      Date: 06/07/2017      Time: 10:01:33  

     ___________________________________________________
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     |  Livermore  Software  Technology  Corporation   |
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     |  7374 Las Positas Road                          |
     |  Livermore, CA 94551                            |
     |  Tel: (925) 449-2500  Fax: (925) 449-2507       |
     |  www.lstc.com                                   |
     |_________________________________________________|
     |                                                 |
     |  LS-DYNA, A Program for Nonlinear Dynamic       |
     |  Analysis of Structures in Three Dimensions     |
     |  Version : mpp d R7.1.3    Date: 05/19/2016     |
     |  Revision: 111795          Time: 09:01:13       |
     |                                                 |
     |  Features enabled in this version:              |
     |    Distributed Memory Parallel                  |
     |    CESE CHEMISTRY EM ICFD STOCHASTIC_PARTICLES  |
     |    FFTW (multi-dimensional FFTW Library)        |
     |    ANSYS License (ans140)                       |
     |                                                 |
     |  Licensed to: DYNAmore GmbH                     |
     |  Issued by  : dynamore_03032017                 |
     |                                                 |
     |  Platform   : Linux RHEL 5.4                    |
     |  OS Level   : Platform-MPI 8.1.1 Xeon64 uo      |
     |  Compiler   : Intel Fortran Compiler 13.1 SSE2  |
     |  Hostname   : littlefinger.stg.dynamore         |
     |  Precision  : Double precision (I8R8)           |
     |  SVN Version: 111795                            |
     |                                                 |
     |  Unauthorized use infringes LSTC copyrights     |
     |_________________________________________________|


 Input file: ex_01_thin_shell_elform_2.k                                             

 The native file format       : 64-bit small endian
 Binary file                  : 32 bit IEEE selected
 Memory option                : AUTO selected
 Memory size from default     :    20000000,     20000000

 Memory for the head node
 Memory installed (MB)        :        31938
 Memory free (MB)             :        14160
 Memory required (MB)         :          152

 ********  notice  ********  notice  ********  notice  ********
 *                                                            *
 * This is the LS-DYNA Finite Element code.                   *
 *                                                            *
 * Neither LSTC nor the authors assume any responsibility for *
 * the validity, accuracy, or applicability of any results    *
 * obtained from this system. The user must verify his own    *
 * results.                                                   *
 *                                                            *
 * LSTC 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 LSTC through your site focus.               *
 *                                                            *
 * Copyright (C) 1990-2015                                    *
 * by Livermore Software Technology Corp. (LSTC)              *
 * All rights reserved                                        *
 *                                                            *
 ********  notice  ********  notice  ********  notice  ********

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            L I S T   O F   K E Y W O R D   C O U N T S   

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total # of *HOURGLASS..............................       0
total # of *ICFD_BOUNDARY_CONJ_HEAT................       0
total # of *ICFD_BOUNDARY_FLUX_TEMP................       0
total # of *ICFD_BOUNDARY_FREESLIP.................       0
total # of *ICFD_BOUNDARY_FSI......................       0
total # of *ICFD_BOUNDARY_NONSLIP..................       0
total # of *ICFD_BOUNDARY_PRESCRIBED_MOVEMESH......       0
total # of *ICFD_BOUNDARY_PRESCRIBED_PRE...........       0
total # of *ICFD_BOUNDARY_PRESCRIBED_TEMP..........       0
total # of *ICFD_BOUNDARY_PRESCRIBED_VEL...........       0
total # of *ICFD_CONTROL_ADAPT.....................       0
total # of *ICFD_CONTROL_ADAPT_SIZE................       0
total # of *ICFD_CONTROL_FSI.......................       0
total # of *ICFD_CONTROL_LOAD......................       0
total # of *ICFD_CONTROL_MESH......................       0
total # of *ICFD_CONTROL_MESH_MOV..................       0
total # of *ICFD_CONTROL_OUTPUT....................       0
total # of *ICFD_CONTROL_PARTITION.................       0
total # of *ICFD_CONTROL_SPLIT.....................       0
total # of *ICFD_CONTROL_SURFMESH..................       0
total # of *ICFD_CONTROL_TIME......................       0
total # of *ICFD_CONTROL_TURBULENCE................       0
total # of *ICFD_CONTROL_TURB_SYNTHESIS............       0
total # of *ICFD_DATABASE_AVERAGE..................       0
total # of *ICFD_DATABASE_DRAG.....................       0
total # of *ICFD_DEFINE_POINT......................       0
total # of *ICFD_DEFINE_NONINERTIAL................       0
total # of *ICFD_INITIAL...........................       0
total # of *ICFD_MAT...............................       0
total # of *ICFD_PART..............................       0
total # of *ICFD_PART_VOL..........................       0
total # of *ICFD_SECTION...........................       0
total # of *ICFD_SET_NODE..........................       0
total # of *INITIAL_AIRBAG_PARTICLE_POSITION.......       0
total # of *INITIAL_AXIAL_FORCE_BEAM...............       0
total # of *INITIAL_DETONATION.....................       0
total # of *INITIAL_FIELD_SOLID....................       0
total # of *INITIAL_IMPULSE_MINE...................       0
total # of *INITIAL_MOMENTUM.......................       0
total # of *INITIAL_PWP_DEPTH .....................       0
total # of *INITIAL_STRAIN_SHELL...................       0
total # of *INITIAL_STRAIN_SHELL_SET...............       0
total # of *INITIAL_STRAIN_SOLID...................       0
total # of *INITIAL_STRAIN_TSHELL..................       0
total # of *INITIAL_STRESS_BEAM....................       0
total # of *INITIAL_STRESS_DEPTH ..................       0
total # of *INITIAL_STRESS_SECTION.................       0
total # of *INITIAL_STRESS_SHELL...................       0
total # of *INITIAL_STRESS_SHELL_SET...............       0
total # of *INITIAL_STRESS_SOLID...................       0
total # of *INITIAL_STRESS_SPH.....................       0
total # of *INITIAL_STRESS_TSHELL..................       0
total # of *INITIAL_TEMPERATURE_SET................       0
total # of *INITIAL_TEMPERATURE_NODE...............       0
total # of *INITIAL_VELOCITY.......................       0
total # of *INITIAL_VELOCITY_NODE..................       0
total # of *INITIAL_VELOCITY_RIGID_BODY............       0
total # of *INITIAL_VOID_PART......................       0
total # of *INITIAL_VOID_SET.......................       0
total # of *INITIAL_VOLUME_FRACTION_GEOMETRY.......       0
total # of *INITIAL_HYDROSTATIC_ALE................       0
total # of *INITIAL_EOS_ALE........................       0
total # of *INITIAL_ALE_MAPPING....................       0
total # of *INTEGRATION_BEAM.......................       0
total # of *INTEGRATION_SHELL......................       0
total # of *INTERFACE_COMPONENT_option.............       0
total # of *INTERFACE_DE_HBOND.....................       0
total # of *INTERFACE_LINKING_DISCRETE_NODE........       0
total # of *INTERFACE_LINKING_DISCRETE_NODE_SET....       0
total # of *INTERFACE_LINKING_EDGE.................       0
total # of *INTERFACE_LINKING_SEGMENT..............       0
total # of *INTERFACE_SPRINGBACK...................       0
total # of *INTERFACE_SSI_AUXILIARY_FREE_FIELD.....       0
total # of *INTERFACE_SSI_STATIC...................       0
total # of *INTERFACE_SSI..........................       0
total # of *LOAD_ALE_CONVECTION ...................       0
total # of *LOAD_AIR_PRESSURE......................       0
total # of *LOAD_BEAM..............................       0
total # of *LOAD_BEAM_SET..........................       0
total # of *LOAD_BODY_GENERALIZED..................       0
total # of *LOAD_BODY_POROUS......................       0
total # of *LOAD_BODY_RX...........................       0
total # of *LOAD_BODY_RY...........................       0
total # of *LOAD_BODY_RZ...........................       0
total # of *LOAD_BODY_X............................       0
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_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_CHEMICAL_REACTION ...........       0
total # of *LOAD_HEAT_CONTROLLER ..................       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_NODE..............................       0
total # of *LOAD_NODE_SET..........................       0
total # of *LOAD_NSG...............................       0
total # of *LOAD_REMOVE_PART ......................       0
total # of *LOAD_SEGMENT...........................      16
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_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_TIME_SEQUENCE......................       0
total # of *LSO_VARIABLE_GROUP.....................       0
total # of *MAT_option.............................       1
total # of *MAT_THERMAL_option.....................       0
total # of *MESH_BL................................       0
total # of *MESH_BL_SYM............................       0
total # of *MESH_EMBEDSHELL........................       0
total # of *MESH_INTERF............................       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 *MAT_NONLOCAL...........................       0
total # of *NODE...................................      25
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 *RIGIDWALL_option.......................       0
total # of *SECTION_option.........................       1
total # of *SET_2D_SEGMENT.........................       0
total # of *SET_BEAM...............................       0
total # of *SET_DISCRETE...........................       0
total # of *SET_MODE...............................       0
total # of *SET_NODE_option........................       0
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..................................       1
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 *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     :      265402 

********** echo of pfile data **********


*********** end of pfile data **********

 MPP execution with       1 procs

 LS-DYNA will perform a structural only analysis 



 Skew Plate with Normal Pressure (thin shell mesh)                       
            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 .......    0.0000E+00

    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
          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 ...............................       1
          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

    energy convergence tolerance ..................    0.1000E-01

    residual convergence tolerance ................    0.9990E+11

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

    absolute convergence tolerance ................    0.1000E+01

    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 ...................       2
          eq.0: no iteration info to screen             
          eq.1: print iteration info to screen, files   
          eq.2: extra iteration info to d3hsp and messag



    IMPLICIT CONTROL CARD 2a.  Solution

    convergence norms .............................       2
          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 ............................       1
          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 ........................      4
          eq. 5: sparse direct double - auto out-of-core 
          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 

    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/experimental unsymmetric   

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



    IMPLICIT CONTROL CARD 4.  Auto Time Step Control

    time step control method ......................       0
          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 ..............................       0

    minimum allowable step size ...................    0.0000E+00

    maximum allowable step size ...................    0.0000E+00
          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

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

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



    IMPLICIT CONTROL CARD 6.  Arc Length            

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

    direction controlling arc length method .......       1

    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


 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..................      25

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

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

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

    number of shell elements.......................      16

    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


    CONTROL CARD 2. Model Size-Boundary Conditions

    number of spc nodes............................       0

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

    number of velocity cards.......................       0

    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..................      16

    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 defintions.............       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


    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 ............       0
          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...............................    0.1000E+01

    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...    0.0000E+00

    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

    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 flag for solid and thick shells........       0
          eq.0:  no                                      
          eq.1:  yes                                     

    option part set ID for eroding solids..........       0
          eq.0:  all solids are checked if eros_flag=1   
          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



    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



    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     

    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                      
          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                      
          eq.  47: cohesive with shell offsets           
          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

    integration for shell through thickness .......       1
          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 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 .......    0.0000E+00

    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..........       2
          eq. 2:  2 point integration in plane          
          eq. 3:  3 point 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

    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

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


    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 

    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.-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


    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   

 
 *** Warning 30365 (INI+365)
     Implicit solver does not support LSTC_MEMORY=auto.
     The option is turned off
    thickness changes considered in type 4 contact.       0
          eq.0:  no                                      
          eq.1:  yes                                     

    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                                     
          eq.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  

    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...................    0.0000E+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             

    stiffness calculation for segment based contact       0
          eq.0:  use 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


    CONTROL CARD 16. Computation Options-Parallel

    number of cpus for parallel computations.......       1

    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                    

    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

    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.............    0.1000E-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.........       1
          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
    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


    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 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.    0.1000E+00

    output interval for interface force database...    0.1000E+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........       4

    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...       0
          eq.0:  exclude (default)                      
          eq.1:  include strains (solid and shells)     

    flag for including stress tensor in database...       1
          eq.1:  include (default)                      
          eq.2:  exclude                                

    flag for including effective plastic strain....       1
          eq.1:  include (default)                      
          eq.2:  exclude                                

    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..       0
    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..........       0
          eq.1:  off                                    
          eq.2:  on                                     

    output shell element dt, mass, added mass......       0
          eq.1:  off                                    
          eq.2:  output dt                              
          eq.3:  output mass                            

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

    filter parameter...............................    0.0000E+00

    flag for solid element additional output.......       0
          eq.1:  output 3 additional variables          
          eq.2:  output 5 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.........    0.0000E+00
    output interval for element print blocks.......    0.1000E+00
    output interval for global/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.......    0.0000E+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 ....    0.0000E+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



    CONTROL CARD 25. ALE 1st card

    Default continuum treatment....................       0
         eq.1: Lagrangian (default)
         eq.2: Eulerian
         eq.3: Arbitrary Lagrangian Eulerian
         eq.4: Eulerian Ambient

    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

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


    CONTROL CARD 26. ALE 2nd card

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

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

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

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

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

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

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

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

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

    Pressure equilibrium...........................       0
         eq.0: Off
         eq.1: On
    Number of parts considered in ALE convection...       0

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

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

    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


    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


    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 

    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



    CONTROL CARD 50. EFG 

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

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

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

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

    intfs..........................................       0



 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.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  rs strainrate sensitive concrete  
     eq.85  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 anisotropic 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.202 steel EC3                            
     eq.203 hysteretic reinforcement             
     eq.205 discrete beam surface contact        
     eq.206 Park Ang beam                        
     eq.208 bolt beam                            
     eq.213 awg composite damage                 
     eq.214 dry fabric                           
     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.228 tabulated johnson cook aniso         
     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.251 tailored properties                  
     eq.252 toughened adhesive polymer           
     eq.255 piecewise linear plastic thermal     
     eq.256 amorphous solids finite stain        
     eq.261 laminated fracture daimler pinho     
     eq.262 laminated fracture daimler camanho   
     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                                
 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.......................    4
     hourglass coefficient................. 1.00000E-01
     bulk viscosity type...................    1
     quadratic bulk viscosity coefficient.. 1.50000E+00
     linear bulk viscosity coefficient..... 6.00000E-02

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


 material type # 1  (Elastic)                                            

 part     id .....................            1
 section  id .....................            1
 material id .....................            1
 section  title .................. 
                                                                                 
 material title .................. 
                                                                                 
           material type ..............     1     
           equation-of-state type .....     0
           hourglass type .............     4
           bulk viscosity type ........     1

     density .......................... = 7.80000E+03
     hourglass coefficient (membrane).. = 1.00000E-01
     hourglass coefficient (rotation).. = 1.00000E-01
     hourglass coefficient (warping ).. = 1.00000E-01
     quadratic bulk viscosity ......... = 1.50000E+00
     linear bulk viscosity ............ = 6.00000E-02
     element type ..................... =    2
          eq.0: 4, 6, 8, 10-node solid element or SPH 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 

     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
     flag for adaptive remeshing ...... =    0
          eq.0: inactive                    
          eq.1: h-adaptive only             
          eq.2: r-adaptive only             
     rayleigh damping coefficient...... = 0.00000E+00
     e ................................ = 2.10000E+11
     vnu .............................. = 3.00000E-01

     for belytschko-schwer beam only     
     ga, axial damping factor ......... = 0.00000E+00
     gb, bending damping factor ....... = 0.00000E+00
     shear area factor ................ = 1.00000E+00
     thru-thickness integration points  = 5.00000E+00
     print out option ................. = 3.00000E+00
          eq.1.0:average resultants & fiber lengths       
          eq.2.0:resultants at plan points & fiber lengths
          eq.3.0:resultants,stresses all points & fiber lengths

     integration rule ................. = 0.00000E+00
          lt.0.0:absolute value is specified rule #  
          eq.0.0:gauss (trapezoidal if > 10 IP) 
          eq.1.0:trapezoidal rule          
     shell formulation ................ =    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             
         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 elem(5DOF) 
         eq.  22: linear shear panel element(3DOF) 
         eq.  23: 8-node quadratic quadrilateral   
         eq.  24: 6-node quadratic triangular      
         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                 
         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                 
         eq.  47: cohesive with shell offsets      
         eq.  55: 8-node 2D plane strain fracture  
         eq.  98: interpolation shell element      
         eq.  99: elastic vibration element        
         eq. 201: isogeometric nurbs element       
         ge.1000: user defined (generalized) shell 
     shell thickness:         node 1 .. = 1.00000E-02
                              node 2 .. = 1.00000E-02
                              node 3 .. = 1.00000E-02
                              node 4 .. = 1.00000E-02

     reference surface ................ = 0.00000E+00
          eq. 1.0:top                    
          eq. 0.0:middle                 
          eq.-1.0:bottom                 

     mass per unit area ............... = 0.00000E+00

     flag for discontinuous thickness    
     field for elements with thickness   
     stretch .......................... =    2
          eq. 0: default is 1                     
          eq. 1: thickness field is continuous    
          eq. 2: thickness field is discontinous  



 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     3.0     0.0000E+00     0.0000E+00     0.0000E+00     0.0
         2     3.0     0.2165E+00     0.1250E+00     0.0000E+00     0.0
         3     3.0     0.4330E+00     0.2500E+00     0.0000E+00     0.0
         4     3.0     0.6495E+00     0.3750E+00     0.0000E+00     0.0
         5     3.0     0.8660E+00     0.5000E+00     0.0000E+00     0.0
         6     3.0     0.2500E+00     0.0000E+00     0.0000E+00     0.0
         7     0.0     0.4665E+00     0.1250E+00     0.0000E+00     0.0
         8     0.0     0.6830E+00     0.2500E+00     0.0000E+00     0.0
         9     0.0     0.8995E+00     0.3750E+00     0.0000E+00     0.0
        10     3.0     0.1116E+01     0.5000E+00     0.0000E+00     0.0
        11     3.0     0.5000E+00     0.0000E+00     0.0000E+00     0.0
        12     0.0     0.7165E+00     0.1250E+00     0.0000E+00     0.0
        13     0.0     0.9330E+00     0.2500E+00     0.0000E+00     0.0
        14     0.0     0.1150E+01     0.3750E+00     0.0000E+00     0.0
        15     3.0     0.1366E+01     0.5000E+00     0.0000E+00     0.0
        16     3.0     0.7500E+00     0.0000E+00     0.0000E+00     0.0
        17     0.0     0.9665E+00     0.1250E+00     0.0000E+00     0.0
        18     0.0     0.1183E+01     0.2500E+00     0.0000E+00     0.0
        19     0.0     0.1400E+01     0.3750E+00     0.0000E+00     0.0
        20     3.0     0.1616E+01     0.5000E+00     0.0000E+00     0.0
        21     3.0     0.1000E+01     0.0000E+00     0.0000E+00     0.0
        22     3.0     0.1217E+01     0.1250E+00     0.0000E+00     0.0
        23     3.0     0.1433E+01     0.2500E+00     0.0000E+00     0.0
        24     3.0     0.1650E+01     0.3750E+00     0.0000E+00     0.0
        25     3.0     0.1866E+01     0.5000E+00     0.0000E+00     0.0



 n o d a l   s p c   s u m m a r y   o n   *NODE cards
                               boundary conditions (on=1)
        node                      x  y  z rx ry rz           
           1                      0  0  1  0  0  0
           2                      0  0  1  0  0  0
           3                      0  0  1  0  0  0
           4                      0  0  1  0  0  0
           5                      0  0  1  0  0  0
           6                      0  0  1  0  0  0
          10                      0  0  1  0  0  0
          11                      0  0  1  0  0  0
          15                      0  0  1  0  0  0
          16                      0  0  1  0  0  0
          20                      0  0  1  0  0  0
          21                      0  0  1  0  0  0
          22                      0  0  1  0  0  0
          23                      0  0  1  0  0  0
          24                      0  0  1  0  0  0
          25                      0  0  1  0  0  0



 s h e l l   e l e m e n t s

     elem id     part id       node1       node2       node3       node4
      thick1      thick2      thick3      thick4       angle      offset
           1           1           1           6           7           2
  1.0000E-02  1.0000E-02  1.0000E-02  1.0000E-02  0.0000E+00  0.0000E+00
           2           1           6          11          12           7
  1.0000E-02  1.0000E-02  1.0000E-02  1.0000E-02  0.0000E+00  0.0000E+00
           3           1          11          16          17          12
  1.0000E-02  1.0000E-02  1.0000E-02  1.0000E-02  0.0000E+00  0.0000E+00
           4           1          16          21          22          17
  1.0000E-02  1.0000E-02  1.0000E-02  1.0000E-02  0.0000E+00  0.0000E+00
           5           1           2           7           8           3
  1.0000E-02  1.0000E-02  1.0000E-02  1.0000E-02  0.0000E+00  0.0000E+00
           6           1           7          12          13           8
  1.0000E-02  1.0000E-02  1.0000E-02  1.0000E-02  0.0000E+00  0.0000E+00
           7           1          12          17          18          13
  1.0000E-02  1.0000E-02  1.0000E-02  1.0000E-02  0.0000E+00  0.0000E+00
           8           1          17          22          23          18
  1.0000E-02  1.0000E-02  1.0000E-02  1.0000E-02  0.0000E+00  0.0000E+00
           9           1           3           8           9           4
  1.0000E-02  1.0000E-02  1.0000E-02  1.0000E-02  0.0000E+00  0.0000E+00
          10           1           8          13          14           9
  1.0000E-02  1.0000E-02  1.0000E-02  1.0000E-02  0.0000E+00  0.0000E+00
          11           1          13          18          19          14
  1.0000E-02  1.0000E-02  1.0000E-02  1.0000E-02  0.0000E+00  0.0000E+00
          12           1          18          23          24          19
  1.0000E-02  1.0000E-02  1.0000E-02  1.0000E-02  0.0000E+00  0.0000E+00
          13           1           4           9          10           5
  1.0000E-02  1.0000E-02  1.0000E-02  1.0000E-02  0.0000E+00  0.0000E+00
          14           1           9          14          15          10
  1.0000E-02  1.0000E-02  1.0000E-02  1.0000E-02  0.0000E+00  0.0000E+00
          15           1          14          19          20          15
  1.0000E-02  1.0000E-02  1.0000E-02  1.0000E-02  0.0000E+00  0.0000E+00
          16           1          19          24          25          20
  1.0000E-02  1.0000E-02  1.0000E-02  1.0000E-02  0.0000E+00  0.0000E+00



 e l e m e n t   p r i n t o u t 


 shell elements printed 
           6           7          10          11



 l o a d   c u r v e s  

     number of load curves  =           1

     load function id number=           1
     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.-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

      abscissa     ordinate
     0.0000       0.0000000E+00
    1.00000       7.0000000E+02



 p r e s s u r e   b. c.   c a r d s

  card  load curve   start time   node 1   node 2   node 3   node 4  scale factor  load id   ro*c     rb lc#
      1        1      0.000E+00        1        6        7        2     0.100E+01        0
      2        1      0.000E+00        2        7        8        3     0.100E+01        0
      3        1      0.000E+00        3        8        9        4     0.100E+01        0
      4        1      0.000E+00        4        9       10        5     0.100E+01        0
      5        1      0.000E+00        6       11       12        7     0.100E+01        0
      6        1      0.000E+00        7       12       13        8     0.100E+01        0
      7        1      0.000E+00        8       13       14        9     0.100E+01        0
      8        1      0.000E+00        9       14       15       10     0.100E+01        0
      9        1      0.000E+00       11       16       17       12     0.100E+01        0
     10        1      0.000E+00       12       17       18       13     0.100E+01        0
     11        1      0.000E+00       13       18       19       14     0.100E+01        0
     12        1      0.000E+00       14       19       20       15     0.100E+01        0
     13        1      0.000E+00       16       21       22       17     0.100E+01        0
     14        1      0.000E+00       17       22       23       18     0.100E+01        0
     15        1      0.000E+00       18       23       24       19     0.100E+01        0
     16        1      0.000E+00       19       24       25       20     0.100E+01        0







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

 load curve #            1
 *LOAD_SEGMENT, *LOAD_SHELL - pressure load curve

 Performing Recursive Coordinate Bisection (RCB)

Decomposition region 1:

   Everything

Region  1 is distributed

   With no coordinate transformation

Normalized element costs assigned during decomposition:
            Minumum: 1.000000E+00
            Maximum: 1.000000E+00
 Standard Deviation: 0.000000E+00


 Memory required for decomposition      :       265402


 Skew Plate with Normal Pressure (thin shell mesh)                       
            code input version =1993
            formats            =mlarg



 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          = 0.39000000E+02
     x-coordinate of mass center = 0.93301270E+00
     y-coordinate of mass center = 0.25000000E+00
     z-coordinate of mass center = 0.00000000E+00

     inertia tensor of material
     row1=     0.9141E+00    -0.1583E+01     0.0000E+00
     row2=    -0.1583E+01     0.6398E+01     0.0000E+00
     row3=     0.0000E+00     0.0000E+00     0.7312E+01

     principal inertias 
     i11 =    0.4898E+00
     i22 =    0.6823E+01
     i33 =    0.7312E+01

     principal directions
     row1=     0.9659E+00    -0.2588E+00     0.0000E+00
     row2=     0.2588E+00     0.9659E+00     0.0000E+00
     row3=     0.0000E+00     0.0000E+00     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          = 0.39000000E+02
     x-coordinate of mass center = 0.93301270E+00
     y-coordinate of mass center = 0.25000000E+00
     z-coordinate of mass center = 0.00000000E+00

     inertia tensor of body
     row1=     0.9141E+00    -0.1583E+01     0.0000E+00
     row2=    -0.1583E+01     0.6398E+01     0.0000E+00
     row3=     0.0000E+00     0.0000E+00     0.7312E+01

     principal inertias of body
     i11 =    0.4898E+00
     i22 =    0.6823E+01
     i33 =    0.7312E+01

     principal directions
     row1=     0.9659E+00    -0.2588E+00     0.0000E+00
     row2=     0.2588E+00     0.9659E+00     0.0000E+00
     row3=     0.0000E+00     0.0000E+00     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= 0.39000000E+02

 t o t a l  m a s s          = 0.39000000E+02
 x-coordinate of mass center = 0.93301270E+00
 y-coordinate of mass center = 0.25000000E+00
 z-coordinate of mass center = 0.00000000E+00



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


 The following binary output files are being created,
 and contain data equivalent to the indicated ascii output files
   binout0000: (on processor       0)
    elout (shells)                          
    elout_det (shell)                       

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

 Memory required to begin solution (memory=     265402  memory2=      12981 )
          Minimum      12981  on processor     0
          Maximum      12981  on processor     0
          Average      12981 

 Linear Algebra dynamically allocated memory
          Maximum       2231 

 Additional dynamically allocated memory
          Minimum    1577005  on processor     0
          Maximum    1577005  on processor     0
          Average    1577005 

 Total allocated memory
          Minimum    1592217  on processor     0
          Maximum    1592217  on processor     0
          Average    1592217 

  16 smallest timesteps
 ------------------------------------------------
 element       number                part    timestep
 shell             14                   1  2.0683E-05
 shell              7                   1  2.0683E-05
 shell             16                   1  2.0683E-05
 shell             15                   1  2.0683E-05
 shell             12                   1  2.0683E-05
 shell              9                   1  2.0683E-05
 shell              8                   1  2.0683E-05
 shell              4                   1  2.0683E-05
 shell              3                   1  2.0683E-05
 shell              2                   1  2.0683E-05
 shell             13                   1  2.0683E-05
 shell             10                   1  2.0683E-05
 shell              6                   1  2.0683E-05
 shell              5                   1  2.0683E-05
 shell              1                   1  2.0683E-05
 shell             11                   1  2.0683E-05
       1 t 0.0000E+00 dt 1.00E+00 flush i/o buffers            06/07/17 10:01:34
       1 t 0.0000E+00 dt 1.00E+00 write d3plot file            06/07/17 10:01:34

 BEGIN implicit statics  step      1 t= 1.0000E+00             06/07/17 10:01:34
 ============================================================
                time =  1.00000E+00
   current step size =  1.00000E+00
 min. memory for in-core stiffness factorization=            0.1 Mw on processor      0
 
 *** Warning 60124 (IMP+124)
       1 negative eigenvalues detected
       4 t 1.0000E+00 dt 1.00E+00 write d3plot file            06/07/17 10:01:34
 
 *** termination time reached ***

 N o r m a l    t e r m i n a t i o n                          06/07/17 10:01:34
 

 Max. Memory reqd for implicit sol: max used          144742
 Max. Memory reqd for implicit sol: incore            139251
 Max. Memory reqd for implicit sol: oocore            134674

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

 Memory required to complete solution (memory=     265402  memory2=     144742 )
          Minimum     144742  on processor     0
          Maximum     144742  on processor     0
          Average     144742 

 Linear Algebra dynamically allocated memory
          Maximum      23451 

 Additional dynamically allocated memory
          Minimum    1587037  on processor     0
          Maximum    1587037  on processor     0
          Average    1587037 

 Total allocated memory
          Minimum    1755230  on processor     0
          Maximum    1755230  on processor     0
          Average    1755230 

 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 ... 5.0491E-02   42.27     6.5343E-02   13.67
    KW Reading ......... 1.8637E-03    1.56     1.8650E-03    0.39
    KW Writing ......... 1.2611E-03    1.06     1.9670E-03    0.41
  MPP Decomposition .... 1.7882E-02   14.97     1.0466E-01   21.90
    Init Proc .......... 6.4341E-03    5.39     8.3941E-02   17.56
    Decomposition ...... 3.9331E-03    3.29     5.4330E-03    1.14
    Translation ........ 7.4176E-03    6.21     1.5110E-02    3.16
  Initialization ....... 3.0781E-02   25.77     1.5858E-01   33.18
    Init Proc Phase 1 .. 7.5600E-03    6.33     1.2336E-02    2.58
    Init Proc Phase 2 .. 1.2868E-03    1.08     4.8490E-03    1.01
  Element processing ... 1.7734E-03    1.48     1.7750E-03    0.37
    Shells ............. 1.5923E-03    1.33     1.5900E-03    0.33
  Binary databases ..... 5.5955E-04    0.47     1.5380E-03    0.32
  ASCII database ....... 5.6917E-04    0.48     2.0610E-03    0.43
  Contact algorithm .... 1.8987E-05    0.02     1.9000E-05    0.00
  Rigid Bodies ......... 6.3048E-05    0.05     6.2000E-05    0.01
  Implicit ............. 1.8568E-03    1.55     3.1080E-03    0.65
  Implicit Lin. Alg. ... 1.1907E-02    9.97     1.3103E-01   27.42
    Imp. LA Mtx Assemb . 6.9562E-03    5.82     1.1759E-01   24.60
    Imp. LA Factor ..... 4.7603E-03    3.99     1.2397E-02    2.59
    Imp. LA Solve ...... 1.5894E-04    0.13     1.0130E-03    0.21
  Others ............... 3.5474E-03    2.97     9.7500E-03    2.04
  ----------------------------------------------------------------
  T o t a l s            1.1945E-01  100.00     4.7793E-01  100.00

 Problem time       =    1.0000E+00
 Problem cycle      =         4
 Total CPU time     =         0 seconds (   0 hours  0 minutes  0 seconds)
 CPU time per zone cycle  =    317118 nanoseconds
 Clock time per zone cycle=   2333484 nanoseconds

 Parallel execution with      1 MPP proc
 NLQ used/max                72/    72

  C P U   T i m i n g   i n f o r m a t i o n

  Processor   Hostname                              CPU/Avg_CPU  CPU(seconds)
  ---------------------------------------------------------------------------
  #       0   littlefinger.stg.dynamore                 1.00000   1.8000E-01
  ---------------------------------------------------------------------------
  T o t a l s                                                     1.8000E-01


 Start time   06/07/2017 10:01:33  
 End time     06/07/2017 10:01:34  
 Elapsed time       1 seconds(   0 hours  0 min.  1 sec.) for       4 cycles

 N o r m a l    t e r m i n a t i o n                          06/07/17 10:01:34
       4 t 1.0000E+00 dt 1.00E+00 flush i/o buffers            06/07/17 10:01:34
