*HEADING
*PREPRINT,MODEL=NO,HISTORY=NO
*****************
** TEST 1: CAX4
*****************
*NODE,NSET=NALL
*NSET,NSET=LEFT
*NSET,NSET=BOT
*NSET,NSET=RIGHT
*ELEMENT,TYPE=CAX4,ELSET=TEST1
*ELSET,ELSET=TEST
*ELSET,ELSET=REFER
*SOLID SECTION,ELSET=TEST1,MATERIAL=ELAS
*****************
** TEST 2: CPE4
*******************
**
*NODE,NSET=NALL
*NSET,NSET=LEFT
*NSET,NSET=BOT
*NSET,NSET=RIGHT
*ELEMENT,TYPE=CPE4,ELSET=TEST2
*ELSET,ELSET=TEST
*ELSET,ELSET=REFER
*SOLID SECTION,ELSET=TEST2,MATERIAL=ELAS
******************
** TEST 3: CGAX4
******************
**
*NODE,NSET=NALL
*NSET,NSET=LEFT
*NSET,NSET=BOT
*NSET,NSET=RIGHT
*ELEMENT,TYPE=CGAX4,ELSET=TEST4
*ELSET,ELSET=TEST
*ELSET,ELSET=REFER
*SOLID SECTION,ELSET=TEST4,MATERIAL=ELAS
*******************
** TEST 4: CAXA
******************
**
*NODE,NSET=NALL
*NSET,NSET=LEFT
*NSET,NSET=BOT
*NSET,NSET=RIGHT
*ELEMENT,TYPE=CAXA41,ELSET=TEST7,OFFSET=10000
*ELSET,ELSET=TEST
*ELSET,ELSET=REFER
*SOLID SECTION,ELSET=TEST7,MATERIAL=ELAS
***************************
** TEST 5: CAX4 WITH REBAR
***************************
*NODE,NSET=NALL
*ELEMENT,TYPE=SFMAX1,ELSET=SFMAX1-1
*SURFACE SECTION,ELSET=SFMAX1-1
*REBAR LAYER,ANGULAR SPACING
REB8A,1.000000,19.188136,0.000000,ELAS,10.000000,1
*EMBEDDED ELEMENT
*ELEMENT,TYPE=SFMAX1,ELSET=SFMAX1-2
*SURFACE SECTION,ELSET=SFMAX1-2
*REBAR LAYER,ANGULAR SPACING
REB8B,1.000000,19.188136,0.000000,ELAS,10.000000,1
*EMBEDDED ELEMENT
*NSET,NSET=LEFT
*NSET,NSET=BOT
*NSET,NSET=RIGHT
*ELEMENT,TYPE=CAX4,ELSET=TEST8
*INITIAL CONDITIONS,TYPE=STRESS,REBAR
1811,REB8A,10.,
1812,REB8B,10.,,
*INITIAL CONDITIONS,TYPE=HARDENING,REBAR
1811,REB8A,0.2,20.,
1812,REB8B,0.2,20.,
*ELSET,ELSET=TEST
*ELSET,ELSET=REFER
*SOLID SECTION,ELSET=TEST8,MATERIAL=ELAS
*****************
** TEST 6: CPE4R
*******************
**
*NODE,NSET=NALL
*NSET,NSET=LEFT
*NSET,NSET=BOT
*NSET,NSET=RIGHT
*ELEMENT,TYPE=CPE4R,ELSET=TEST9
*ELSET,ELSET=TEST
*ELSET,ELSET=REFER
*SOLID SECTION,ELSET=TEST9,MATERIAL=ELAS
******************
** TEST 7: CGAX4R
******************
**
*NODE,NSET=NALL
*NSET,NSET=LEFT
*NSET,NSET=BOT
*NSET,NSET=RIGHT
*ELEMENT,TYPE=CGAX4R,ELSET=TEST11
*ELSET,ELSET=TEST
*ELSET,ELSET=REFER
*SOLID SECTION,ELSET=TEST11,MATERIAL=ELAS
*******************
** TEST 8: CAXA41
******************
**
*NODE,NSET=NALL
*NSET,NSET=LEFT
*NSET,NSET=BOT
*NSET,NSET=RIGHT
*ELEMENT,TYPE=CAXA41,ELSET=TEST14,OFFSET=10000
*ELSET,ELSET=TEST
*ELSET,ELSET=REFER
*SOLID SECTION,ELSET=TEST14,MATERIAL=ELAS
**************************
** TEST 9: S4R WITH REBAR
**************************
**
*NODE,NSET=NALL
*NSET,NSET=LEFT
*NSET,NSET=BOT
*NSET,NSET=RIGHT
*ELEMENT,TYPE=S4R,ELSET=TEST15
*INITIAL CONDITIONS,TYPE=STRESS,REBAR
1501,REB9,10.,
1511,REB9,10.,
***INITIAL CONDITIONS,TYPE=HARDENING,REBAR
**1501,,0.2,20.,
**1511,,0.2,20.,
*ELSET,ELSET=TEST
*ELSET,ELSET=REFER
*SHELL SECTION,ELSET=TEST15,MATERIAL=ELAS
1.,
*REBAR LAYER
REB9,0.5,1.0,0,ELAS,30,1
**************************
** TEST 10: M3D4R WITH REBAR
**************************
**
*NODE,NSET=NALL
*NSET,NSET=LEFT
*NSET,NSET=BOT
*NSET,NSET=RIGHT
*ELEMENT,TYPE=M3D4R,ELSET=TEST16
*INITIAL CONDITIONS,TYPE=STRESS,REBAR
1601,,10.,
1611,,10.,
*INITIAL CONDITIONS,TYPE=HARDENING,REBAR
1601,,0.2,20.,
1611,,0.2,20.,
*ELSET,ELSET=TEST
*ELSET,ELSET=REFER
*MEMBRANE SECTION,ELSET=TEST16,MATERIAL=ELAS
1.,
*REBAR LAYER
REB10,0.5,1.0,0,ELAS,30,1
****************************
** TEST 11: S4 WITH REBAR
**************************
**
*NODE,NSET=NALL
*NSET,NSET=LEFT
*NSET,NSET=BOT
*NSET,NSET=RIGHT
*ELEMENT,TYPE=S4,ELSET=TEST17
*INITIAL CONDITIONS,TYPE=STRESS,REBAR
1701,REB9,10.,
1711,REB9,10.,
***INITIAL CONDITIONS,TYPE=HARDENING,REBAR
**1501,,0.2,20.,
**1511,,0.2,20.,
*ELSET,ELSET=TEST
*ELSET,ELSET=REFER
*SHELL SECTION,ELSET=TEST17,MATERIAL=ELAS
1.,
*REBAR LAYER
REB11,0.5,1.0,0,ELAS,30,1
**
** REMAINDER OF DECK SAME FOR ALL TESTS
**
*ELSET,ELSET=EALL
TEST,REFER
*MATERIAL,NAME=ELAS
*ELASTIC
200.E3,0.3
*PLASTIC,HARD=COMBINED,DATA TYPE=PARAMETERS
200.,2.222E4, 34.65,
*CYCLIC HARDENING, PARAMETERS
*DENSITY
1.E-4,
*INITIAL CONDITIONS,TYPE=STRESS
EALL,10.,
***INITIAL CONDITIONS,TYPE=HARDENING
**EALL,0.2,20.,
**
**
*STEP,,NLGEOM, INC=100
 step #1: REMOVE TEST ELEMENTS
*STATIC
0.1, 1.0
*BOUNDARY
NALL,3,6
LEFT,1
BOT,2
*MODEL CHANGE,REMOVE,TYPE=ELEMENT
TEST,
*EL PRINT,POSITION=CENTROID,FREQ=99
S,
E,
PE,
*EL PRINT,REBAR,FREQ=99
S,E,PE,RBANG,RBROT
*EL FILE,REBAR,FREQ=99
S,E,PE,RBANG,RBROT
*EL FILE,POSITION=CENTROID,FREQ=99
S,E,PE
*NODE PRINT,NSET=LEFT,FREQ=99
RF   ,
*NODE FILE,FREQ=99
RF,
*EL FILE,REBAR
S
E
*END STEP
**
**
*STEP,NLGEOM, INC=100
 STEP #2: ADD TEST ELEMENT BACK IN
*STATIC
.1,1.
*MODEL CHANGE,ADD=STRAINFREE,TYPE=ELEMENT
TEST,
*BOUNDARY
RIGHT,1,1,.02
*END STEP
**
**
**
*STEP,NLGEOM,INC=100
 STEP #3: STRETCH ELEMENTS FURTHER
*STATIC
0.1,1.
*BOUNDARY
RIGHT,1,1,.05
*END STEP