*HEADING : NAFEMS TEST LE1, Plane Stress Elements -- Elliptic Membr. [CPS8] *NODE,NSET=EL1 1, 0.00000E+00, 1.0000 , 0.00000E+00 234, 0.58250 ,0.95665 , 0.00000E+00 467, 1.1650 ,0.81283 , 0.00000E+00 600, 1.4975 ,0.66285 , 0.00000E+00 714, 1.7825 ,0.45351 , 0.00000E+00 778, 1.9425 ,0.23806 , 0.00000E+00 801, 2.0000 ,0.00000E+00, 0.00000E+00 1001, 0.00000E+00, 1.2915 , 0.00000E+00 1467, 1.2865 , 1.0498 , 0.00000E+00 1714, 1.9684 ,0.58571 , 0.00000E+00 1801, 2.2085 ,0.00000E+00, 0.00000E+00 2001, 0.00000E+00, 1.5830 , 0.00000E+00 2234, 0.70395 , 1.5144 , 0.00000E+00 2467, 1.4079 , 1.2867 , 0.00000E+00 2600, 1.8097 , 1.0493 , 0.00000E+00 2714, 2.1542 ,0.71791 , 0.00000E+00 2778, 2.3475 ,0.37685 , 0.00000E+00 2801, 2.4170 ,0.00000E+00, 0.00000E+00 3001, 0.00000E+00, 2.1665 , 0.00000E+00 3467, 1.6505 , 1.7610 , 0.00000E+00 3714, 2.5254 ,0.98256 , 0.00000E+00 3801, 2.8335 ,0.00000E+00, 0.00000E+00 4001, 0.00000E+00, 2.7500 , 0.00000E+00 4234, 0.94656 , 2.6308 , 0.00000E+00 4467, 1.8931 , 2.2353 , 0.00000E+00 4600, 2.4334 , 1.8228 , 0.00000E+00 4714, 2.8966 , 1.2472 , 0.00000E+00 4778, 3.1566 ,0.65467 , 0.00000E+00 4801, 3.2500 ,0.00000E+00, 0.00000E+00 *NSET,NSET=XSYM,GEN 1,4001,1000 *NSET,NSET=YSYM,GEN 801,4801,1000 *ELEMENT,TYPE=CPS8, ELSET=EALL 1, 1, 467, 2467, 2001, 234, 1467, 2234, 1001 2, 467, 714, 2714, 2467, 600, 1714, 2600, 1467 3, 714, 801, 2801, 2714, 778, 1801, 2778, 1714 *ELGEN, ELSET=EALL 1, 2, 2000,10 2, 2, 2000,10 3, 2, 2000,10 *MATERIAL,NAME=MATPROP *ELASTIC 210.0E9,0.3 *ELSET,ELSET=LOAD 11,12,13 *SOLID SECTION,MATERIAL=MATPROP, ELSET=EALL 0.1, *BOUNDARY XSYM,XSYMM YSYM,YSYMM *ELSET,ELSET=OUT 3,13 *ELSET,ELSET=PRINT 3, *STEP *STATIC *DLOAD LOAD,P3, -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