*HEADING
: TEST MASS PROPERTIES FOR CAX3, CAX4R, SAX1, MAX1 
ELEMENTS INCLUDED IN A RIGID BODY (CONCENTRATED LOAD)
DEFORMABLE TO RIGID ELEMENTS
*PREPRINT, ECHO=YES, MODEL=YES, HISTORY=YES
*RESTART,WRITE
*NODE,NSET=NODES
101,4.0,-3.0
102,4.0,-1.0
103,2.0,-1.0
104,2.0,1.0
105,4.0,1.0
106,4.0,3.0
301,0.0,4.0
302,1.0,4.0
1010,4.0,4.0
1020,4.0,6.0
1030,2.0,6.0
1040,2.0,8.0
1050,4.0,8.0
1060,4.0,10.0
3010,0.0,11.0
3020,1.0,11.0
30100,0.0,12.0
30200,1.0,12.0
303,0.0,-4.0
304,1.0,-4.0
*NSET,NSET=RFNODE
100, 
*ELEMENT, TYPE=CAX4R, ELSET=CAX1
101,103,102,105,104
*ELEMENT, TYPE=CAX3, ELSET=CAX2
1010,1030,1020,1040
1040,1040,1020,1050
*ELEMENT, TYPE=SAX1, ELSET=SHELL1
102,101,102
103,105,106
301,302,301
*ELEMENT, TYPE=MAX1, ELSET=SHELL2
1020,1010,1020
1030,1050,1060
3010,3020,3010
*ELEMENT, TYPE=SAX1, ELSET=SHELL3
302,304,303
*ELEMENT, TYPE=SAX1, ELSET=RIG1
30100,30100,30200
*SOLID SECTION, ELSET=CAX1,MATERIAL=MAT1
1.0, 
*SOLID SECTION, ELSET=CAX2, MATERIAL=MAT1
1.0, 
*SHELL SECTION,MATERIAL=MAT1,ELSET=SHELL1
1.0, 
*MEMBRANE SECTION,MATERIAL=MAT1,ELSET=SHELL2
1.0, 
*SHELL SECTION,MATERIAL=MAT1,ELSET=SHELL3
1.0, 
*SHELL SECTION,MATERIAL=MAT1,ELSET=RIG1
0.1, 
*MATERIAL, NAME=MAT1
*ELASTIC
2.E+9, .3
*DENSITY
1.0, 
*ELSET, ELSET=RIGID
CAX1, CAX2, SHELL1, SHELL2, RIG1
*RIGID BODY,ELSET=RIGID,REF NODE=100,POSITION=CENTER OF MASS
*BOUNDARY
100,2,2
304,1,2
*STEP, NLGEOM, INC=100
*DYNAMIC
0.001 , 0.01
*CLOAD
100,1,1.E5
*OUTPUT, FIELD,FREQ=1
*NODE OUTPUT, NSET=NODES
U
*NODE FILE, F=10
U, 
*END STEP