Hello everyone,
I am trying to do a Non Linear analysys on a plate with dimensions 500 x 200 x 10 mm.
My setup is 40 steps in 1 second.
But after 26 steps, the analysys stops with the error: "Part (1) requires more memory than available. Please reduce the part size"
So it says I need to split my part into smaller parts, but does anyone have an idea how to split my file into smaller parts with the same end result?
So what do I have to split and what do I have to do?
Here is an image of my plate:
Can someone help me?
Thanks in advance,
Thomas
Hi Thomas,
I find it hard to believe the error message. Why would it run for 26 steps and then run out of memory? What are you doing in the analysis? What are the loads, setup, material models, material properties, and so on? You may want to take a closer look at the log file to see if there is some other hint, warning, or error that occurs before the "more memory" error.
But to answer your question, the software is implying that you need to create an assembly of parts instead of one part to model the 500 x 200 x 10 mm plate. Two parts, each 250 x 200 x 10 mm and arranged end-to-end, is the same as the 500 x 200 x 100 mm model.
Or 5 pieces each 100 x 200 x 10.
Or 100000 parts each 1 x 1 x 10 mm, etc. (Ok, maybe a 100000 part assembly is overkill ;-).
Thanks for the help.
I am doing Static Stress with Nonlinear materials.
My load curve:
The material properties:
My setup is the left side of the plate is Fixed and on the right side of the plate there is a force in the direction of X
In the log, I don't see any other warnings:
Autodesk(R) Simulation Mechanical Event Simulation (MES) Version 2014.00.00.0513-WIN 22-Feb-2013 Copyright (c) 2013, Autodesk, Inc. All rights reserved. ** Total available memory = 372920 (KB). ** Options executed are: NOMIN - NO optimization for matrix storage RUN - Execute processor STRAIN - Output strain data for Superview DUPLEX - Duplex communication with tWAIT=5 seconds PRRO - Output reaction force data, n=2 STATIC - Static solution: do not consider inertial and damping effects ** Perform analysis ** Reading input file ... PROGRAM VERSION: 201400000513 alg-win-ix86.dll VERSION: 201400000513 algconfig-win-ix86.dll VERSION: 201400000513 agsdb_ar-win-ix86.dll VERSION: 201400000513 solvercallback-win-ix86.dll VERSION: 201400000513 amgsolve.exe VERSION: 0360000000 NUMNP DOF NEGL NEGNL MODEX NSTE DT TSTART IPRI IPSF 124472 000111 0 1 1 40 0.250E-01 0.000E+00 1 3 ** Open output files ... ** Open temporary files ... Model=C:\Users\Thomas\Dropbox\Masterproef\Plastische controle\Plaat 500 x 200 - PLASTISCH.ds_data\1\ds **** Model Unit System Settings: -------------------------------------------- Unit System : Custom Force : N Length : mm Time : s Temperature (Absolute) : deg C (K) Thermal Energy : J Voltage : V Current : A Electrical Resistance : ohm Mass : N*s^2/mm -------------------------------------------- No. of nodes = 124472 No. of equations = 371514 Maximum no. of iteration = 15 No. of steps = 40 Convergence tolerance = 1.0000E-04 ** Input elements... ** 3-D continuum element calculation, number of element = 24453 ** Nonzero entries initially in upper triangle matrix = 27642894 ** Parallel AMG Iterative Solver Solution Time Percent DT L Iter. Residual 0.00000000E+00 0.0000 0.025000 1 0 0.0000E+00 2.50000000E-02 2.5000 0.025000 1 1 2.4917E-01 2.50000000E-02 2.5000 0.025000 1 2 3.8934E-03 2.50000000E-02 2.5000 0.025000 1 3 1.1482E-07c 5.00000000E-02 5.0000 0.025000 1 1 2.4918E-01 5.00000000E-02 5.0000 0.025000 1 2 3.8927E-03 5.00000000E-02 5.0000 0.025000 1 3 1.1474E-07c 7.50000000E-02 7.5000 0.025000 1 1 2.4916E-01 7.50000000E-02 7.5000 0.025000 1 2 3.8913E-03 7.50000000E-02 7.5000 0.025000 1 3 1.1459E-07c 1.00000000E-01 10.0000 0.025000 1 1 2.4911E-01 1.00000000E-01 10.0000 0.025000 1 2 3.8892E-03 1.00000000E-01 10.0000 0.025000 1 3 1.1436E-07c 1.25000000E-01 12.5000 0.025000 1 1 2.4903E-01 1.25000000E-01 12.5000 0.025000 1 2 3.8864E-03 1.25000000E-01 12.5000 0.025000 1 3 1.1409E-07c 1.50000000E-01 15.0000 0.025000 1 1 2.4892E-01 1.50000000E-01 15.0000 0.025000 1 2 3.8830E-03 1.50000000E-01 15.0000 0.025000 1 3 1.1373E-07c 1.75000000E-01 17.5000 0.025000 1 1 2.4878E-01 1.75000000E-01 17.5000 0.025000 1 2 3.8789E-03 1.75000000E-01 17.5000 0.025000 1 3 1.1329E-07c 2.00000000E-01 20.0000 0.025000 1 1 2.4862E-01 2.00000000E-01 20.0000 0.025000 1 2 3.8741E-03 2.00000000E-01 20.0000 0.025000 1 3 1.1280E-07c 2.25000000E-01 22.5000 0.025000 1 1 2.4842E-01 2.25000000E-01 22.5000 0.025000 1 2 3.8686E-03 2.25000000E-01 22.5000 0.025000 1 3 1.1222E-07c 2.50000000E-01 25.0000 0.025000 1 1 2.4819E-01 2.50000000E-01 25.0000 0.025000 1 2 3.8625E-03 2.50000000E-01 25.0000 0.025000 1 3 1.1157E-07c 2.75000000E-01 27.5000 0.025000 1 1 2.4794E-01 2.75000000E-01 27.5000 0.025000 1 2 3.8557E-03 2.75000000E-01 27.5000 0.025000 1 3 1.1090E-07c 3.00000000E-01 30.0000 0.025000 1 1 2.4765E-01 3.00000000E-01 30.0000 0.025000 1 2 3.8482E-03 3.00000000E-01 30.0000 0.025000 1 3 1.1017E-07c 3.25000000E-01 32.5000 0.025000 1 1 2.4734E-01 3.25000000E-01 32.5000 0.025000 1 2 3.8401E-03 3.25000000E-01 32.5000 0.025000 1 3 1.0938E-07c 3.50000000E-01 35.0000 0.025000 1 1 2.4700E-01 3.50000000E-01 35.0000 0.025000 1 2 3.8313E-03 3.50000000E-01 35.0000 0.025000 1 3 1.0851E-07c 3.75000000E-01 37.5000 0.025000 1 1 2.4663E-01 3.75000000E-01 37.5000 0.025000 1 2 3.8219E-03 3.75000000E-01 37.5000 0.025000 1 3 1.0760E-07c 4.00000000E-01 40.0000 0.025000 1 1 2.4623E-01 4.00000000E-01 40.0000 0.025000 1 2 3.8119E-03 4.00000000E-01 40.0000 0.025000 1 3 1.0664E-07c 4.25000000E-01 42.5000 0.025000 1 1 2.4364E-01 4.25000000E-01 42.5000 0.025000 1 2 3.8782E-03 4.25000000E-01 42.5000 0.025000 1 3 1.1607E-06c 4.50000000E-01 45.0000 0.025000 1 1 2.3028E-01 4.50000000E-01 45.0000 0.025000 1 2 4.0684E-03 4.50000000E-01 45.0000 0.025000 1 3 1.1767E-05c 4.75000000E-01 47.5000 0.025000 1 1 2.0132E-01 4.75000000E-01 47.5000 0.025000 1 2 4.1244E-03 4.75000000E-01 47.5000 0.025000 1 3 7.6848E-05c 5.00000000E-01 50.0000 0.025000 1 1 1.4168E-01 5.00000000E-01 50.0000 0.025000 1 2 2.7945E-03 5.00000000E-01 50.0000 0.025000 1 3 3.2915E-04 5.00000000E-01 50.0000 0.025000 1 4 9.0525E-06c 5.25000000E-01 52.5000 0.025000 1 1 7.1351E-02 5.25000000E-01 52.5000 0.025000 1 2 1.4980E-03 5.25000000E-01 52.5000 0.025000 1 3 1.5592E-03 5.25000000E-01 52.5000 0.025000 1 4 1.4550E-05c 5.50000000E-01 55.0000 0.025000 1 1 3.3717E-02 5.50000000E-01 55.0000 0.025000 1 2 1.1002E-02 5.50000000E-01 55.0000 0.025000 1 3 4.0442E-03 5.50000000E-01 55.0000 0.025000 1 4 1.1641E-04 5.50000000E-01 55.0000 0.025000 1 5 2.8452E-06c 5.75000000E-01 57.5000 0.025000 1 1 5.0380E-02 5.75000000E-01 57.5000 0.025000 1 2 1.1844E-02 5.75000000E-01 57.5000 0.025000 1 3 1.3693E-02 5.75000000E-01 57.5000 0.025000 1 4 1.2932E-03 5.75000000E-01 57.5000 0.025000 1 5 4.2095E-06c 6.00000000E-01 60.0000 0.025000 1 1 1.0019E-01 6.00000000E-01 60.0000 0.025000 1 2 6.6348E-02 6.00000000E-01 60.0000 0.025000 1 3 3.2212E-02 6.00000000E-01 60.0000 0.025000 1 4 2.0882E-03 6.00000000E-01 60.0000 0.025000 1 5 3.1911E-05c 6.25000000E-01 62.5000 0.025000 1 1 1.4862E-01 6.25000000E-01 62.5000 0.025000 1 2 6.5035E-01 6.25000000E-01 62.5000 0.025000 1 3 3.6426E-02 6.25000000E-01 62.5000 0.025000 1 4 1.8292E-02 6.25000000E-01 62.5000 0.025000 1 5 3.7518E-03 6.25000000E-01 62.5000 0.025000 1 6 1.0534E-05c 6.50000000E-01 65.0000 0.025000 1 1 1.8483E-01 6.50000000E-01 65.0000 0.025000 1 2 7.7191E-01 6.50000000E-01 65.0000 0.025000 1 3 1.0269E-01 6.50000000E-01 65.0000 0.025000 1 4 3.9590E-02 6.50000000E-01 65.0000 0.025000 1 5 1.1151E-02 6.50000000E-01 65.0000 0.025000 1 6 3.9761E-03 6.50000000E-01 65.0000 0.025000 1 7 4.6740E-04 6.50000000E-01 65.0000 0.025000 1 8 3.7943E-05c 6.75000000E-01 67.5000 0.025000 1 1 2.1233E-01 6.75000000E-01 67.5000 0.025000 1 2 9.8431E-01 6.75000000E-01 67.5000 0.025000 1 3 1.7425E-01 6.75000000E-01 67.5000 0.025000 1 4 1.1709E-01 6.75000000E-01 67.5000 0.025000 1 5 8.6586E-03 6.75000000E-01 67.5000 0.025000 1 6 2.2657E-01 6.75000000E-01 67.5000 0.025000 1 7 3.9378E-02 6.75000000E-01 67.5000 0.025000 1 8 1.9340E-02 ** Error: Part (1) requires more memory than available. Please reduce the part size by splitting it to several smaller parts ** Error (1) ** Job started : 2014-03-28 09:28:25 ** Job finished : 2014-03-28 11:02:04 ** Total elapsed time : 1:32:38 (hours:minutes:seconds) !! Program aborted !
And the summary:
Autodesk(R) Simulation Mechanical Event Simulation (MES) Version 2014.00.00.0513-WIN 22-Feb-2013 Copyright (c) 2013, Autodesk, Inc. All rights reserved. ---------------------------------------------------------------- Date & Time : 2014-03-28 09:28:25 Input Model : C:\Users\Thomas\Dropbox\Masterproef\Plastische controle\Plaat 500 x 200 - PLAST ISCH.ds_data\1\ds Command Line Options : silent ** Model description **** Model Unit System Settings: -------------------------------------------- Unit System : Custom Force : N Length : mm Time : s Temperature (Absolute) : deg C (K) Thermal Energy : J Voltage : V Current : A Electrical Resistance : ohm Mass : N*s^2/mm -------------------------------------------- ** Master Control Information Number of nodal points . . . . . . (NUMNP) =124472 Master x-translation code . . . . . (IDOF(1)) = 0 Master y-translation code . . . . . (IDOF(2)) = 0 Master z-translation code . . . . . (IDOF(3)) = 0 Master x-rotation code . . . . . (IDOF(4)) = 1 Master y-rotation code . . . . . (IDOF(5)) = 1 Master z-rotation code . . . . . (IDOF(6)) = 1 Number of linear element parts. . . (NEGL) = 0 Number of nonlinear element parts . (NEGNL) = 1 Solution mode . . . . . . . . . . . (MODEX) = 2 EQ.0: Data check EQ.1: Execution EQ.2: restart Ratio of allocated memory . . . . . (RMEST) =0.200 Coordinate system . . . . . . . . . (JCORD) = 0 EQ.0: Cartesian coordinate EQ.1: Cylindrical coordinate Printout flag . . . . . . . . . . . (IPSF ) = 3 Current level of time step reduction(Klevel) = 2 Total number of time steps . . . . (NSTE) = 54 Time step increment . . . . . . . . (DT) = 0.1250E-01 Time at solution start . . . . . (TSTART) = 0.6500E+00 Printing interval . . . . . . . . . (IPRI) = 1 Version number . . . . . . . . . . (VERSION) = 2014.000 ** Analysis information Analysis type . . . . . . . . . . . (IMASS) = 0 EQ.0: Static analysis EQ.1: Dynamic analysis/Frequency analysis with lumped mass EQ.2: Dynamic analysis/Frequency analysis with consistent mass Nonlinearity code . . . . . . . . . (KLIN) = 1 EQ.0: Linear analysis (NEGNL=0) EQ.1: Nonlinear analysis (NEGNL >= 1) ** Iteration Control for Nonlinear Element Number of time steps between reforming effective stiffness matrix . . . (ISREF) = 1 Maximum number of stiffness reformations permitted in each time step . . (NUMREF) = 15 Number of time steps between equilibrium iterations . . . . . (IEQUIT) = 1 Maximum number of equilibrium iterations permitted . . . . . . (ITEMAX) = 15 Displacement convergence tolerance (DTOL) = 0.100E-03 Force convergence tolerance . . . . (FTOL) = 0.100E-14 Energy convergence tolerance . . (DTOL*FTOL) = 0.100E-18 Line search tolerance . . . . . . . (STOL) = 0.500E+00 Contact wall tolerance . . . . . . .(CTOL) = 0.100E-01 Nonlinear iterative solution method (IMETHD) = 5 EQ.0: Modified Newton method EQ.1: Full Newton method EQ.2: Combined full-modified Newton method EQ.3: Modified Newton method with line search EQ.4: Full Newton method with line search EQ.5: Combined full-modified Newton method with line search EQ.6: Full Newton method (Riks) EQ.7: Full Newton method with updated line search Convergence criteria code for equilibrium iterations . . . . . . . . . . . . . . . . . (ICRITE) = 0 EQ.0: Displacement only EQ.1: Energy only EQ.2: Force only (reserved) EQ.3: Displacement or energy EQ.4: Displacement or force (reserved) EQ.5: Displacement and energy (reserved) EQ.6: Displacement and force (reserved) Convergence based on code for equilibrium iterations . . . . . . . . . . . . . . . . . (methodEQ) = 1 EQ.0: Total displacement EQ.1: Displacement since last time step EQ.2: Displacement of the first iteration Matrix reform interval within each time step . . . . . . . . . . . . . . . . . (MREFIN) = 1 Maximum number of stiffness reformations permitted in each matrix reform interval . . . (MREFNU) = 15 Damping matrix code . . . . . . . . (IDAMP) = 0 EQ.0: No Rayleigh damping EQ.1: Rayleigh damping Number of nodal masses . . . . . . (IMASSN) = 0 Number of nodal dampers . . . . . . (IDAMPN) = 0 ** Element Loading Information Mass proportional loading index . (IMASLD) = 0 EQ.0 : No mass proportional loads EQ.1 : Mass proportional loads : Gravity, centrifugal loads, or any mass proportional body loads Thermal loading index . . . . . (ITHERM) = 0 Electric potential loading index (Ipiezo) = 0 ** General Loading Information Number of spatial orientation points . . . . . . . . . . . . . . . . . . . (NTRAPT) = 1 Number of 2D deformation independent traction/pressure faces/elements (dead load) . . . . . (NTR2DC) = 0 Number of 3D deformation independent traction/pressure faces/elements (dead load) . . . . . (NTR3DC) = 0 Number of 2D deformation dependent traction/pressure faces/elements (follower load). . . . (NTR2DF) = 0 Number of 3D deformation dependent traction/pressure faces/elements (follower load). . . . (NTR3DF) = 0 Number of gravity and/or constant acceleration cases . . . . . . . . . . . . . . . . (MASCON) = 0 Number of centrifugal load cases (MASCEN) = 0 Number of constraint equation parts . . (NCEqGp) = 0 Number of total constraint equations. . (NConEq) = 0 Number of prescribed displacements . . . . . . . . . . . . . . . . (NPRDIS) = 0 Maximum number of constraint active intervals . . . . . . . . . . . . . . . . (MACTIM) = 0 ** Displacement/Velocity/Acceleration Printout Code Number of blocks of nodal printout . . (NPB) = 0 Displacement printout code . . . . . . (IDC) = 0 EQ.0: No printout EQ.1: Printout ** Nodal point data suppressed (use /PRNOD to print) Number of equations . . . . . . . . (NEQ) = 371514 ** Applied Loading Information Number of nodal loads . . . . . . . . (NLOAD) = 0 Number of load curves . . . . . . . . (NLCUR) = 1 Max number of points in load curves . (NPTM) = 2 Load function number = 1 Number of time points = 2 Time Magnitude ------------ --------------- 0.00000E+00 0.0000000E+00 1.00000E+00 1.0000000E+00 ** Spatial Orientation Point Coordinates Point No. X Y Z ------------------------------------------------------- 1 0.00000E+00 0.00000E+00 0.00000E+00 ** Shell element 6-DOF nodes Node list 2 3 7 8 151 152 553 554 697 698 699 700 701 702 703 704 705 706 707 708 709 710 711 712 713 714 715 716 717 718 719 720 721 722 723 724 725 726 727 728 729 730 731 732 733 734 735 736 737 738 739 740 741 742 743 744 745 746 747 748 749 750 751 752 753 754 755 756 757 758 759 760 761 762 763 764 765 766 767 768 769 770 771 772 773 774 775 776 777 778 779 780 781 782 783 784 785 786 787 788 789 790 791 792 793 794 795 796 797 798 799 800 801 802 803 804 805 806 807 808 1489 1490 1491 1492 1493 1494 1495 1496 1497 1498 1499 1500 1501 1502 1503 1504 1505 1506 1507 1508 1509 1510 1511 1512 1513 1514 1515 1516 1517 1518 1519 1520 1521 1522 1523 1524 1525 1526 1527 1528 1529 1530 1531 1532 1533 1534 1535 1536 1537 1538 1539 1540 1541 1542 1543 1544 1545 1546 1547 1548 1549 1550 1551 1552 1553 1554 1555 1556 1557 1558 1559 1560 1561 1562 1563 1564 1565 1566 1567 1568 1569 1570 1571 1572 1573 1574 1575 1576 1577 1578 1579 1580 1581 1582 1583 1584 1585 1586 1587 1588 1589 1590 1591 1592 1593 1594 1595 1596 1597 1598 1599 1600 17939 17941 18367 18908 19342 19345 19909 19910 19911 19912 19913 19914 19915 19916 19917 19918 19919 19920 19921 19922 19923 19924 19925 19926 19927 19928 19929 19930 19931 19932 19933 19934 19935 19936 19937 19938 19939 19940 19941 19942 19943 19944 19945 19946 19947 19948 19949 19950 19951 19952 19953 19954 19955 19956 19957 19958 19959 19960 19961 19962 19963 19964 19965 19966 19967 19968 19969 19970 19971 19972 19973 19974 19975 19976 19977 19978 19979 19980 19981 19982 19983 19984 19985 19986 19987 19988 19989 19990 19991 19992 19993 19994 19995 19996 19997 19998 19999 20000 20001 20002 20003 20004 20005 20006 20007 20008 20009 20010 20011 20012 20013 20014 20015 20016 20017 20018 20019 20020 20021 20022 20023 20024 20025 20026 20027 20028 20029 20030 20031 20032 20033 20034 20035 20036 20037 20038 20039 20040 20041 20042 20043 20044 20045 20046 20047 20048 20049 20050 20051 20052 20053 20054 20055 20056 20057 20058 20059 20060 20061 20062 20063 20064 20065 20066 20067 20068 20069 20070 20071 20072 20073 20074 20075 20076 20077 20078 20079 20080 20081 20082 20083 20084 20085 20086 20087 20088 20089 20090 20091 20092 20093 20094 20095 20096 20097 20098 20099 20100 20101 20102 20103 20104 20105 20106 20107 20108 20109 20110 20111 20112 20113 20114 20115 20116 20117 20118 20119 20120 20121 20122 20123 20124 20125 20126 20127 20128 20129 20130 20131 20132 20133 20134 20135 20136 20137 20138 20139 20140 20141 20142 20143 20144 20145 20146 20147 20148 20149 20150 20151 20152 20153 20154 20155 20156 20157 20158 20159 20160 20161 20162 20163 20164 20165 20166 20167 20168 20169 20170 20171 20172 20173 20174 20175 20176 20177 20178 20179 20180 20181 20182 20183 20184 20185 20186 20187 20188 20189 20190 20191 20192 20193 20194 20195 20196 20197 20198 20199 20200 20201 20202 20203 20204 20205 20206 20207 20208 20209 20210 20211 20212 20213 20214 20215 20216 20217 20218 20219 20220 20221 20222 20223 20224 20225 20226 20227 20228 20229 20230 20231 20232 20233 20234 20235 20236 20237 20238 20239 20240 20241 20242 20243 20244 20245 20246 20247 20248 20249 20250 20251 20252 20253 20254 20255 20256 20257 20258 20259 20260 20261 20262 20263 20264 20265 20266 20267 20268 20269 20270 20271 20272 20273 20274 20275 20276 20277 20278 20279 20280 20281 20282 20283 20284 20285 20286 20287 20288 20289 20290 20291 20292 20293 20294 20295 20296 20297 20298 20299 20300 20301 20302 20303 20304 ** Input initial conditions Initial conditions code . . . . . . . (ICON) = 0 EQ.0: Zero initial conditions EQ.1: Initial conditions are read EQ.2: Initial conditions are read from .PIN file EQ.3: Initial conditions are read from .INI file (but MODEX.eq.2 over-rides ICON) ** Element Part Data Element part number (Nonlinear) . . . . . . . = 1 3-D continuum element definition (Type 25) Number of elements . . . . . . . . (NPAR(2)) = 24453 Type of nonlinear element analysis (NPAR(3)) = 2 EQ.1: Material nonlinearity only EQ.2: Total Lagrangian formulation EQ.3: Updated Lagrangian formulation Type of element formulation (NPAR(4)) = 1 EQ.0: With incompatible mode (8-noded brick only) EQ.1: Without incompatible mode Number of diff. sets of element traction/pressure loads (NPAR(6)) = 171 Max no. of nodes defining one element NPAR(7) = 20 Number of material axis sets for orthotropic material model (Model 2 or 7) . . . . . . . (NPAR(8)) = 1 EQ.0 : Material axes Ea, Eb, and Ec coincide with global (x,y,z) coordinate axes Integration order (r-s direction) for element stiffness generation . . . . . . (NPAR(10)) = 3 Integration order (t direction) for element stiffness generation . . . . . . (NPAR(11)) = 3 Number of stress output tables . .(NPAR(13)) = 0 EQ.0: Print at integration points 3-D continuum material definition Material model . . . . . . . . . . (NPAR(15)) = 4 EQ.1: Linear elastic isotropic EQ.2: Linear elastic orthotropic EQ.3: Nonlinear curve description model EQ.4: von Mises elasto-plastic - isotropic hardening EQ.5: von Mises elasto-plastic - kinematic hardening EQ.6: Thermoelastic model EQ.7: Linear thermal elastic orthotropic EQ.8: Nearly incompressible hyperelastic (Mooney-Rivlin) EQ.9: Nearly incompressible hyperelastic (Ogden) EQ.10: Thermal elasto-plastic - isotropic hardening EQ.11: Thermal elasto-plastic - kinematic hardening EQ.12: Thermal elastic creep model EQ.13: Thermal elastic creep model (simple) EQ.14: Thermal elasto-plastic creep (ORNL) - isotropic EQ.15: Thermal elasto-plastic creep (ORNL) - kinematic EQ.16 Plastic model (Drucker-Prager) EQ.17: Elasto-plastic Multilinear Isotropic Model EQ.18: Elasto-plastic Multilinear Kinematic Model EQ.19: Piezo-electric Model - special EQ.20: Piezo-electric Model - generalized EQ.21: Highly compressible Hyperfoam Model (Ogden Foam) EQ.22: Nearly incompressible hyperelastic (Blatz-Ko) EQ.23: Nearly incompressible hyperelastic (Neo-Hookean, N/A) EQ.24: Nearly incompressible hyperelastic (Yeoh) EQ.25: nearly incompressible hyperelastic (Arruda-Boyce) EQ.26: Nearly incompressible hyperelastic (Van der Waals, N/A) EQ.28: Reinforced concrete EQ.29: Duncan-Chang soil model EQ.30: Modflow MSA models EQ.101:Linear viscoelastic isotropic EQ.102:Linear viscoelastic orthotropic EQ.103:Linear thermal viscoelastic isotropic EQ.104:Linear thermal viscoelastic orthotropic EQ.105:Viscoelastic Mooney-Rivlin EQ.106:Viscoelastic Ogden EQ.107:Viscoelastic Ogden foam EQ.108:Viscoelastic Arruda-Boyce EQ.109:Viscoelastic Blatz-Ko EQ.110:Viscoelastic Neo-Hookean EQ.111:Viscoelastic Yeoh EQ.112:Viscoelastic van der Waals No of diff. sets of material const.(NPAR(16)) = 1 No of material constants per set . (NPAR(17)) = 4 Array (WA) per integration point . (NPAR(18)) = 24 Material constants set number ................ = 1 DEN (DENSITY) . . . . . . . . = 0.700000E-08 Young's Modulus (E). . . . . . = 0.2100E+06 Poisson's Ratio (Nu) . . . . . = 0.3000E+00 Initial Yield Stress (Ey) . . = 0.2350E+03 Stress Hardening Parameter (Et)= 0.2000E+03 ** 3-D continuum element data suppressed (use /PRELE to print) ** Solution State Parameters (2) ** mTOT,maxSizeA,mUSE,mFRE(8 Bytes) == 0, 18642501, 0, 0 ** mGK(%) (doubles) == 0 ( 0.0000% of Physical Memory) ** iSPARSE,iPACK,iCHOP,kLIN,iSTAT,iMASS == 8,0,0,1,0,0 ** maxK,kLEVEL,nrestart,kSTEP,kEXIT,iRUN == 2,2,1,2,27,0 ** n_step,n_case,nste_ext,totalT,dt0 == 26,26,0, 1.000000000000000E+00, 2.500000000000000E-02 ** Initial condition list (in node#) suppressed (use /PRINI to print) ** Job started : 2014-03-28 09:28:25 ** Job finished : 2014-03-28 11:02:04 ** Total elapsed time : 1:32:38 (hours:minutes:seconds)
Thanks for your help.
Thomas
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