*HEADING
*PREPRINT,MODEL=NO,HISTORY=NO
*****************
** TEST 1: CAX4H
*****************
*NODE,NSET=NALL
*NSET,NSET=LEFT
*NSET,NSET=BOT
*NSET,NSET=RIGHT
*ELEMENT,TYPE=CAX4H,ELSET=TEST1
*ELSET,ELSET=TEST
*ELSET,ELSET=REFER
*SOLID SECTION,ELSET=TEST1,MATERIAL=ELAS
*****************
** TEST 2: CPE4H
*******************
**
*NODE,NSET=NALL
*NSET,NSET=LEFT
*NSET,NSET=BOT
*NSET,NSET=RIGHT
*ELEMENT,TYPE=CPE4H,ELSET=TEST2
*ELSET,ELSET=TEST
*ELSET,ELSET=REFER
*SOLID SECTION,ELSET=TEST2,MATERIAL=ELAS
******************
** TEST 3: CGAX4H
******************
**
*NODE,NSET=NALL
*NSET,NSET=LEFT
*NSET,NSET=BOT
*NSET,NSET=RIGHT
*ELEMENT,TYPE=CGAX4H,ELSET=TEST4
*ELSET,ELSET=TEST
*ELSET,ELSET=REFER
*SOLID SECTION,ELSET=TEST4,MATERIAL=ELAS
*******************
** TEST 4: CAXA4H1
******************
**
*NODE,NSET=NALL
*NSET,NSET=LEFT
*NSET,NSET=BOT
*NSET,NSET=RIGHT
*ELEMENT,TYPE=CAXA4H1,ELSET=TEST7,OFFSET=10000
*ELSET,ELSET=TEST
*ELSET,ELSET=REFER
*SOLID SECTION,ELSET=TEST7,MATERIAL=ELAS
***************************
** TEST 5: CAX4H WITH REBAR
***************************
*NODE,NSET=NALL
*NSET,NSET=LEFT
*NSET,NSET=BOT
*NSET,NSET=RIGHT
*ELEMENT,TYPE=CAX4H,ELSET=TEST8
*ELEMENT,TYPE=SFMAX1,ELSET=SFMAX1-1
*SURFACE SECTION,ELSET=SFMAX1-1
*REBAR LAYER,ANGULAR SPACING
REB8A,1.000000,19.188136,0.000000,REBAR,10.000000,1
*EMBEDDED ELEMENT,HOST ELSET=CAX4H_ONE
*ELEMENT,TYPE=SFMAX1,ELSET=SFMAX1-2
*SURFACE SECTION,ELSET=SFMAX1-2
*REBAR LAYER,ANGULAR SPACING
REB8B,1.000000,19.188136,0.000000,REBAR,10.000000,1
*EMBEDDED ELEMENT,HOST ELSET=CAX4H_TWO
*INITIAL CONDITIONS,TYPE=STRESS,REBAR
1811, REB8A, -1.0
1812, REB8B, -1.0
*ELSET,ELSET=TEST
*ELSET,ELSET=REFER
*ELSET,ELSET=CAX4H_ONE
*ELSET,ELSET=CAX4H_TWO
*SOLID SECTION,ELSET=TEST8,MATERIAL=ELAS
*****************
** TEST 6: CPE4RH
*******************
**
*NODE,NSET=NALL
*NSET,NSET=LEFT
*NSET,NSET=BOT
*NSET,NSET=RIGHT
*ELEMENT,TYPE=CPE4RH,ELSET=TEST9
*ELSET,ELSET=TEST
*ELSET,ELSET=REFER
*SOLID SECTION,ELSET=TEST9,MATERIAL=ELAS
*HOURGLASS STIFFNESS
******************
** TEST 7: CGAX4RH
******************
**
*NODE,NSET=NALL
*NSET,NSET=LEFT
*NSET,NSET=BOT
*NSET,NSET=RIGHT
*ELEMENT,TYPE=CGAX4RH,ELSET=TEST11
*ELSET,ELSET=TEST
*ELSET,ELSET=REFER
*SOLID SECTION,ELSET=TEST11,MATERIAL=ELAS
*HOUR GLASS STIFFNESS
*******************
** TEST 8: CAXAH
******************
**
*NODE,NSET=NALL
*NSET,NSET=LEFT
*NSET,NSET=BOT
*NSET,NSET=RIGHT
*ELEMENT,TYPE=CAXA4H1,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
*ELSET,ELSET=TEST
*ELSET,ELSET=REFER
*SHELL SECTION,ELSET=TEST15,MATERIAL=ELAS
1.,
*REBAR LAYER
REB15,0.5,1.0,0,REBAR,30,1
**************************
** TEST 10: M3D4R WITH REBAR
**************************
**
*NODE,NSET=NALL
*NSET,NSET=LEFT
*NSET,NSET=BOT
*NSET,NSET=RIGHT
*ELEMENT,TYPE=M3D4R,ELSET=TEST16
*ELSET,ELSET=TEST
*ELSET,ELSET=REFER
*MEMBRANE SECTION,ELSET=TEST16,MATERIAL=ELAS
1.,
*REBAR LAYER
REB16,0.5,1.0,0,REBAR,30,1
**
** REMAINDER OF DECK SAME FOR ALL TESTS
**
*ELSET,ELSET=EALL
TEST,REFER
*MATERIAL,NAME=REBAR
*ELASTIC
1000., .25
*MATERIAL,NAME=ELAS
*HYPERELASTIC
80., 20.
*INITIAL CONDITIONS,TYPE=STRESS
 EALL,1.0
**
**
*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,
STH,
E,
*EL PRINT,REBAR,FREQ=99
S,E,RBANG,RBROT
*EL FILE,REBAR,FREQ=99
S,E,RBANG
*EL FILE,REBAR,FREQ=99
RBROT,
*EL FILE,POSITION=CENTROID,FREQ=99
S,E
*NODE PRINT,NSET=LEFT,FREQ=99
RF   ,
*NODE FILE,FREQ=99
RF   ,
*END STEP
**
**
*STEP,NLGEOM, INC=100
 STEP #2: ADD TEST ELEMENT BACK IN
*STATIC
.1,1.
*MODEL CHANGE,ADD=WITHSTRAIN,TYPE=ELEMENT
TEST,
*BOUNDARY
RIGHT,1,1,.2
*END STEP
**
**
*STEP,NLGEOM, INC=100
 STEP #3: REMOVE TEST ELEMENT
*STATIC
.1,1.
*MODEL CHANGE,REMOVE,TYPE=ELEMENT
TEST,
*BOUNDARY,OP=NEW
NALL,3,6
LEFT,1
BOT,2
RIGHT,1
*EL FILE,REBAR,FREQ=99
S,E,RBANG
*EL FILE,POSITION=CENTROID,FREQ=99
S,E
*END STEP
**
**
*STEP,NLGEOM, INC=100
 STEP #4: STRETCH ELEMENTS FURTHER WHILE ELEMENTS ARE ABSENT
*STATIC
.1,1.
*BOUNDARY
RIGHT,1,1,.3
*MODEL CHANGE,ADD=WITHSTRAIN,TYPE=ELEMENT
TEST,
*EL FILE,REBAR,FREQ=99
S,E,RBANG
*EL FILE,REBAR,FREQ=99
RBROT,
*EL FILE,POSITION=CENTROID,FREQ=99
S,E
*END STEP
**