*HEADING
: NAFEMS TEST LE1, Plane Stress Elements -- Elliptic Membr.  [CPS6]
*NODE
    1,     0.00000,     1.0000,    0.00000
  234,     0.58250,    0.95665,    0.00000
  467,      1.1650,    0.81283,    0.00000
  600,      1.4975,    0.66285,    0.00000
  714,      1.7825,    0.45351,    0.00000
  778,      1.9425,    0.23806,    0.00000
  801,      2.0000,    0.00000,    0.00000
 1001,     0.00000,     1.2915,    0.00000
 1234,     0.64323,     1.2355,    0.00000
 1467,      1.2865,     1.0498,    0.00000
 1600,      1.6536,    0.85608,    0.00000
 1714,      1.9684,    0.58571,    0.00000
 1778,      2.1450,    0.30746,    0.00000
 1801,      2.2085,    0.00000,    0.00000
 2001,     0.00000,     1.5830,    0.00000
 2234,     0.70395,     1.5144,    0.00000
 2467,      1.4079,     1.2867,    0.00000
 2600,      1.8097,     1.0493,    0.00000
 2714,      2.1542,    0.71791,    0.00000
 2778,      2.3475,    0.37685,    0.00000
 2801,      2.4170,    0.00000,    0.00000
 3001,     0.00000,     2.1665,    0.00000
 3234,     0.82526,     2.0726,    0.00000
 3467,      1.6505,     1.7610,    0.00000
 3600,      2.1215,     1.4361,    0.00000
 3714,      2.5254,    0.98256,    0.00000
 3778,      2.7520,    0.51576,    0.00000
 3801,      2.8335,    0.00000,    0.00000
 4001,     0.00000,     2.7500,    0.00000
 4234,     0.94656,     2.6308,    0.00000
 4467,      1.8931,     2.2353,    0.00000
 4600,      2.4334,     1.8228,    0.00000
 4714,      2.8966,     1.2472,    0.00000
 4778,      3.1566,    0.65467,    0.00000
 4801,      3.2500,    0.00000,    0.00000
*NSET,NSET=XSYM,GEN
 1,4001,1000
*NSET,NSET=YSYM,GEN
 801,4801,1000
*ELEMENT,TYPE=CPS6, ELSET=EALL
 1,   1, 2467, 2001, 1234, 2234, 1001
 2,   1,  467, 2467,  234, 1467, 1234
 3, 467, 2714, 2467, 1600, 2600, 1467
 4, 467,  714, 2714,  600, 1714, 1600
 5, 714, 2801, 2714, 1778, 2778, 1714
 6, 714,  801, 2801,  778, 1801, 1778
*ELGEN, ELSET=EALL
 1, 2, 2000,10
 2, 2, 2000,10
 3, 2, 2000,10
 4, 2, 2000,10
 5, 2, 2000,10
 6, 2, 2000,10
*MATERIAL,NAME=MATPROP
*ELASTIC
 210.0E9,0.3
*ELSET,ELSET=LOAD
 11,13,15
*SOLID SECTION,MATERIAL=MATPROP, ELSET=EALL
 0.1, 
*BOUNDARY
 XSYM,XSYMM
 YSYM,YSYMM
*ELSET,ELSET=OUT
 5,6,15,16
*ELSET,ELSET=PRINT
 5,6
*STEP
*STATIC
*DLOAD
 LOAD,P2, -10.0E6
*NODE PRINT,FREQ=0
*EL PRINT,ELSET=PRINT, POSITION=AVERAGED AT NODES
 S, 
*EL FILE,ELSET=PRINT, POSITION=AVERAGED AT NODES
 S, 
*END STEP