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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
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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