*HEADING
**
** ABAQUS INPUT FILE UPGRADE: This input file was upgraded from
** version 5.8 or later to version 6.3 with 0 warning(s) and 1 
** error(s).
** 
** Search the input file for **ERROR.
*RESTART,WRITE,FREQ=999
*PREPRINT,ECHO=YES,HISTORY=NO,MODEL=NO
*NODE,NSET=ALL
1, 
2,10.
3,10.,10.
4,0.,10.
5,5.
6,10.,5.
7,5.,10.
8,0.,5.
*NSET,NSET=LEFT
1,4,8
*NSET,NSET=BOT
1,2,5
*ELEMENT,TYPE=S8R5,ELSET=SHELL
1, 1,2,3,4,5,6,7,8
*SHELL SECTION,MATERIAL=ELMAT, ELSET=SHELL
10.,3
**     **ERROR: The NAME parameter on *REBAR is now required. This parameter will need
**          to be added manually.
**
**
*REBAR LAYER
REBAR1,0.1,2.5,-2.5,RBMAT1,0,1
*MATERIAL,NAME=ELMAT
*ELASTIC
3.E6, 
*DENSITY
7.5E-4, 
*MATERIAL,NAME=RBMAT1
*ELASTIC
30.E6, 
*DENSITY
7.5E-4, 
*NSET,NSET=RIGHT
2,3,6
*BOUNDARY
LEFT,1,6
RIGHT,4
RIGHT,6
*SPECTRUM,TYPE=DISPLACEMENT,NAME=TEST
 0,    0, 0.0
 2, 0.01, 0.0
 2, 1000, 0.0
 0,    0, 0.1
 1, 0.01, 0.1
 1, 1000, 0.1
*STEP
*FREQUENCY,EIGENSOLVER=SUBSPACE
5, 
*MODAL FILE
*EL PRINT, FREQ=0
*NODE PRINT, FREQ=0
*END STEP
*STEP
*RESPONSE SPECTRUM
TEST,0.,0.,1.,1.
*SELECT EIGENMODES
1,2,3
*modal damping, modal=direct
 1,3,0.02
*MODAL PRINT
GU, 
*MODAL FILE
GU, 
*END STEP
*STEP
*FREQUENCY,EIGENSOLVER=SUBSPACE
5, 
*BOUNDARY
2, 1,1,0.
*MODAL FILE
*END STEP