*Preprint,model=yes
*Import,update=no,state=yes,step=3,inc=60
 AX, CAR, PROJCAR, RTH, SLP, SLT
 CDN, EUL, FLT, PROJFLT, REV, ROT, UNI
 AX-EUL, CAR-CDN, CAR-ROT, JN-FLT
 LNK-UNI, RTH-CV, SLP-REV, SLT-ALN
*******************************************
** put mass and rotary inertia at top nodes
*******************************************
*ELEMENT, TYPE=MASS, ELSET=MASS
 1011,1303
 1021,1503
 1031,1703
*ELGEN, ELSET=MASS
 1011,5,2,1
 1021,6,2,1
 1031,8,2,1
*ELEMENT, TYPE=MASS, ELSET=MASS
 1041,10507
1042,10305
*MASS, ELSET=MASS
 12.0
*ELEMENT, TYPE=ROTARYI, ELSET=ROTI
 2011,1303
 2021,1503
 2031,1703
*ELGEN, ELSET=ROTI
 2011,5,2,1
 2021,6,2,1
 2031,8,2,1
*ELEMENT, TYPE=ROTARYI, ELSET=ROTI
 2041, 10507
2042,10305
*ROTARY INERTIA, ELSET=ROTI
 120.0, 120.0, 120.0
**************************************************
*BOUNDARY
 1711, 1,2
*BOUNDARY
 plate, 1,6
*BOUNDARY
10305,4,6
*RESTART, WRITE, NUMBER=2, TIME MARKS=YES
*Step
*Dynamic,Explicit,direct user control
 0.0075, 2.5
***Output,field,time interval=0.075,variable=preselect
*OUTPUT,HISTORY, time interval=0.5
*NODE OUTPUT, NSET=TOP
 U,V,A
*Element output,elset=qa_test
CP,CU,CV,CA,CCU,CTF,CVF,CEF,CUE
*End step