*Preprint,model=yes
*Import,update=no,state=yes,step=2,int=2
 AX, CAR, RTH, SLP, SLT
 CDN, EUL, FLT, 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
*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
*ROTARY INERTIA, ELSET=ROTI
 120.0, 120.0, 120.0
**************************************************
*AMPLITUDE, NAME=COSINE, DEF=PERIODIC,time=total time
 1, 2.0, 0.0, 0.0
 1.0, 0.0
*BOUNDARY
 1711, 1,2
*BOUNDARY
 plate, 1,6
*Step
*Dynamic,Explicit,direct user control
 0.0075, 1.25
*CONNECTOR LOAD, AMP=COSINE
 CONN1,1, 4.8
 CONN2,2, 4.8
 CONN3,3, 4.8
 CONN4,4, 48.0
 CONN5,5, 48.0
 CONN6,6, 48.0
***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,CSF,CNF,CTF,CVF,CEF,CRF
*End step