*HEADING
 : Test Rigid Body Ouput Variables for all plane stress elements.
 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=CPS4R, ELSET=CPS4R
 1,  1, 3, 13, 11
*ELEMENT, TYPE=CPS4, ELSET=CPS4
 2,  1, 3, 13, 11
*ELEMENT, TYPE=CPS3, ELSET=CPS3
 3,  1,  3, 13
 4,  13, 11, 1
*SOLID SECTION, ELSET=CPS4R, MATERIAL=A1
*SOLID SECTION, ELSET=CPS4, MATERIAL=A1
*SOLID SECTION, ELSET=CPS3, MATERIAL=A1
**
** 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=CPS8R, ELSET=CPS8R
 11,  51, 53, 73, 71, 52, 63, 72, 61
*ELEMENT, TYPE=CPS8, ELSET=CPS8
 12,  51, 53, 73, 71, 52, 63, 72, 61
*ELEMENT, TYPE=CPS6, ELSET=CPS6
 13,  51, 53, 73, 52, 63, 62
 14,  73, 71, 51, 72, 61, 62
*SOLID SECTION, ELSET=CPS8R, MATERIAL=A1
*SOLID SECTION, ELSET=CPS8, MATERIAL=A1
*SOLID SECTION, ELSET=CPS6, MATERIAL=A1
*ELEMENT, TYPE=B21, ELSET=BEAM
 5, 1, 3
 6, 51, 53
*BEAM SECTION, ELSET=BEAM, SECTION=RECT, MATERIAL=A2
 2.0, 2.0
*MATERIAL, NAME=A1
*ELASTIC
 30.0E6, 0.3
*DENSITY
 7.5E-4, 
*MATERIAL, NAME=A2
*ELASTIC
 30.0E9, 0.3
*DENSITY
 7.5E-9, 
*BOUNDARY
 1, 1, 2, 0.0
51, 1, 2, 0.0
*INITIAL CONDITION, TYPE=VELOCITY
  3, 2,  3.14159
 13, 2,  3.14159
 11, 1, -3.14159
 13, 1, -3.14159
 52, 2,  1.57080
 53, 2,  3.14159
 62, 2,  1.57080
 63, 2,  3.14159
 72, 2,  1.57080
 73, 2,  3.14159
 61, 1, -1.57080
 62, 1, -1.57080
 63, 1, -1.57080
 71, 1, -3.14159
 72, 1, -3.14159
 73, 1, -3.14159
**
*STEP, NLGEOM, AMP=RAMP, INC=100
*DYNAMIC
 0.1, 1.0
*CONTROLS, PARAMETER=FIELD
 ,,,1.0E-1
*BOUNDARY
  1, 6, 6, 1.57080
  3, 6, 6, 1.57080
 51, 6, 6, 1.57080
 53, 6, 6, 1.57080
*NODE FILE, F=999
COORD, 
V, 
*EL FILE, ELSET=CPS4R, F=999
 XC, 
 UC, 
 VC, 
 RI, 
 HC, 
 HO, 
 MASS, 
 VOL, 
*EL FILE, ELSET=CPS4, F=999
 XC, 
 UC, 
 VC, 
 RI, 
 HC, 
 HO, 
 MASS, 
 VOL, 
*EL FILE, ELSET=CPS3, F=999
 XC, 
 UC, 
 VC, 
 RI, 
 HC, 
 HO, 
 MASS, 
 VOL, 
*EL FILE, ELSET=CPS8R, F=999
 XC, 
 UC, 
 VC, 
 RI, 
 HC, 
 HO, 
 MASS, 
 VOL, 
*EL FILE, ELSET=CPS8, F=999
 XC, 
 UC, 
 VC, 
 RI, 
 HC, 
 HO, 
 MASS, 
 VOL, 
*EL FILE, ELSET=CPS6, F=999
 XC, 
 UC, 
 VC, 
 RI, 
 HC, 
 HO, 
 MASS, 
 VOL, 
*NODE PRINT, F=0
*EL PRINT, F=0
*END STEP