*HEADING
 : Test Rigid Body Ouput Variables for all shell elements.
 (axisymmetric shells tested in file XRBMAXIS)
 rigid rotation of 1.57080 rad (90 deg) about Z axis.
*RESTART, WRITE, F=999
**
** linear node/element definitions
*NODE, NSET=NALL
  1, 1.0, 0.0, 0.0
  3, 3.0, 0.0, 0.0
 11, 1.0, 2.0, 0.0
 13, 3.0, 2.0, 0.0
*ELEMENT, TYPE=S4R, ELSET=S4R
 1,  1, 3, 13, 11
 2,  1, 3, 13, 11
*ELEMENT, TYPE=S4, ELSET=S4
 3,  1, 3, 13, 11
 4,  1, 3, 13, 11
*ELEMENT, TYPE=S4R5, ELSET=S4R5
 5,  1, 3, 13, 11
*ELEMENT, TYPE=STRI3, ELSET=STRI3
 6,  1, 3, 13
*ELEMENT, TYPE=S3R, ELSET=STRI3
 7,  13, 11, 1
*ELSET, ELSET=LINEAR
 S4R, S4, S4R5, STRI3
*SHELL SECTION, ELSET=LINEAR, MATERIAL=A1
 1.0, 
**
** quadratic node/element definitions
*NODE, NSET=NALL
 51, 1.0, 0.0, 0.0
 52, 2.0, 0.0, 0.0
 53, 3.0, 0.0, 0.0
 61, 1.0, 1.0, 0.0
 62, 2.0, 1.0, 0.0
 63, 3.0, 1.0, 0.0
 71, 1.0, 2.0, 0.0
 72, 2.0, 2.0, 0.0
 73, 3.0, 2.0, 0.0
*ELEMENT, TYPE=S8R, ELSET=S8R
 11,  51, 53, 73, 71, 52, 63, 72, 61
*ELEMENT, TYPE=S8R5, ELSET=S8R5
 12,  51, 53, 73, 71, 52, 63, 72, 61
*ELEMENT, TYPE=S9R5, ELSET=S9R5
 13,  51, 53, 73, 71, 52, 63, 72, 61, 62
*ELEMENT, TYPE=STRI65, ELSET=STRI65
 14,  51, 53, 73, 52, 63, 62
 15,  73, 71, 51, 72, 61, 62
*ELSET, ELSET=QUAD
 S8R, S8R5, S9R5, STRI65
*SHELL SECTION, ELSET=QUAD, MATERIAL=A1
 1.0, 
**
*MATERIAL, NAME=A1
*ELASTIC
 30.0E6, 0.3
*DENSITY
 7.5E-4, 
*BOUNDARY
 1, 1, 2, 0.0
51, 1, 2, 0.0
NALL, 3, 5, 0.0
**
*STEP, NLGEOM, AMP=RAMP, INC=100
*DYNAMIC,DIRECT
 0.02, 1.0
*CONTROLS, PARAMETER=FIELD
 ,,,1.0E-1
*BOUNDARY
NALL, 6, 6, 1.57080
*NODE FILE, F=999
COORD, 
V, 
*EL FILE, ELSET=S4R, F=999
 XC, 
 UC, 
 VC, 
 RI, 
 HC, 
 HO, 
 MASS, 
 VOL, 
*EL FILE, ELSET=S4, F=999
 XC, 
 UC, 
 VC, 
 RI, 
 HC, 
 HO, 
 MASS, 
 VOL, 
*EL FILE, ELSET=S4R5, F=999
 XC, 
 UC, 
 VC, 
 RI, 
 HC, 
 HO, 
 MASS, 
 VOL, 
*EL FILE, ELSET=STRI3, F=999
 XC, 
 UC, 
 VC, 
 RI, 
 HC, 
 HO, 
 MASS, 
 VOL, 
*EL FILE, ELSET=S8R, F=999
 XC, 
 UC, 
 VC, 
 RI, 
 HC, 
 HO, 
 MASS, 
 VOL, 
*EL FILE, ELSET=S8R5, F=999
 XC, 
 UC, 
 VC, 
 RI, 
 HC, 
 HO, 
 MASS, 
 VOL, 
*EL FILE, ELSET=S9R5, F=999
 XC, 
 UC, 
 VC, 
 RI, 
 HC, 
 HO, 
 MASS, 
 VOL, 
*EL FILE, ELSET=STRI65, F=999
 XC, 
 UC, 
 VC, 
 RI, 
 HC, 
 HO, 
 MASS, 
 VOL, 
*NODE PRINT, F=0
*EL PRINT, F=0
*END STEP