*HEADING
 NAFEMS TEST FV22, [SC6R] L.O.E. MESH     
 Shell Elements -- Clamped thick rhombic plate          
*PREPRINT, MODEL=YES
*NODE
    1,0.,0.
   11,10.,0.
 1001,7.07107,7.07107
 1011,17.707107,7.07107
 2001,0.,0.,1.0
 2011,10.,0.,1.0
 3001,7.07107,7.07107,1.0
 3011,17.707107,7.07107,1.0
*NGEN,NSET=EDGE1
 1,11
*NGEN,NSET=EDGE3
 1001,1011
*NFILL,NSET=ALLN
 EDGE1,EDGE3,10,100
*NGEN,NSET=EDGE11
 2001,2011
*NGEN,NSET=EDGE31
 3001,3011
*NFILL,NSET=ALLN
 EDGE11,EDGE31,10,100
*NSET,NSET=EDGE2,GEN
   11,1011,100
*NSET,NSET=EDGE21,GEN
 2011,3011,100
*NSET,NSET=EDGE4,GEN
    1,1001,100
*NSET,NSET=EDGE41,GEN
 2001,3001,100
*NSET,NSET=BOT_EDGE
 EDGE1,EDGE2,EDGE3,EDGE4
*NSET,NSET=TOP_EDGE
 EDGE11,EDGE21,EDGE31,EDGE41
*NSET,NSET=EDGE
 TOP_EDGE, BOT_EDGE
*NSET,NSET=TRANSF
 EDGE2,EDGE4,EDGE21,EDGE41
*NSET, NSET=INT_BOT, GEN
 2102,2110,1
 2202,2210,1
 2302,2310,1
 2402,2410,1
 2502,2510,1
 2602,2610,1
 2702,2710,1
 2802,2810,1
 2902,2910,1
*NSET, NSET=INT_TOP, GEN
 102,110,1
 202,210,1
 302,310,1
 402,410,1
 502,510,1
 602,610,1
 702,710,1
 802,810,1
 902,910,1
*TRANSFORM,NSET=TRANSF
 0.707107,0.707107,0., -0.707107,0.707107,0.
*ELEMENT,TYPE=SC6R
 1, 1,2,102,2001,2002,2102
 10000, 1,102,101, 2001,2102,2101
*ELGEN,ELSET=ALLE
 1, 10,1,1, 10,100,10
 10000, 10,1,1, 10,100,10
*SHELL SECTION,ELSET=ALLE,MATERIAL=MAT
 1.0,
*MATERIAL,NAME=MAT
*ELASTIC
 200.E9,0.3
*DENSITY
 8000.,
*BOUNDARY
 EDGE,1,3
*EQUATION
 2
 INT_TOP, 1, 1.0, INT_BOT, 1, 1.0
 2
 INT_TOP, 2, 1.0, INT_BOT, 2, 1.0
 2
 INT_TOP, 3, 1.0, INT_BOT, 3, -1.0
*STEP,PERT
*FREQUENCY, eigensolver=lanczos, SIM=NO
 6, , 
*OUTPUT,FIELD,VAR=PRESELECT
*NODE PRINT
*EL PRINT,F=0
*ENDSTEP