*HEADING
 : Test Rigid Body Ouput Variables for plane strain els.
 rigid rotation of 1.57080 rad (90 deg) about Z axis.
*RESTART, WRITE, F=1
**
** 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=CPE4R, ELSET=CPE4R
 1,  1, 3, 13, 11
*ELEMENT, TYPE=CPE4, ELSET=CPE4
 2,  1, 3, 13, 11
*ELEMENT, TYPE=CPE3, ELSET=CPE3
 3,  1,  3, 13
 4,  13, 11, 1
*SOLID SECTION, ELSET=CPE4R, MATERIAL=A1
*SOLID SECTION, ELSET=CPE4, MATERIAL=A1
*SOLID SECTION, ELSET=CPE3, MATERIAL=A1
**
** hybrids and incompatible modes
*ELEMENT, TYPE=CPE4RH, ELSET=CPE4RH
 11,  1, 3, 13, 11
*ELEMENT, TYPE=CPE4H, ELSET=CPE4H
 12,  1, 3, 13, 11
*ELEMENT, TYPE=CPE3H, ELSET=CPE3H
 13,  1,  3, 13
 14,  13, 11, 1
*ELEMENT, TYPE=CPE4I, ELSET=CPE4I
 15,  1, 3, 13, 11
*ELEMENT, TYPE=CPE4IH, ELSET=CPE4IH
 16,  1, 3, 13, 11
*SOLID SECTION, ELSET=CPE4RH, MATERIAL=A1
*SOLID SECTION, ELSET=CPE4H, MATERIAL=A1
*SOLID SECTION, ELSET=CPE3H, MATERIAL=A1
*SOLID SECTION, ELSET=CPE4I, MATERIAL=A1
*SOLID SECTION, ELSET=CPE4IH, 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=CPE8R, ELSET=CPE8R
 21,  51, 53, 73, 71, 52, 63, 72, 61
*ELEMENT, TYPE=CPE8, ELSET=CPE8
 22,  51, 53, 73, 71, 52, 63, 72, 61
*ELEMENT, TYPE=CPE6, ELSET=CPE6
 23,  51, 53, 73, 52, 63, 62
 24,  73, 71, 51, 72, 61, 62
*ELEMENT, TYPE=CPE6M, ELSET=CPE6M
 25,  51, 53, 73, 52, 63, 62
 26,  73, 71, 51, 72, 61, 62
*SOLID SECTION, ELSET=CPE8R, MATERIAL=A1
*SOLID SECTION, ELSET=CPE8, MATERIAL=A1
*SOLID SECTION, ELSET=CPE6, MATERIAL=A1
*SOLID SECTION, ELSET=CPE6M, MATERIAL=A1
**
** hybrids
*ELEMENT, TYPE=CPE8RH, ELSET=CPE8RH
 27,  51, 53, 73, 71, 52, 63, 72, 61
*ELEMENT, TYPE=CPE8H, ELSET=CPE8H
 28,  51, 53, 73, 71, 52, 63, 72, 61
*ELEMENT, TYPE=CPE6H, ELSET=CPE6H
 29,  51, 53, 73, 52, 63, 62
 30,  73, 71, 51, 72, 61, 62
*ELEMENT, TYPE=CPE6MH, ELSET=CPE6MH
 31,  51, 53, 73, 52, 63, 62
 32,  73, 71, 51, 72, 61, 62
*SOLID SECTION, ELSET=CPE8RH, MATERIAL=A1
*SOLID SECTION, ELSET=CPE8H, MATERIAL=A1
*SOLID SECTION, ELSET=CPE6H, MATERIAL=A1
*SOLID SECTION, ELSET=CPE6MH, MATERIAL=A1
*ELEMENT, TYPE=B21, ELSET=BEAM
 45, 1, 3
 46, 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
 5.0E-2,,,1.0E-2
*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=CPE4R, F=999
 XC, 
 UC, 
 VC, 
 RI, 
 HC, 
 HO, 
 MASS, 
 VOL, 
*EL FILE, ELSET=CPE4, F=999
 XC, 
 UC, 
 VC, 
 RI, 
 HC, 
 HO, 
 MASS, 
 VOL, 
*EL FILE, ELSET=CPE3, F=999
 XC, 
 UC, 
 VC, 
 RI, 
 HC, 
 HO, 
 MASS, 
 VOL, 
*EL FILE, ELSET=CPE4RH, F=999
 XC, 
 UC, 
 VC, 
 RI, 
 HC, 
 HO, 
 MASS, 
 VOL, 
*EL FILE, ELSET=CPE4H, F=999
 XC, 
 UC, 
 VC, 
 RI, 
 HC, 
 HO, 
 MASS, 
 VOL, 
*EL FILE, ELSET=CPE3H, F=999
 XC, 
 UC, 
 VC, 
 RI, 
 HC, 
 HO, 
 MASS, 
 VOL, 
*EL FILE, ELSET=CPE4I, F=999
 XC, 
 UC, 
 VC, 
 RI, 
 HC, 
 HO, 
 MASS, 
 VOL, 
*EL FILE, ELSET=CPE4IH, F=999
 XC, 
 UC, 
 VC, 
 RI, 
 HC, 
 HO, 
 MASS, 
 VOL, 
*EL FILE, ELSET=CPE8R, F=999
 XC, 
 UC, 
 VC, 
 RI, 
 HC, 
 HO, 
 MASS, 
 VOL, 
*EL FILE, ELSET=CPE8, F=999
 XC, 
 UC, 
 VC, 
 RI, 
 HC, 
 HO, 
 MASS, 
 VOL, 
*EL FILE, ELSET=CPE6, F=999
 XC, 
 UC, 
 VC, 
 RI, 
 HC, 
 HO, 
 MASS, 
 VOL, 
*EL FILE, ELSET=CPE6M, F=999
 XC, 
 UC, 
 VC, 
 RI, 
 HC, 
 HO, 
 MASS, 
 VOL, 
*EL FILE, ELSET=CPE8RH, F=999
 XC, 
 UC, 
 VC, 
 RI, 
 HC, 
 HO, 
 MASS, 
 VOL, 
*EL FILE, ELSET=CPE8H, F=999
 XC, 
 UC, 
 VC, 
 RI, 
 HC, 
 HO, 
 MASS, 
 VOL, 
*EL FILE, ELSET=CPE6H, F=999
 XC, 
 UC, 
 VC, 
 RI, 
 HC, 
 HO, 
 MASS, 
 VOL, 
*EL FILE, ELSET=CPE6MH, F=999
 XC, 
 UC, 
 VC, 
 RI, 
 HC, 
 HO, 
 MASS, 
 VOL, 
*OUTPUT,FIELD,FREQ=1
*ELEMENT OUTPUT
S,
*OUTPUT,FIELD,FREQ=1
*NODE OUTPUT
 U,
*ELEMENT OUTPUT,POS=NODES
S,
MISESONLY,PRESSONLY
*NODE PRINT, F=0
*EL PRINT, F=0
*END STEP