E+00     0.0000E+00     0.0
         3     0.0     0.6667E+02     0.0000E+00     0.0000E+00     0.0
         4     0.0     0.1000E+03     0.0000E+00     0.0000E+00     0.0
         5     0.0     0.0000E+00     0.3333E+02     0.0000E+00     0.0
         6     0.0     0.3333E+02     0.3333E+02     0.0000E+00     0.0
         7     0.0     0.6667E+02     0.3333E+02     0.0000E+00     0.0
         8     0.0     0.1000E+03     0.3333E+02     0.0000E+00     0.0
         9     0.0     0.0000E+00     0.6667E+02     0.0000E+00     0.0
        10     0.0     0.3333E+02     0.6667E+02     0.0000E+00     0.0
        11     0.0     0.6667E+02     0.6667E+02     0.0000E+00     0.0
        12     0.0     0.1000E+03     0.6667E+02     0.0000E+00     0.0
        13     0.0     0.0000E+00     0.1000E+03     0.0000E+00     0.0
        14     0.0     0.3333E+02     0.1000E+03     0.0000E+00     0.0
        15     0.0     0.6667E+02     0.1000E+03     0.0000E+00     0.0
        16     0.0     0.1000E+03     0.1000E+03     0.0000E+00     0.0
        17     0.0     0.0000E+00     0.0000E+00     0.3333E+02     0.0
        18     0.0     0.3333E+02     0.0000E+00     0.3333E+02     0.0
        19     0.0     0.6667E+02     0.0000E+00     0.3333E+02     0.0
        20     0.0     0.1000E+03     0.0000E+00     0.3333E+02     0.0
        21     0.0     0.0000E+00     0.3333E+02     0.3333E+02     0.0
        22     0.0     0.3333E+02     0.3333E+02     0.3333E+02     0.0
        23     0.0     0.6667E+02     0.3333E+02     0.3333E+02     0.0
        24     0.0     0.1000E+03     0.3333E+02     0.3333E+02     0.0
        25     0.0     0.0000E+00     0.6667E+02     0.3333E+02     0.0
        26     0.0     0.3333E+02     0.6667E+02     0.3333E+02     0.0
        27     0.0     0.6667E+02     0.6667E+02     0.3333E+02     0.0
        28     0.0     0.1000E+03     0.6667E+02     0.3333E+02     0.0
        29     0.0     0.0000E+00     0.1000E+03     0.3333E+02     0.0
        30     0.0     0.3333E+02     0.1000E+03     0.3333E+02     0.0
        31     0.0     0.6667E+02     0.1000E+03     0.3333E+02     0.0
        32     0.0     0.1000E+03     0.1000E+03     0.3333E+02     0.0
        33     0.0     0.0000E+00     0.0000E+00     0.6667E+02     0.0
        34     0.0     0.3333E+02     0.0000E+00     0.6667E+02     0.0
        35     0.0     0.6667E+02     0.0000E+00     0.6667E+02     0.0
        36     0.0     0.1000E+03     0.0000E+00     0.6667E+02     0.0
        37     0.0     0.0000E+00     0.3333E+02     0.6667E+02     0.0
        38     0.0     0.3333E+02     0.3333E+02     0.6667E+02     0.0
        39     0.0     0.6667E+02     0.3333E+02     0.6667E+02     0.0
        40     0.0     0.1000E+03     0.3333E+02     0.6667E+02     0.0
        41     0.0     0.0000E+00     0.6667E+02     0.6667E+02     0.0
        42     0.0     0.3333E+02     0.6667E+02     0.6667E+02     0.0
        43     0.0     0.6667E+02     0.6667E+02     0.6667E+02     0.0
        44     0.0     0.1000E+03     0.6667E+02     0.6667E+02     0.0
        45     0.0     0.0000E+00     0.1000E+03     0.6667E+02     0.0
        46     0.0     0.3333E+02     0.1000E+03     0.6667E+02     0.0
        47     0.0     0.6667E+02     0.1000E+03     0.6667E+02     0.0
        48     0.0     0.1000E+03     0.1000E+03     0.6667E+02     0.0
        49     0.0     0.0000E+00     0.0000E+00     0.1000E+03     0.0
        50     0.0     0.3333E+02     0.0000E+00     0.1000E+03     0.0
        51     0.0     0.6667E+02     0.0000E+00     0.1000E+03     0.0
        52     0.0     0.1000E+03     0.0000E+00     0.1000E+03     0.0
        53     0.0     0.0000E+00     0.3333E+02     0.1000E+03     0.0
        54     0.0     0.3333E+02     0.3333E+02     0.1000E+03     0.0
        55     0.0     0.6667E+02     0.3333E+02     0.1000E+03     0.0
        56     0.0     0.1000E+03     0.3333E+02     0.1000E+03     0.0
        57     0.0     0.0000E+00     0.6667E+02     0.1000E+03     0.0
        58     0.0     0.3333E+02     0.6667E+02     0.1000E+03     0.0
        59     0.0     0.6667E+02     0.6667E+02     0.1000E+03     0.0
        60     0.0     0.1000E+03     0.6667E+02     0.1000E+03     0.0
        61     0.0     0.0000E+00     0.1000E+03     0.1000E+03     0.0
        62     0.0     0.3333E+02     0.1000E+03     0.1000E+03     0.0
        63     0.0     0.6667E+02     0.1000E+03     0.1000E+03     0.0
        64     0.0     0.1000E+03     0.1000E+03     0.1000E+03     0.0
        65     0.0     0.0000E+00     0.0000E+00     0.1333E+03     0.0
        66     0.0     0.3333E+02     0.0000E+00     0.1333E+03     0.0
        67     0.0     0.6667E+02     0.0000E+00     0.1333E+03     0.0
        68     0.0     0.1000E+03     0.0000E+00     0.1333E+03     0.0
        69     0.0     0.0000E+00     0.3333E+02     0.1333E+03     0.0
        70     0.0     0.3333E+02     0.3333E+02     0.1333E+03     0.0
        71     0.0     0.6667E+02     0.3333E+02     0.1333E+03     0.0
        72     0.0     0.1000E+03     0.3333E+02     0.1333E+03     0.0
        73     0.0     0.0000E+00     0.6667E+02     0.1333E+03     0.0
        74     0.0     0.3333E+02     0.6667E+02     0.1333E+03     0.0
        75     0.0     0.6667E+02     0.6667E+02     0.1333E+03     0.0
        76     0.0     0.1000E+03     0.6667E+02     0.1333E+03     0.0
        77     0.0     0.0000E+00     0.1000E+03     0.1333E+03     0.0
        78     0.0     0.3333E+02     0.1000E+03     0.1333E+03     0.0
        79     0.0     0.6667E+02     0.1000E+03     0.1333E+03     0.0
        80     0.0     0.1000E+03     0.1000E+03     0.1333E+03     0.0
        81     0.0     0.0000E+00     0.0000E+00     0.1667E+03     0.0
        82     0.0     0.3333E+02     0.0000E+00     0.1667E+03     0.0
        83     0.0     0.6667E+02     0.0000E+00     0.1667E+03     0.0
        84     0.0     0.1000E+03     0.0000E+00     0.1667E+03     0.0
        85     0.0     0.0000E+00     0.3333E+02     0.1667E+03     0.0
        86     0.0     0.3333E+02     0.3333E+02     0.1667E+03     0.0
        87     0.0     0.6667E+02     0.3333E+02     0.1667E+03     0.0
        88     0.0     0.1000E+03     0.3333E+02     0.1667E+03     0.0
        89     0.0     0.0000E+00     0.6667E+02     0.1667E+03     0.0
        90     0.0     0.3333E+02     0.6667E+02     0.1667E+03     0.0
        91     0.0     0.6667E+02     0.6667E+02     0.1667E+03     0.0
        92     0.0     0.1000E+03     0.6667E+02     0.1667E+03     0.0
        93     0.0     0.0000E+00     0.1000E+03     0.1667E+03     0.0
        94     0.0     0.3333E+02     0.1000E+03     0.1667E+03     0.0
        95     0.0     0.6667E+02     0.1000E+03     0.1667E+03     0.0
        96     0.0     0.1000E+03     0.1000E+03     0.1667E+03     0.0
        97     0.0     0.0000E+00     0.0000E+00     0.2000E+03     0.0
        98     0.0     0.3333E+02     0.0000E+00     0.2000E+03     0.0
        99     0.0     0.6667E+02     0.0000E+00     0.2000E+03     0.0
       100     0.0     0.1000E+03     0.0000E+00     0.2000E+03     0.0
       101     0.0     0.0000E+00     0.3333E+02     0.2000E+03     0.0
       102     0.0     0.3333E+02     0.3333E+02     0.2000E+03     0.0
       103     0.0     0.6667E+02     0.3333E+02     0.2000E+03     0.0
       104     0.0     0.1000E+03     0.3333E+02     0.2000E+03     0.0
       105     0.0     0.0000E+00     0.6667E+02     0.2000E+03     0.0
       106     0.0     0.3333E+02     0.6667E+02     0.2000E+03     0.0
       107     0.0     0.6667E+02     0.6667E+02     0.2000E+03     0.0
       108     0.0     0.1000E+03     0.6667E+02     0.2000E+03     0.0
       109     0.0     0.0000E+00     0.1000E+03     0.2000E+03     0.0
       110     0.0     0.3333E+02     0.1000E+03     0.2000E+03     0.0
       111     0.0     0.6667E+02     0.1000E+03     0.2000E+03     0.0
       112     0.0     0.1000E+03     0.1000E+03     0.2000E+03     0.0
       113     0.0     0.0000E+00     0.0000E+00     0.2333E+03     0.0
       114     0.0     0.3333E+02     0.0000E+00     0.2333E+03     0.0
       115     0.0     0.6667E+02     0.0000E+00     0.2333E+03     0.0
       116     0.0     0.1000E+03     0.0000E+00     0.2333E+03     0.0
       117     0.0     0.0000E+00     0.3333E+02     0.2333E+03     0.0
       118     0.0     0.3333E+02     0.3333E+02     0.2333E+03     0.0
       119     0.0     0.6667E+02     0.3333E+02     0.2333E+03     0.0
       120     0.0     0.1000E+03     0.3333E+02     0.2333E+03     0.0
       121     0.0     0.0000E+00     0.6667E+02     0.2333E+03     0.0
       122     0.0     0.3333E+02     0.6667E+02     0.2333E+03     0.0
       123     0.0     0.6667E+02     0.6667E+02     0.2333E+03     0.0
       124     0.0     0.1000E+03     0.6667E+02     0.2333E+03     0.0
       125     0.0     0.0000E+00     0.1000E+03     0.2333E+03     0.0
       126     0.0     0.3333E+02     0.1000E+03     0.2333E+03     0.0
       127     0.0     0.6667E+02     0.1000E+03     0.2333E+03     0.0
       128     0.0     0.1000E+03     0.1000E+03     0.2333E+03     0.0
       129     0.0     0.0000E+00     0.0000E+00     0.2667E+03     0.0
       130     0.0     0.3333E+02     0.0000E+00     0.2667E+03     0.0
       131     0.0     0.6667E+02     0.0000E+00     0.2667E+03     0.0
       132     0.0     0.1000E+03     0.0000E+00     0.2667E+03     0.0
       133     0.0     0.0000E+00     0.3333E+02     0.2667E+03     0.0
       134     0.0     0.3333E+02     0.3333E+02     0.2667E+03     0.0
       135     0.0     0.6667E+02     0.3333E+02     0.2667E+03     0.0
       136     0.0     0.1000E+03     0.3333E+02     0.2667E+03     0.0
       137     0.0     0.0000E+00     0.6667E+02     0.2667E+03     0.0
       138     0.0     0.3333E+02     0.6667E+02     0.2667E+03     0.0
       139     0.0     0.6667E+02     0.6667E+02     0.2667E+03     0.0
       140     0.0     0.1000E+03     0.6667E+02     0.2667E+03     0.0
       141     0.0     0.0000E+00     0.1000E+03     0.2667E+03     0.0
       142     0.0     0.3333E+02     0.1000E+03     0.2667E+03     0.0
       143     0.0     0.6667E+02     0.1000E+03     0.2667E+03     0.0
       144     0.0     0.1000E+03     0.1000E+03     0.2667E+03     0.0
       145     0.0     0.0000E+00     0.0000E+00     0.3000E+03     0.0
       146     0.0     0.3333E+02     0.0000E+00     0.3000E+03     0.0
       147     0.0     0.6667E+02     0.0000E+00     0.3000E+03     0.0
       148     0.0     0.1000E+03     0.0000E+00     0.3000E+03     0.0
       149     0.0     0.0000E+00     0.3333E+02     0.3000E+03     0.0
       150     0.0     0.3333E+02     0.3333E+02     0.3000E+03     0.0
       151     0.0     0.6667E+02     0.3333E+02     0.3000E+03     0.0
       152     0.0     0.1000E+03     0.3333E+02     0.3000E+03     0.0
       153     0.0     0.0000E+00     0.6667E+02     0.3000E+03     0.0
       154     0.0     0.3333E+02     0.6667E+02     0.3000E+03     0.0
       155     0.0     0.6667E+02     0.6667E+02     0.3000E+03     0.0
       156     0.0     0.1000E+03     0.6667E+02     0.3000E+03     0.0
       157     0.0     0.0000E+00     0.1000E+03     0.3000E+03     0.0
       158     0.0     0.3333E+02     0.1000E+03     0.3000E+03     0.0
       159     0.0     0.6667E+02     0.1000E+03     0.3000E+03     0.0
       160     0.0     0.1000E+03     0.1000E+03     0.3000E+03     0.0


 s o l i d   e l e m e n t s
     elem id     part id       node1       node2       node3       node4
                               node5       node6       node7       node8
           1           1           1           2           6           5
                                  17          18          22          21

           2           1           2           3           7           6
                                  18          19          23          22

           3           1           3           4           8           7
                                  19          20          24          23

           4           1           5           6          10           9
                                  21          22          26          25

           5           1           6           7          11          10
                                  22          23          27          26

           6           1           7           8          12          11
                                  23          24          28          27

           7           1           9          10          14          13
                                  25          26          30          29

           8           1          10          11          15          14
                                  26          27          31          30

           9           1          11          12          16          15
                                  27          28          32          31

          10           1          17          18          22          21
                                  33          34          38          37

          11           1          18          19          23          22
                                  34          35          39          38

          12           1          19          20          24          23
                                  35          36          40          39

          13           1          21          22          26          25
                                  37          38          42          41

          14           1          22          23          27          26
                                  38          39          43          42

          15           1          23          24          28          27
                                  39          40          44          43

          16           1          25          26          30          29
                                  41          42          46          45

          17           1          26          27          31          30
                                  42          43          47          46

          18           1          27          28          32          31
                                  43          44          48          47

          19           1          33          34          38          37
                                  49          50          54          53

          20           1          34          35          39          38
                                  50          51          55          54

          21           1          35          36          40          39
                                  51          52          56          55

          22           1          37          38          42          41
                                  53          54          58          57

          23           1          38          39          43          42
                                  54          55          59          58

          24           1          39          40          44          43
                                  55          56          60          59

          25           1          41          42          46          45
                                  57          58          62          61

          26           1          42          43          47          46
                                  58          59          63          62

          27           1          43          44          48          47
                                  59          60          64          63

          28           1          49          50          54          53
                                  65          66          70          69

          29           1          50          51          55          54
                                  66          67          71          70

          30           1          51          52          56          55
                                  67          68          72          71

          31           1          53          54          58          57
                                  69          70          74          73

          32           1          54          55          59          58
                                  70          71          75          74

          33           1          55          56          60          59
                                  71          72          76          75

          34           1          57          58          62          61
                                  73          74          78          77

          35           1          58          59          63          62
                                  74          75          79          78

          36           1          59          60          64          63
                                  75          76          80          79

          37           1          65          66          70          69
                                  81          82          86          85

          38           1          66          67          71          70
                                  82          83          87          86

          39           1          67          68          72          71
                                  83          84          88          87

          40           1          69          70          74          73
                                  85          86          90          89

          41           1          70          71          75          74
                                  86          87          91          90

          42           1          71          72          76          75
                                  87          88          92          91

          43           1          73          74          78          77
                                  89          90          94          93

          44           1          74          75          79          78
                                  90          91          95          94

          45           1          75          76          80          79
                                  91          92          96          95

          46           1          81          82          86          85
                                  97          98         102         101

          47           1          82          83          87          86
                                  98          99         103         102

          48           1          83          84          88          87
                                  99         100         104         103

          49           1          85          86          90          89
                                 101         102         106         105

          50           1          86          87          91          90
                                 102         103         107         106

          51           1          87          88          92          91
                                 103         104         108         107

          52           1          89          90          94          93
                                 105         106         110         109

          53           1          90          91          95          94
                                 106         107         111         110

          54           1          91          92          96          95
                                 107         108         112         111

          55           1          97          98         102         101
                                 113         114         118         117

          56           1          98          99         103         102
                                 114         115         119         118

          57           1          99         100         104         103
                                 115         116         120         119

          58           1         101         102         106         105
                                 117         118         122         121

          59           1         102         103         107         106
                                 118         119         123         122

          60           1         103         104         108         107
                                 119         120         124         123

          61           1         105         106         110         109
                                 121         122         126         125

          62           1         106         107         111         110
                                 122         123         127         126

          63           1         107         108         112         111
                                 123         124         128         127

          64           1         113         114         118         117
                                 129         130         134         133

          65           1         114         115         119         118
                                 130         131         135         134

          66           1         115         116         120         119
                                 131         132         136         135

          67           1         117         118         122         121
                                 133         134         138         137

          68           1         118         119         123         122
                                 134         135         139         138

          69           1         119         120         124         123
                                 135         136         140         139

          70           1         121         122         126         125
                                 137         138         142         141

          71           1         122         123         127         126
                                 138         139         143         142

          72           1         123         124         128         127
                                 139         140         144         143

          73           1         129         130         134         133
                                 145         146         150         149

          74           1         130         131         135         134
                                 146         147         151         150

          75           1         131         132         136         135
                                 147         148         152         151

          76           1         133         134         138         137
                                 149         150         154         153

          77           1         134         135         139         138
                                 150         151         155         154

          78           1         135         136         140         139
                                 151         152         156         155

          79           1         137         138         142         141
                                 153         154         158         157

          80           1         138         139         143         142
                                 154         155         159         158

          81           1         139         140         144         143
                                 155         156         160         159

$ nodspc=   16


 n o d a l   s p c s
                            boundary conditions (on=1)
        node      spc id     x  y  z rx ry rz   spc setid       birth       death
           1           0     1  1  1  1  1  1           0  0.0000E+00  1.0000E+20
           2           0     1  1  1  1  1  1           0  0.0000E+00  1.0000E+20
           3           0     1  1  1  1  1  1           0  0.0000E+00  1.0000E+20
           4           0     1  1  1  1  1  1           0  0.0000E+00  1.0000E+20
           5           0     1  1  1  1  1  1           0  0.0000E+00  1.0000E+20
           6           0     1  1  1  1  1  1           0  0.0000E+00  1.0000E+20
           7           0     1  1  1  1  1  1           0  0.0000E+00  1.0000E+20
           8           0     1  1  1  1  1  1           0  0.0000E+00  1.0000E+20
           9           0     1  1  1  1  1  1           0  0.0000E+00  1.0000E+20
          10           0     1  1  1  1  1  1           0  0.0000E+00  1.0000E+20
          11           0     1  1  1  1  1  1           0  0.0000E+00  1.0000E+20
          12           0     1  1  1  1  1  1           0  0.0000E+00  1.0000E+20
          13           0     1  1  1  1  1  1           0  0.0000E+00  1.0000E+20
          14           0     1  1  1  1  1  1           0  0.0000E+00  1.0000E+20
          15           0     1  1  1  1  1  1           0  0.0000E+00  1.0000E+20
          16           0     1  1  1  1  1  1           0  0.0000E+00  1.0000E+20



 l o a d   c u r v e s  

     number of load curves  =           1

     load function id number= 1
     title                  =                                                                                 
     number of time points  = 2
     discretization inc.    = 100
     initialization flag    = 0
        eq. 0 analysis only
        eq. 1 initialization only
        eq. 2 both

     input format           =    2e20.0
     abscissa scale factor  =    0.1000E+01
     ordinate scale factor  =    0.1000E+01
     abscissa offset value  =    0.0000E+00
     ordinate offset value  =    0.0000E+00
     table definition       = 0
        eq.-3 5d table           
        eq.-2 4d table           
        eq.-1 3d table           
        eq. 0 curve              
        eq. 1 table              
        eq. 2 general X-Y data   
        eq. 3 function           
        eq. 4 3858  interpolation
        eq. 5 4534a interpolation
        eq. 6 general R-S data   
        eq. 7 non-discretized curve

      abscissa     ordinate
     0.0000       1.0000000E+00
    1.00000E+99   1.0000000E+00



 v e l. / a c c. / d i s p.   b. c.   i n p u t  

      accl/displc flag=0  [velocity]           
      accl/displc flag=1  [acceleration]       
      accl/displc flag=2  [displacement]       
      accl/displc flag=3  [rb vel. vs. disp]   
      accl/displc flag=4  [rb relative disp]   

 node or part id of rigid body

                   loadc  dir       scale          vx          vy          vz
                 145                   1   -4.  1.0000E+00  0.0000E+00  0.0000E+00  1.0000E+00
             accl/displc flag= 0
             birth time      =   0.000E+00
             death time      =   1.000E+28
             local axis (rb) = 0
                 146                   1   -4.  1.0000E+00  0.0000E+00  0.0000E+00  1.0000E+00
             accl/displc flag= 0
             birth time      =   0.000E+00
             death time      =   1.000E+28
             local axis (rb) = 0
                 147                   1   -4.  1.0000E+00  0.0000E+00  0.0000E+00  1.0000E+00
             accl/displc flag= 0
             birth time      =   0.000E+00
             death time      =   1.000E+28
             local axis (rb) = 0
                 148                   1   -4.  1.0000E+00  0.0000E+00  0.0000E+00  1.0000E+00
             accl/displc flag= 0
             birth time      =   0.000E+00
             death time      =   1.000E+28
             local axis (rb) = 0
                 149                   1   -4.  1.0000E+00  0.0000E+00  0.0000E+00  1.0000E+00
             accl/displc flag= 0
             birth time      =   0.000E+00
             death time      =   1.000E+28
             local axis (rb) = 0
                 150                   1   -4.  1.0000E+00  0.0000E+00  0.0000E+00  1.0000E+00
             accl/displc flag= 0
             birth time      =   0.000E+00
             death time      =   1.000E+28
             local axis (rb) = 0
                 151                   1   -4.  1.0000E+00  0.0000E+00  0.0000E+00  1.0000E+00
             accl/displc flag= 0
             birth time      =   0.000E+00
             death time      =   1.000E+28
             local axis (rb) = 0
                 152                   1   -4.  1.0000E+00  0.0000E+00  0.0000E+00  1.0000E+00
             accl/displc flag= 0
             birth time      =   0.000E+00
             death time      =   1.000E+28
             local axis (rb) = 0
                 153                   1   -4.  1.0000E+00  0.0000E+00  0.0000E+00  1.0000E+00
             accl/displc flag= 0
             birth time      =   0.000E+00
             death time      =   1.000E+28
             local axis (rb) = 0
                 154                   1   -4.  1.0000E+00  0.0000E+00  0.0000E+00  1.0000E+00
             accl/displc flag= 0
             birth time      =   0.000E+00
             death time      =   1.000E+28
             local axis (rb) = 0
                 155                   1   -4.  1.0000E+00  0.0000E+00  0.0000E+00  1.0000E+00
             accl/displc flag= 0
             birth time      =   0.000E+00
             death time      =   1.000E+28
             local axis (rb) = 0
                 156                   1   -4.  1.0000E+00  0.0000E+00  0.0000E+00  1.0000E+00
             accl/displc flag= 0
             birth time      =   0.000E+00
             death time      =   1.000E+28
             local axis (rb) = 0
                 157                   1   -4.  1.0000E+00  0.0000E+00  0.0000E+00  1.0000E+00
             accl/displc flag= 0
             birth time      =   0.000E+00
             death time      =   1.000E+28
             local axis (rb) = 0
                 158                   1   -4.  1.0000E+00  0.0000E+00  0.0000E+00  1.0000E+00
             accl/displc flag= 0
             birth time      =   0.000E+00
             death time      =   1.000E+28
             local axis (rb) = 0
                 159                   1   -4.  1.0000E+00  0.0000E+00  0.0000E+00  1.0000E+00
             accl/displc flag= 0
             birth time      =   0.000E+00
             death time      =   1.000E+28
             local axis (rb) = 0
                 160                   1   -4.  1.0000E+00  0.0000E+00  0.0000E+00  1.0000E+00
             accl/displc flag= 0
             birth time      =   0.000E+00
             death time      =   1.000E+28
             local axis (rb) = 0

 ************************************************************
 Load curve usage 

 load curve # 1
 *BOUNDARY_PRESCRIBED_MOTION_... node velocity


 t i e d   n o d a l   p a i r s   f o r   l i n k i n g


 ************************************************************


  m a s s   p r o p e r t i e s   o f   p a r t # 1
     total mass of part          = 0.30000000E+10
     x-coordinate of mass center = 0.50000000E+02
     y-coordinate of mass center = 0.50000000E+02
     z-coordinate of mass center = 0.15000000E+03

     inertia tensor of material
     row1=     0.2611E+14    -0.2441E-01    -0.8203E-01
     row2=    -0.2441E-01     0.2611E+14    -0.8984E-01
     row3=    -0.8203E-01    -0.8984E-01     0.6111E+13

     principal inertias 
     i11 =    0.2611E+14
     i22 =    0.2611E+14
     i33 =    0.6111E+13

     principal directions
     row1=     0.7071E+00     0.7071E+00     0.4102E-14
     row2=    -0.7071E+00     0.7071E+00     0.4492E-14
     row3=     0.2762E-15    -0.6077E-14     0.1000E+01

 ************************************************************


  m a s s   p r o p e r t i e s   o f   b o d y
     total mass of body          = 0.30000000E+10
     x-coordinate of mass center = 0.50000000E+02
     y-coordinate of mass center = 0.50000000E+02
     z-coordinate of mass center = 0.15000000E+03

     inertia tensor of body
     row1=     0.2611E+14    -0.2441E-01    -0.8203E-01
     row2=    -0.2441E-01     0.2611E+14    -0.8984E-01
     row3=    -0.8203E-01    -0.8984E-01     0.6111E+13

     principal inertias of body
     i11 =    0.2611E+14
     i22 =    0.2611E+14
     i33 =    0.6111E+13

     principal directions
     row1=     0.7071E+00     0.7071E+00     0.4102E-14
     row2=    -0.7071E+00     0.7071E+00     0.4492E-14
     row3=     0.2762E-15    -0.6077E-14     0.1000E+01

 ************************************************************


 ************************************************************

 NOTE : For 2D axisymmetric problems the following
        masses are reported per radian.
        For 2D plain strain/stress problems the
        masses are reported per unit thickness.

 summary of mass 
 part id   =        1   mass= 0.30000000E+10

 t o t a l  m a s s          = 0.30000000E+10
 x-coordinate of mass center = 0.50000000E+02
 y-coordinate of mass center = 0.50000000E+02
 z-coordinate of mass center = 0.15000000E+03



 ************************************************************


 ************************************************************


 S t o r a g e   a l l o c a t i o n   

 Memory required to begin solution      :     225K
 Linear Alg dynamically allocated memory:     1895
 Additional dynamically allocated memory:    2057K
                                   Total:    2284K

  81 smallest timesteps
 ------------------------------------------------
 element       number                part    timestep
 solid             81                   1  2.3235E-02
 solid             80                   1  2.3235E-02
 solid             79                   1  2.3235E-02
 solid             63                   1  2.3235E-02
 solid             62                   1  2.3235E-02
 solid             61                   1  2.3235E-02
 solid             54                   1  2.3235E-02
 solid             53                   1  2.3235E-02
 solid             52                   1  2.3235E-02
 solid             36                   1  2.3235E-02
 solid             35                   1  2.3235E-02
 solid             34                   1  2.3235E-02
 solid             78                   1  2.3235E-02
 solid             75                   1  2.3235E-02
 solid             60                   1  2.3235E-02
 solid             57                   1  2.3235E-02
 solid             51                   1  2.3235E-02
 solid             48                   1  2.3235E-02
 solid             33                   1  2.3235E-02
 solid             30                   1  2.3235E-02
 solid             77                   1  2.3235E-02
 solid             76                   1  2.3235E-02
 solid             74                   1  2.3235E-02
 solid             73                   1  2.3235E-02
 solid             59                   1  2.3235E-02
 solid             58                   1  2.3235E-02
 solid             56                   1  2.3235E-02
 solid             55                   1  2.3235E-02
 solid             50                   1  2.3235E-02
 solid             49                   1  2.3235E-02
 solid             47                   1  2.3235E-02
 solid             46                   1  2.3235E-02
 solid             32                   1  2.3235E-02
 solid             31                   1  2.3235E-02
 solid             29                   1  2.3235E-02
 solid             28                   1  2.3235E-02
 solid             26                   1  2.3235E-02
 solid             25                   1  2.3235E-02
 solid             24                   1  2.3235E-02
 solid             23                   1  2.3235E-02
 solid             22                   1  2.3235E-02
 solid             21                   1  2.3235E-02
 solid             20                   1  2.3235E-02
 solid             19                   1  2.3235E-02
 solid             18                   1  2.3235E-02
 solid             17                   1  2.3235E-02
 solid             16                   1  2.3235E-02
 solid              9                   1  2.3235E-02
 solid              8                   1  2.3235E-02
 solid              7                   1  2.3235E-02
 solid             71                   1  2.3235E-02
 solid             70                   1  2.3235E-02
 solid             69                   1  2.3235E-02
 solid             68                   1  2.3235E-02
 solid             67                   1  2.3235E-02
 solid             66                   1  2.3235E-02
 solid             65                   1  2.3235E-02
 solid             64                   1  2.3235E-02
 solid             44                   1  2.3235E-02
 solid             43                   1  2.3235E-02
 solid             42                   1  2.3235E-02
 solid             41                   1  2.3235E-02
 solid             40                   1  2.3235E-02
 solid             39                   1  2.3235E-02
 solid             38                   1  2.3235E-02
 solid             37                   1  2.3235E-02
 solid             15                   1  2.3235E-02
 solid             14                   1  2.3235E-02
 solid             13                   1  2.3235E-02
 solid             12                   1  2.3235E-02
 solid             11                   1  2.3235E-02
 solid             10                   1  2.3235E-02
 solid              6                   1  2.3235E-02
 solid              5                   1  2.3235E-02
 solid              4                   1  2.3235E-02
 solid              3                   1  2.3235E-02
 solid              2                   1  2.3235E-02
 solid              1                   1  2.3235E-02
 solid             27                   1  2.3235E-02
 solid             72                   1  2.3235E-02
 solid             45                   1  2.3235E-02
       1 t 0.0000E+00 dt 5.00E-01 flush i/o buffers            04/13/26 10:54:43
       1 t 0.0000E+00 dt 5.00E-01 write d3plot file            04/13/26 10:54:43

 BEGIN implicit statics  step      1 t= 5.0000E-01             04/13/26 10:54:43
 ============================================================
                time =  5.00000E-01
   current step size =  5.00000E-01


     ================================================
     ==            IMPLICIT USAGE ALERT            ==
     ================================================
     == Memory Management for Implicit has changed ==
     == after R10.  Please use:                    ==
     ==       memory=     1M                       ==
     ================================================

 Iteration:   1     *|du|/|u| =  1.0000000E+00     *Ei/E0 =  1.0000000E+00
 Iteration:   2     *|du|/|u| =  3.1542463E-04     *Ei/E0 =  2.0513867E-07

 Equilibrium iterations summary step      1 t= 5.0000E-01      04/13/26 10:54:43
    Number of iterations to converge         =           2
    Number of stiffness reformations         =           0
    Number of right hand side evaluations    =           3

 Convergence detected as a combination of
     1. Current  maximum   displacement translational norm           
        Value =   1.4210E-04 vs Tolerance =   3.3166E-03
     2. Ratio of euclidian displacement translational norms          
        Value =   3.1542E-04 vs Tolerance =   1.0000E-03
     3. Ratio of euclidian energy       translational norms          
        Value =   2.0514E-07 vs Tolerance =   1.0000E-02
       6 t 5.0000E-01 dt 5.00E-01 write d3plot file            04/13/26 10:54:43

 BEGIN implicit statics  step      2 t= 1.2924E+00             04/13/26 10:54:43
 ============================================================
                time =  1.29245E+00
   current step size =  7.92447E-01
 Iteration:   1     *|du|/|u| =  6.1316093E-01     *Ei/E0 =  1.0000000E+00
 Iteration:   2     *|du|/|u| =  4.0504710E-04     *Ei/E0 =  5.1360578E-07

 Equilibrium iterations summary step      2 t= 1.2924E+00      04/13/26 10:54:43
    Number of iterations to converge         =           2
    Number of stiffness reformations         =           0
    Number of right hand side evaluations    =           3

 Convergence detected as a combination of
     1. Current  maximum   displacement translational norm           
        Value =   4.7341E-04 vs Tolerance =   3.3166E-03
     2. Ratio of euclidian displacement translational norms          
        Value =   4.0505E-04 vs Tolerance =   1.0000E-03
     3. Ratio of euclidian energy       translational norms          
        Value =   5.1361E-07 vs Tolerance =   1.0000E-02
      10 t 1.2924E+00 dt 7.92E-01 write d3plot file            04/13/26 10:54:43

 BEGIN implicit statics  step      3 t= 2.5484E+00             04/13/26 10:54:43
 ============================================================
                time =  2.54839E+00
   current step size =  1.25594E+00
 Iteration:   1     *|du|/|u| =  4.9288447E-01     *Ei/E0 =  1.0000000E+00
 Iteration:   2     *|du|/|u| =  7.5644875E-04     *Ei/E0 =  1.2838819E-06

 Equilibrium iterations summary step      3 t= 2.5484E+00      04/13/26 10:54:43
    Number of iterations to converge         =           2
    Number of stiffness reformations         =           0
    Number of right hand side evaluations    =           3

 Convergence detected as a combination of
     1. Current  maximum   displacement translational norm           
        Value =   1.6751E-03 vs Tolerance =   3.3166E-03
     2. Ratio of euclidian displacement translational norms          
        Value =   7.5645E-04 vs Tolerance =   1.0000E-03
     3. Ratio of euclidian energy       translational norms          
        Value =   1.2839E-06 vs Tolerance =   1.0000E-02
      14 t 2.5484E+00 dt 1.26E+00 write d3plot file            04/13/26 10:54:43

 BEGIN implicit statics  step      4 t= 4.5389E+00             04/13/26 10:54:43
 ============================================================
                time =  4.53893E+00
   current step size =  1.99054E+00
 Iteration:   1     *|du|/|u| =  4.3865441E-01     *Ei/E0 =  1.0000000E+00
 Iteration:   2     *|du|/|u| =  1.6660885E-03     *Ei/E0 =  3.2053498E-06
 Iteration:   3     *|du|/|u| =  1.8343582E-03     *Ei/E0 =  1.7738265E-08
 Iteration:   4     *|du|/|u| =  1.7639880E-04     *Ei/E0 =  1.1320394E-09

 Equilibrium iterations summary step      4 t= 4.5389E+00      04/13/26 10:54:43
    Number of iterations to converge         =           4
    Number of stiffness reformations         =           0
    Number of right hand side evaluations    =           5

 Convergence detected as a combination of
     1. Current  maximum   displacement translational norm           
        Value =   7.9409E-04 vs Tolerance =   3.3166E-03
     2. Ratio of euclidian displacement translational norms          
        Value =   1.7640E-04 vs Tolerance =   1.0000E-03
     3. Ratio of euclidian energy       translational norms          
        Value =   1.1320E-09 vs Tolerance =   1.0000E-02
      20 t 4.5389E+00 dt 1.99E+00 write d3plot file            04/13/26 10:54:43

 BEGIN implicit statics  step      5 t= 7.6937E+00             04/13/26 10:54:43
 ============================================================
                time =  7.69371E+00
   current step size =  3.15479E+00
 Iteration:   1     *|du|/|u| =  4.1002579E-01     *Ei/E0 =  1.0000000E+00
 Iteration:   2     *|du|/|u| =  3.7960298E-03     *Ei/E0 =  7.9534077E-06
 Iteration:   3     *|du|/|u| =  4.4355440E-03     *Ei/E0 =  1.2834649E-07
 Iteration:   4     *|du|/|u| =  9.0355357E-04     *Ei/E0 =  2.0480837E-08

 Equilibrium iterations summary step      5 t= 7.6937E+00      04/13/26 10:54:43
    Number of iterations to converge         =           4
    Number of stiffness reformations         =           0
    Number of right hand side evaluations    =           5

 Convergence detected as a combination of
     1. Ratio of euclidian displacement translational norms          
        Value =   9.0355E-04 vs Tolerance =   1.0000E-03
     2. Ratio of euclidian energy       translational norms          
        Value =   2.0481E-08 vs Tolerance =   1.0000E-02
      26 t 7.6937E+00 dt 3.15E+00 write d3plot file            04/13/26 10:54:43

 BEGIN implicit statics  step      6 t= 1.2694E+01             04/13/26 10:54:43
 ============================================================
                time =  1.26937E+01
   current step size =  5.00000E+00
 Iteration:   1     *|du|/|u| =  3.9388485E-01     *Ei/E0 =  1.0000000E+00
 Iteration:   2     *|du|/|u| =  9.0970725E-03     *Ei/E0 =  1.9794087E-05
 Iteration:   3     *|du|/|u| =  1.1934066E-02     *Ei/E0 =  1.1122349E-06
 Iteration:   4     *|du|/|u| =  4.3800947E-03     *Ei/E0 =  4.4607471E-07
 Iteration:   5     *|du|/|u| =  1.2609860E-03     *Ei/E0 =  2.8261996E-08
 Iteration:   6     *|du|/|u| =  6.2426619E-04     *Ei/E0 =  6.3595334E-09

 Equilibrium iterations summary step      6 t= 1.2694E+01      04/13/26 10:54:43
    Number of iterations to converge         =           6
    Number of stiffness reformations         =           0
    Number of right hand side evaluations    =           7

 Convergence detected as a combination of
     1. Ratio of euclidian displacement translational norms          
        Value =   6.2427E-04 vs Tolerance =   1.0000E-03
     2. Ratio of euclidian energy       translational norms          
        Value =   6.3595E-09 vs Tolerance =   1.0000E-02
      34 t 1.2694E+01 dt 5.00E+00 write d3plot file            04/13/26 10:54:43

 BEGIN implicit statics  step      7 t= 1.7694E+01             04/13/26 10:54:43
 ============================================================
                time =  1.76937E+01
   current step size =  5.00000E+00
 Iteration:   1     *|du|/|u| =  2.8260334E-01     *Ei/E0 =  9.7924212E-01
 Iteration:   2     *|du|/|u| =  6.3159363E-03     *Ei/E0 =  1.8595326E-05
 Iteration:   3     *|du|/|u| =  8.2210121E-03     *Ei/E0 =  1.0055354E-06
 Iteration:   4     *|du|/|u| =  2.8896086E-03     *Ei/E0 =  3.7586182E-07
 Iteration:   5     *|du|/|u| =  8.9612733E-04     *Ei/E0 =  2.7066706E-08

 Equilibrium iterations summary step      7 t= 1.7694E+01      04/13/26 10:54:43
    Number of iterations to converge         =           5
    Number of stiffness reformations         =           0
    Number of right hand side evaluations    =           6

 Convergence detected as a combination of
     1. Ratio of euclidian displacement translational norms          
        Value =   8.9613E-04 vs Tolerance =   1.0000E-03
     2. Ratio of euclidian energy       translational norms          
        Value =   2.7067E-08 vs Tolerance =   1.0000E-02
      41 t 1.7694E+01 dt 5.00E+00 write d3plot file            04/13/26 10:54:43

 BEGIN implicit statics  step      8 t= 2.2694E+01             04/13/26 10:54:43
 ============================================================
                time =  2.26937E+01
   current step size =  5.00000E+00
 Iteration:   1     *|du|/|u| =  2.2034408E-01     *Ei/E0 =  9.5924847E-01
 Iteration:   2     *|du|/|u| =  4.7048510E-03     *Ei/E0 =  1.7518876E-05
 Iteration:   3     *|du|/|u| =  6.0479776E-03     *Ei/E0 =  9.1324584E-07
 Iteration:   4     *|du|/|u| =  2.0230234E-03     *Ei/E0 =  3.2057459E-07
 Iteration:   5     *|du|/|u| =  6.9717152E-04     *Ei/E0 =  2.6192557E-08

 Equilibrium iterations summary step      8 t= 2.2694E+01      04/13/26 10:54:43
    Number of iterations to converge         =           5
    Number of stiffness reformations         =           0
    Number of right hand side evaluations    =           6

 Convergence detected as a combination of
     1. Ratio of euclidian displacement translational norms          
        Value =   6.9717E-04 vs Tolerance =   1.0000E-03
     2. Ratio of euclidian energy       translational norms          
        Value =   2.6193E-08 vs Tolerance =   1.0000E-02
      48 t 2.2694E+01 dt 5.00E+00 write d3plot file            04/13/26 10:54:43

 BEGIN implicit statics  step      9 t= 2.7694E+01             04/13/26 10:54:43
 ============================================================
                time =  2.76937E+01
   current step size =  5.00000E+00
 Iteration:   1     *|du|/|u| =  1.8056203E-01     *Ei/E0 =  9.4020533E-01
 Iteration:   2     *|du|/|u| =  3.7143787E-03     *Ei/E0 =  1.6459803E-05
 Iteration:   3     *|du|/|u| =  4.7531199E-03     *Ei/E0 =  8.2289934E-07
 Iteration:   4     *|du|/|u| =  1.5128175E-03     *Ei/E0 =  2.6664751E-07
 Iteration:   5     *|du|/|u| =  5.6902019E-04     *Ei/E0 =  2.4902713E-08

 Equilibrium iterations summary step      9 t= 2.7694E+01      04/13/26 10:54:43
    Number of iterations to converge         =           5
    Number of stiffness reformations         =           0
    Number of right hand side evaluations    =           6

 Convergence detected as a combination of
     1. Ratio of euclidian displacement translational norms          
        Value =   5.6902E-04 vs Tolerance =   1.0000E-03
     2. Ratio of euclidian energy       translational norms          
        Value =   2.4903E-08 vs Tolerance =   1.0000E-02
      55 t 2.7694E+01 dt 5.00E+00 write d3plot file            04/13/26 10:54:43

 BEGIN implicit statics  step     10 t= 3.0000E+01             04/13/26 10:54:43
 ============================================================
                time =  3.00000E+01
   current step size =  2.30629E+00
 Iteration:   1     *|du|/|u| =  7.6917547E-02     *Ei/E0 =  1.9614269E-01
 Iteration:   2     *|du|/|u| =  2.8891791E-04     *Ei/E0 =  6.8942948E-07

 Equilibrium iterations summary step     10 t= 3.0000E+01      04/13/26 10:54:43
    Number of iterations to converge         =           2
    Number of stiffness reformations         =           0
    Number of right hand side evaluations    =           3

 Convergence detected as a combination of
     1. Ratio of euclidian displacement translational norms          
        Value =   2.8892E-04 vs Tolerance =   1.0000E-03
     2. Ratio of euclidian energy       translational norms          
        Value =   6.8943E-07 vs Tolerance =   1.0000E-02
      59 t 3.0000E+01 dt 2.31E+00 write d3plot file            04/13/26 10:54:43
 
 *** termination time reached ***
      59 t 3.0000E+01 dt 2.31E+00 write d3dump01 file          04/13/26 10:54:43

 N o r m a l    t e r m i n a t i o n                          04/13/26 10:54:43

 S t o r a g e   a l l o c a t i o n   

 Memory required to complete solution   :     225K
 Linear Alg dynamically allocated memory:      63K
 Additional dynamically allocated memory:    2378K
                                   Total:    2665K

 T i m i n g   i n f o r m a t i o n
                        CPU(seconds)   %CPU  Clock(seconds) %Clock
  ----------------------------------------------------------------
  Keyword Processing ... 0.0000E+00    0.00     1.1000E-02    0.96
    KW Reading ......... 0.0000E+00    0.00     1.0000E-03    0.09
    KW Writing ......... 0.0000E+00    0.00     5.0000E-03    0.44
  Initialization ....... 1.0000E+00  100.00     1.0300E+00   89.72
    Init Proc Phase 1 .. 0.0000E+00    0.00     1.0000E-02    0.87
  Element processing ... 0.0000E+00    0.00     2.2000E-02    1.92
    Solids ............. 0.0000E+00    0.00     1.9000E-02    1.66
    E Other ............ 0.0000E+00    0.00     3.0000E-03    0.26
  Binary databases ..... 0.0000E+00    0.00     1.0000E-03    0.09
  Implicit ............. 0.0000E+00    0.00     4.0000E-03    0.35
  Implicit Nonlinear ... 0.0000E+00    0.00     1.6000E-02    1.39
    Imp. NL force mod .. 0.0000E+00    0.00     9.0000E-03    0.78
  Implicit Lin. Alg. ... 0.0000E+00    0.00     5.4000E-02    4.70
    Imp. LA Mtx Assemb . 0.0000E+00    0.00     1.3000E-02    1.13
    Imp. LA Factor ..... 0.0000E+00    0.00     4.0000E-02    3.48
    Imp. LA Solve ...... 0.0000E+00    0.00     1.0000E-03    0.09
  Group force file ..... 0.0000E+00    0.00     4.0000E-03    0.35
  Misc. 3 .............. 0.0000E+00    0.00     5.0000E-03    0.44
  Misc. 4 .............. 0.0000E+00    0.00     1.0000E-03    0.09
    Timestep Init ...... 0.0000E+00    0.00     1.0000E-03    0.09
  ----------------------------------------------------------------
  T o t a l s            1.0000E+00  100.00     1.1480E+00  100.00

 Problem time       =    3.0000E+01
 Problem cycle      =        59
 Total CPU time     =         1 seconds (   0 hours  0 minutes  1 seconds)
 CPU time per zone cycle  =          0.000 picoseconds
 Clock time per zone cycle=   22389621.276 picoseconds

 Number of CPU's   31
 NLQ used/max     136/  136
 Start time   04/13/2026 10:54:43  
 End time     04/13/2026 10:54:43  
 Elapsed time       0 second  for      59 cycles using 31 SMP threads
             (      0 hour   0 minute   0 second )

 N o r m a l    t e r m i n a t i o n                          04/13/26 10:54:43
