*HEADING : NAFEMS TEST LE10: THICK PLATE - PRESSURE FINE MESH, C3D20R ELEMENTS *NODE,NSET=LAY1 1, 0.00000E+00, 1.0000 , 0.00000E+00 2, 0.29000 ,0.98943 , 0.00000E+00 3, 0.58250 ,0.95665 , 0.00000E+00 4, 0.87750 ,0.89861 , 0.00000E+00 5, 1.1650 ,0.81283 , 0.00000E+00 6, 1.3275 ,0.74795 , 0.00000E+00 7, 1.4750 ,0.67535 , 0.00000E+00 8, 1.6475 ,0.56695 , 0.00000E+00 9, 1.7825 ,0.45351 , 0.00000E+00 10, 1.9075 ,0.30060 , 0.00000E+00 11, 1.9675 ,0.17954 , 0.00000E+00 12, 1.9925 ,8.65216E-02, 0.00000E+00 13, 2.0000 ,0.00000E+00, 0.00000E+00 101, 0.00000E+00, 1.1457 , 0.00000E+00 103, 0.61286 , 1.0961 , 0.00000E+00 105, 1.2257 ,0.93130 , 0.00000E+00 107, 1.5519 ,0.77379 , 0.00000E+00 109, 1.8754 ,0.51961 , 0.00000E+00 111, 2.0701 ,0.20571 , 0.00000E+00 113, 2.1043 ,0.00000E+00, 0.00000E+00 201, 0.00000E+00, 1.2915 , 0.00000E+00 202, 0.32023 , 1.2779 , 0.00000E+00 203, 0.64323 , 1.2355 , 0.00000E+00 204, 0.96900 , 1.1606 , 0.00000E+00 205, 1.2865 , 1.0498 , 0.00000E+00 206, 1.4659 ,0.96598 , 0.00000E+00 207, 1.6288 ,0.87223 , 0.00000E+00 208, 1.8193 ,0.73222 , 0.00000E+00 209, 1.9684 ,0.58571 , 0.00000E+00 210, 2.1064 ,0.38823 , 0.00000E+00 211, 2.1726 ,0.23188 , 0.00000E+00 212, 2.2002 ,0.11174 , 0.00000E+00 213, 2.2085 ,0.00000E+00, 0.00000E+00 301, 0.00000E+00, 1.4372 , 0.00000E+00 303, 0.67359 , 1.3750 , 0.00000E+00 305, 1.3472 , 1.1682 , 0.00000E+00 307, 1.7056 ,0.97066 , 0.00000E+00 309, 2.0613 ,0.65181 , 0.00000E+00 311, 2.2752 ,0.25805 , 0.00000E+00 313, 2.3128 ,0.00000E+00, 0.00000E+00 401, 0.00000E+00, 1.5830 , 0.00000E+00 402, 0.35046 , 1.5663 , 0.00000E+00 403, 0.70395 , 1.5144 , 0.00000E+00 404, 1.0605 , 1.4225 , 0.00000E+00 405, 1.4079 , 1.2867 , 0.00000E+00 406, 1.6043 , 1.1840 , 0.00000E+00 407, 1.7825 , 1.0691 , 0.00000E+00 408, 1.9910 ,0.89749 , 0.00000E+00 409, 2.1542 ,0.71791 , 0.00000E+00 410, 2.3052 ,0.47585 , 0.00000E+00 411, 2.3777 ,0.28422 , 0.00000E+00 412, 2.4079 ,0.13696 , 0.00000E+00 413, 2.4170 ,0.00000E+00, 0.00000E+00 501, 0.00000E+00, 1.8747 , 0.00000E+00 503, 0.76460 , 1.7935 , 0.00000E+00 505, 1.5292 , 1.5239 , 0.00000E+00 507, 1.9361 , 1.2661 , 0.00000E+00 509, 2.3398 ,0.85023 , 0.00000E+00 511, 2.5826 ,0.33660 , 0.00000E+00 513, 2.6253 ,0.00000E+00, 0.00000E+00 601, 0.00000E+00, 2.1665 , 0.00000E+00 602, 0.41086 , 2.1436 , 0.00000E+00 603, 0.82526 , 2.0726 , 0.00000E+00 604, 1.2432 , 1.9468 , 0.00000E+00 605, 1.6505 , 1.7610 , 0.00000E+00 606, 1.8808 , 1.6205 , 0.00000E+00 607, 2.0897 , 1.4632 , 0.00000E+00 608, 2.3341 , 1.2283 , 0.00000E+00 609, 2.5254 ,0.98256 , 0.00000E+00 610, 2.7025 ,0.65125 , 0.00000E+00 611, 2.7874 ,0.38899 , 0.00000E+00 612, 2.8229 ,0.18745 , 0.00000E+00 613, 2.8335 ,0.00000E+00, 0.00000E+00 701, 0.00000E+00, 2.4582 , 0.00000E+00 703, 0.88591 , 2.3517 , 0.00000E+00 705, 1.7718 , 1.9982 , 0.00000E+00 707, 2.2433 , 1.6602 , 0.00000E+00 709, 2.7110 , 1.1149 , 0.00000E+00 711, 2.9923 ,0.44137 , 0.00000E+00 713, 3.0418 ,0.00000E+00, 0.00000E+00 801, 0.00000E+00, 2.7500 , 0.00000E+00 802, 0.47125 , 2.7209 , 0.00000E+00 803, 0.94656 , 2.6308 , 0.00000E+00 804, 1.4259 , 2.4712 , 0.00000E+00 805, 1.8931 , 2.2353 , 0.00000E+00 806, 2.1572 , 2.0569 , 0.00000E+00 807, 2.3969 , 1.8572 , 0.00000E+00 808, 2.6772 , 1.5591 , 0.00000E+00 809, 2.8966 , 1.2472 , 0.00000E+00 810, 3.0997 ,0.82665 , 0.00000E+00 811, 3.1972 ,0.49375 , 0.00000E+00 812, 3.2378 ,0.23794 , 0.00000E+00 813, 3.2500 ,0.00000E+00, 0.00000E+00 *NCOPY,SHIFT,OLDSET=LAY1,NEWSET=LAY2,CHANGE NUMBER=1000 0.,0.,0.15 *NCOPY,SHIFT,OLDSET=LAY2,NEWSET=LAY3,CHANGE NUMBER=1000 0.,0.,0.15 *NCOPY,SHIFT,OLDSET=LAY3,NEWSET=LAY4,CHANGE NUMBER=1000 0.,0.,0.15 *NCOPY,SHIFT,OLDSET=LAY4,NEWSET=LAY5,CHANGE NUMBER=1000 0.,0.,0.15 *NSET,NSET=AB,GEN 1, 801,100 1001,1801,100 2001,2801,100 3001,3801,100 4001,4801,100 *NSET,NSET=DC,GEN 13, 813,100 1013,1813,100 2013,2813,100 3013,3813,100 4013,4813,100 *NSET,NSET=BC,GEN 801, 813,1 1801,1813,1 2801,2813,1 3801,3813,1 4801,4813,1 *NSET,NSET=MID,GEN 2801,2813,1 *ELEMENT,TYPE=C3D20R 1, 1,3,203,201,2001,2003,2203,2201,2,103,202,101,2002,2103,2202, 2101,1001,1003,1203,1201 *ELGEN,ELSET=ALLE 1, 6,2,1, 4,200,10, 2,2000,100 *MATERIAL,NAME=MATPROP *ELASTIC 210.0E9,0.3 *ELSET,ELSET=LOAD,GEN 101,136,1 *ELSET,ELSET=EOUT 106, *SOLID SECTION,ELSET=ALLE,MATERIAL=MATPROP *BOUNDARY AB,1 DC,2 BC,1,2 MID,3 *STEP,PERT *STATIC *DLOAD LOAD,P2, 1.0E6 *NODE PRINT,FREQ=0 *EL PRINT,POSITION=AVERAGED AT NODES,ELSET=EOUT S, *EL FILE,POSITION=AVERAGED AT NODES,ELSET=EOUT S, *END STEP