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LOAD FUNCTION NUMBER = 1
NUMBER OF TIME POINTS = 2
TIME VALUE FUNCTION
0.0 0.0
200.00000 0.1592D 02
CONCENTRATED LOADS
NODE DIRECTION LOAD CURVE LOAD CURVE MULTIPL
0 53 3 1 -0.1000D 01
1 I N I T I A L C O N D I T I O N S
INITIAL CONDITIONS CODE (ICON) = 0
EQ.0, ZERO INITIAL CONDITIONS
EQ.1, INITIAL CONDITIONS ARE READ
(BUT RESTART OVER-RIDES ICON)
1E L E M E N T G R O U P D A T A
E L E M E N T G R O U P ........................... = 1 ( NONLINEAR )
E L E M E N T D E F I N I T I O N
ELEMENT TYPE . . . . . . . . . . . . .( NPAR(1) ). . = 2
EQ.1, TRUSS ELEMENTS
EQ.2, 2-DIM ELEMENTS
EQ.3, 3-DIM ELEMENTS
NUMBER OF ELEMENTS. . . . . . . . . . .( NPAR(2) ). . = 10
TYPE OF NONLINEAR ANALYSIS . . . . . .( NPAR(3) ). . = 3
EQ.1, MATERIAL NONLINEARITY ONLY
EQ.2, TOTAL LAGRANGIAN FORMULATION
EQ.3, UPDATED LAGRANGIAN FORMULATION
ELEMENT SUBTYPE . . . . . . . . . . . .( NPAR(5) ). . = 0
EQ.0, AXISYMMETRIC ELEMENTS
EQ.1, PLANE STRAIN ELEMENTS
EQ.2, PLANE STRESS ELEMENTS
MAX NUMBER OF NODES DESCRIBING
ANY ONE ELEMENT . . . . . . . . . .( NPAR(7) ). . = 8
NUMBER OF INTEGRATION POINTS FOR
ELEMENT STIFFNESS GENERATION. . . .( NPAR(10)). . = 2
NUMBER OF STRESS OUTPUT TABLES . . . .( NPAR(13)). . = 0
EQ.0, PRINT AT INTEGRATION POINTS
M A T E R I A L D E F I N I T I O N
MATERIAL MODEL. . . . . . . . . . . . .( NPAR(15)). . = 1
EQ.1, ISOTROPIC
EQ.2, ORTHOTROPIC
EQ.3, VARIABLE TANGENT MODULI
EQ.4, CURVE DESCRIPTION MODEL
EQ.5, CURVE DESCRIPTION MODEL (TENSION CUT-OFF)
EQ.6, ELASTOPLASTIC ( VON MISES )
EQ.7, ELASTOPLASTIC (DRUCKER-PRAGER)
EQ.8, INCOMPRESSIBLE ELASTIC (MOONEY-RIVLIN)
NUMBER OF DIFFERENT SETS OF MATERIAL
CONSTANTS . . . . . . . . . . . . .( NPAR(16)). . = 1
NUMBER OF MATERIAL CONSTANTS PER SET. .( NPAR(17)). . = 2
DIMENSION OF STORAGE ARRAY (WA)
PER INTEGRATION POINT . . . . . . .( NPAR(18)). . = 0
MATERIAL CONSTANTS SET NUMBER .... 1
DEN ..........( DENSITY ).. = 0.0
E ............( PROP(1) ).. = 0.100000D 08
VNU ..........( PROP(2) ).. = 0.300000D 00
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