*HEADING
: DIRECT ENFORCEMENT DISPLACEMENT CONTROL FOR ELASTIC MATERIAL
          WITH DAMAGE, NOT ALIGNED W/ GLOBAL AXES, STACKED [GK3D6]
*NODE,NSET=NALL
1,-0.1464466,-0.5,0.8535533
2,0.3535533,0.2071067,1.3535534
3,0.5,0.7071067,0.5
4,0.0,0.0,0.0
5,-0.5732233,-0.25,0.9267767
6,-0.0732233,0.4571067,1.4267767
7,0.0732233,0.9571067,0.5732233
8,-0.4267767,0.25,0.0732233
9,-1.0,0.0,1.0
10,-0.5,0.7071067,1.5
11,-0.3535533,1.2071067,0.6464466
12,-0.8535533,0.5,0.1464466
*TRANSFORM,NSET=NALL
0.5,0.7071067,0.5,-0.8535533,0.5,0.1464466
*ORIENTATION,NAME=MATAXES
-0.1464466,-0.5,0.8535533,0.5,0.7071067,0.5
3,0.0
*ELEMENT,TYPE=GK3D6,ELSET=EINT
1,1,2,4,5,6,8
2,3,4,2,7,8,6
3,5,6,8,9,10,12
4,7,8,6,11,12,10
*GASKET SECTION,ELSET=EINT,BEHAVIOR=IS,ORIENTATION=MATAXES
*GASKET BEHAVIOR,NAME=IS
*GASKET ELASTICITY,COMPONENT=MEMBRANE
2000.,0.2
*GASKET ELASTICITY,COMPONENT=TRANSVERSE SHEAR
200.,
**
** loading type : DE - Damaged Elasticity
**
*GASKET THICKNESS BEHAVIOR,TYPE=DAMAGE,DIRECTION=LOADING
0.,0.
10.71,0.052
28.57,0.087
46.43,0.139
82.14,0.217
164.3,0.287
*GASKET THICKNESS BEHAVIOR,TYPE=DAMAGE,DIRECTION=UNLOADING
0.0,0.0,0.139
14.28,0.122,0.139
46.43,0.139,0.139
0.,0.,0.217
12.,0.17,0.217
40.,0.21,0.217
82.14,0.217,0.217
0.,0.0,0.287
11.0,0.24,0.287
164.3,0.287,0.287
*EXPANSION
1.e-2,
*******************************************
*AMPLITUDE,NAME=HIST
0.0,-0., 1.0,-0.089, 2.0,-0.098, 3.0,-0.0, 
4.0,-0.098, 5.0,-0.005, 6.0,-0.0, 7.0,-0.105, 
8.0,-0.11, 9.0,-0.0, 10.0,-0.11, 11.0,-0.12, 
12.0,-0.0, 13.0,-0.12, 14.0,-0.13, 15.0,-0.0, 
16.0,-0.13, 17.0,-0.139, 18.0,-0.0, 19.0,-0.139,
20.0,-0.217, 21.0,-0.0, 22.0,-0.217, 23.0,-0.240, 
24.0,-0.0, 25.0,-0.240, 26.0,-0.265, 27.0,-0.0, 
28.0,-0.27, 29.0,-0.295, 30.0,-0.0
*BOUNDARY
1,1,3
2,1,3
3,1,3
4,1,3
*******************************************
*STEP,INC=10000
Test Normal Behavior of Gasket
*STATIC
0.01,30.,,0.01
*BOUNDARY,AMP=HIST
9,2,2,1.0
10,2,2,1.0
11,2,2,1.0
12,2,2,1.0
*NODE PRINT,FREQ=0
U, 
RF, 
*NODE FILE,FREQ=148
U, 
RF, 
*EL PRINT,FREQ=0, ELSET=EINT
S, 
E, 
NE, 
EE, 
EVOL, 
THE, 
TEMP, 
*EL FILE,FREQ=148, ELSET=EINT
E, 
EE, 
NE, 
S, 
EVOL, 
THE, 
*OUTPUT,FIELD,FREQ=148,VAR=PRE
*END STEP
*********************************************
*STEP
Test Membrane Behavior of Element
*STATIC
*BOUNDARY,OP=NEW
1,1,2
2,2,2
3,2,3
4,1,3
5,1,1
7,3,3
8,1,1
8,3,3
9,1,1
11,3,3
12,1,1
12,3,3
2,1,1,0.05
3,1,1,0.05
6,1,1,0.05
7,1,1,0.05
10,1,1,0.05
11,1,1,0.05
*END STEP
*********************************************
*STEP
Test Transverse Behavior of Element
*STATIC
*BOUNDARY,OP=NEW
1,1,3
2,1,3
3,1,3
4,1,3
9,1,1,1.00
9,3,3,1.00
10,1,1,1.00
10,3,3,1.00
11,1,1,1.00
11,3,3,1.00
12,1,1,1.00
12,3,3,1.00
9,2
10,2
11,2
12,2
*END STEP
*******************************************
*STEP
Free Thermal Expansion of Element
*STATIC
*BOUNDARY,OP=NEW
1,1,2
2,2,2
3,2,2
4,1,3
*TEMPERATURE,OP=NEW
NALL,100.
*END STEP
***************************************