Copyright Autodesk, Inc. All rights reserved. (C)2009 2010 2011 2012 2013 Portions of this software are covered by U.S. Patent Numbers 5,287,408 and 6,096,088. Coupled 3D Flow Solver. Version: ami2014-cerium_compile_windows-x64 (Build 13213-374) 64-bit build Analysis running on host: ALJIES64-47 Operating System: Windows 7 Service Pack 1 Processor type: GenuineIntel Intel64 Family 6 Model 44 Stepping 2 ~2664 MHz Number of Processors: 12 Total Physical Memory: 98287 MBytes Analysis commenced at Fri Oct 25 17:38:39 2013 Mesh and boundary conditions file name : 3xx_c301311239_p00_63_rim_no_r02.udm Results files core name : 3xx_c301311239_p00_63_rim_no_r02~2 Core shift calculation : ON -------------------------------------------------------------------------- Solver Parameters: ================= Solver setup: ------------ Solver = Coupled 3D Solution type = Stokes Simulate inertia effect = No Simulate gravity effect = No Gate diameter at cavity injection locations = Specified as 2.000 mm Filling parameters: ------------------ Maximum %volume to fill per time step = 4.000 % Maximum iterations per time step = 50 Convergence tolerance (scaling factor) = 1.000 Flow front scheme = Level set Packing parameters: ------------------ Maximum time step = 2.000 s Maximum iterations per time step = 50 Convergence tolerance (scaling factor) = 1.000 Intermediate results: -------------------- Intermediate results type = Write at constant intervals Number of intermediate results in filling phase = 5 Number of intermediate results in packing phase = 5 Number of intermediate results in cooling phase = 3 -------------------------------------------------------------------------- Material Data: ============= Manufacturer DSM Trade name Arnite AV2 390 XT Family name PET Specific heat: Tabulated data: Temperature Specific Heat T (K) Cp (J/kg-K) ----------- ------------- 328.1500 1150.0000 336.1500 1212.0000 351.1500 1298.0000 373.1500 1388.0000 416.1500 1501.0000 439.1500 1576.0000 454.1500 1683.0000 460.1500 1825.0000 477.1500 2781.0000 484.1500 1749.0000 487.1500 1617.0000 561.1500 1694.0000 Thermal conductivity: Tabulated data: Temperature Thermal Conductivity T (K) K (W/m-K) ----------- -------------------- 369.1500 0.3970 389.1500 0.4260 429.1500 0.4200 449.1500 0.3960 468.1500 0.3920 488.1500 0.4170 508.1500 0.4080 526.1500 0.3630 546.1500 0.3540 566.1500 0.3390 Transition temperature = 212.0000 C pvT Model: 2-domain modified Tait coefficients: b5 = 529.1500 K b6 = 2.3290E-07 K/Pa Liquid phase Solid phase ------------------------------- b1m = 0.0006 b1s = 0.0006 m^3/kg b2m = 3.7350E-07 b2s = 1.0760E-07 m^3/kg-K b3m = 1.8541E+08 b3s = 4.8305E+08 Pa b4m = 0.0055 b4s = 0.0025 1/K b7 = 4.5220E-05 m^3/kg b8 = 0.0423 1/K b9 = 1.2500E-08 1/Pa Viscosity model: Cross-WLF coefficients: n = 0.3356 TAUS = 4.9258E+05 Pa D1 = 2.9295E+18 Pa-s D2 = 340.1500 K D3 = 0.0000 K/Pa A1 = 45.6600 A2T = 51.6000 K Juncture loss equation : DPe = c1 * TAUW^c2 where c1 = 3.1510 Pa^(1-c2) c2 = 1.0990 Mechanical properties data: E1 = 1.8182E+04 MPa E2 = 1.0469E+04 MPa v12 = 0.3911 v23 = 0.5002 G12 = 4624.8402 MPa Transversely isotropic coefficient of thermal expansion (CTE) data: Alpha1 = 1.3670E-05 1/C Alpha2 = 3.1320E-05 1/C Filler properties :Glass Fiber Density (rho) = 2.5400 g/cm^3 Mechanical properties data: E = 7.2000E+04 MPa v = 0.2200 Coefficient of thermal expansion (CTE) data: Alpha1 = 5.0000E-06 1/C Alpha2 = 5.0000E-06 1/C Weight = 50.0000 Aspect ratio (L/D) = 25.0000 Polymer matrix properties (decomposed from composite and fiber properties) Polymer matrix mechanical properties data: E = 3449.9942 MPa v = 0.4080 Polymer matrix coefficient of thermal expansion (CTE) data: Alpha1 = 7.0011E-05 1/C No mesh for the cores was found. Core shift analysis switched OFF -------------------------------------------------------------------------- Model Details: ============= Mesh Type = 3D Tetrahedra Tetrahedral refinement layers (specified minimum) = 12 Total number of part nodes = 564567 Number of tetrahedron nodes = 564567 Total number of injection location nodes = 3 The injection location node numbers are: 20294 47138 29651 Total number of elements = 3361102 Number of part elements = 3361102 Number of tetrahedral elements = 3361102 Total volume = 53.0792 cm^3 Volume of tetrahedral elements = 53.0792 cm^3 Volume filled initially = 0.0000 cm^3 Volume to be filled = 53.0792 cm^3 Part volume to be filled = 53.0792 cm^3 Sprue/runner/gate volume to be filled = 0.0000 cm^3 Parting plane normal (dx) = 0.0000 (dy) = 0.0000 (dz) = 1.0000 Total projected area = 75.3069 cm^2 -------------------------------------------------------------------------- Fiber orientation calculation : ON Fiber Orientation Calculation Parameters ======================================== Fiber orientation model = Folgar-Tucker Fiber interaction coefficient (Ci) = 0.0040 ** WARNING 98114 ** The material used in this analysis is a short fiber-filled material. Fiber breakage calculations are only supported for long fiber-filled materials. Continuing analysis without fiber breakage calculations. Mechanical Property Calculation Options ======================================= Micro-mechanics model option = Automatic Tandon-Weng micromechanics model is chosen for the analysis Thermal expansion coefficient model option = Rosen-Hashin Closure approximation model option = Orthotropic 3 ** WARNING 304920 ** There is insufficient refinement of the tetrahedral mesh in some areas, which may affect solution accuracy. Inspect with the "Node layer number" plot and consider improving the mesh. [For the 12 tetrahedral refinement layers requested, the node layer number is expected to reach 7 at the part centerline.] ** WARNING 304930 ** The node layer number on the part centerline is 6 or less for 90.0 percent of the part. ** WARNING 304940 ** The node layer number on the part centerline is more than one less than requested (i.e. 5 or less) for 58.0 percent of the part. -------------------------------------------------------------------------- Process Settings: ================ Machine parameters: ------------------ Maximum injection pressure = 1.8000E+02 MPa Maximum machine clamp force = 7.0002E+03 tonne Maximum machine injection rate = 5.0000E+03 cm^3/s Machine hydraulic response time = 1.0000E-02 s Temperature control: ------------------- Melt temperature = 290.00 C Mold temperature = 130.00 C Mold-melt heat transfer coefficients Global values. (Superseded by any values set on individual elements.) Filling = 5000.0000 W/m^2-C Packing = 2500.0000 W/m^2-C Detached = 1250.0000 W/m^2-C Atmospheric temperature = 25.00 C Filling Control: --------------- Filling control type = Injection time Fill time = 1.50 s Stroke volume determination = Automatic Velocity/pressure switch-over control: ------------------------------------- Velocity/pressure switch-over control type = By %volume filled Percentage volume of the part = 98.00 % Pack/holding control: -------------------- Pack/holding control type = %Filling pressure vs time Pressure profile: duration % filling pressure ----------------------------- 0.00 s 50.00 4.00 s 50.00 Cooling time: ------------ Cooling time determination = Specified Cooling time = 23.0000 s -------------------------------------------------------------------------- Matrix Solver Settings: ====================== AMG matrix solver selection = Automatic Matrix solver used = AMG Number of threads for parallelization = Specify number of threads Number of threads used in the analysis = 6 -------------------------------------------------------------------------- Filling Phase: Status: V = Velocity control ============= V/P = Velocity/pressure switch-over P = Pressure control |----------------------------------------------------------------------| | Time | Fill Vol| Inj Press | Clamp F | Flow Rate| Frozen | Status| | (s) | (%) | (MPa) | (tonne) | (cm^3/s) | Vol (%)| | |----------------------------------------------------------------------| | 0.002 | 0.012 | 4.394e-01 | 0.00e+00 | 2.952 | 0.00 | V | | 0.006 | 0.210 | 2.386e+00 | 3.80e-05 | 9.410 | 0.00 | V | | 0.015 | 0.741 | 4.429e+00 | 4.29e-04 | 21.832 | 0.00 | V | | 0.025 | 1.181 | 5.213e+00 | 8.01e-04 | 30.096 | 0.01 | V | | 0.043 | 2.405 | 5.819e+00 | 2.94e-03 | 33.318 | 0.28 | V | | 0.058 | 3.377 | 6.138e+00 | 6.22e-03 | 34.421 | 0.56 | V | | 0.080 | 4.861 | 6.460e+00 | 1.06e-02 | 34.749 | 1.15 | V | | 0.096 | 5.925 | 6.610e+00 | 1.30e-02 | 34.983 | 1.53 | V | | 0.125 | 7.852 | 6.783e+00 | 1.62e-02 | 35.128 | 2.00 | V | | 0.148 | 9.375 | 6.915e+00 | 1.88e-02 | 35.191 | 2.30 | V | | 0.199 | 12.724 | 7.100e+00 | 2.59e-02 | 35.231 | 2.86 | V | | 0.229 | 14.707 | 7.240e+00 | 3.01e-02 | 35.254 | 3.25 | V | | 0.276 | 17.821 | 7.371e+00 | 4.08e-02 | 35.270 | 3.80 | V | | 0.305 | 19.680 | 7.516e+00 | 4.99e-02 | 35.267 | 4.20 | V | | 0.341 | 22.072 | 7.639e+00 | 6.14e-02 | 35.261 | 4.69 | V | | 0.377 | 24.441 | 7.754e+00 | 7.35e-02 | 35.291 | 5.12 | V | | 0.424 | 27.491 | 7.878e+00 | 8.96e-02 | 35.303 | 5.61 | V | | 0.466 | 30.231 | 8.045e+00 | 1.14e-01 | 35.295 | 6.09 | V | | 0.502 | 32.580 | 8.185e+00 | 1.34e-01 | 35.282 | 6.54 | V | | 0.548 | 35.581 | 8.439e+00 | 1.90e-01 | 35.265 | 7.07 | V | | 0.580 | 37.618 | 8.628e+00 | 2.23e-01 | 35.243 | 7.48 | V | | 0.628 | 40.734 | 8.825e+00 | 2.65e-01 | 35.264 | 8.04 | V | | 0.652 | 42.279 | 8.982e+00 | 2.91e-01 | 35.263 | 8.34 | V | | 0.695 | 45.103 | 9.156e+00 | 3.39e-01 | 35.268 | 8.79 | V | | 0.719 | 46.622 | 9.287e+00 | 3.70e-01 | 35.282 | 9.03 | V | | 0.746 | 48.353 | 9.408e+00 | 4.05e-01 | 35.280 | 9.31 | V | | 0.766 | 49.640 | 9.511e+00 | 4.33e-01 | 35.286 | 9.50 | V | | 0.797 | 51.642 | 9.635e+00 | 4.80e-01 | 35.293 | 9.77 | V | | 0.826 | 53.527 | 9.830e+00 | 5.42e-01 | 35.280 | 10.03 | V | | 0.858 | 55.565 | 1.004e+01 | 6.31e-01 | 35.259 | 10.34 | V | | 0.881 | 57.061 | 1.020e+01 | 6.89e-01 | 35.262 | 10.56 | V | | 0.915 | 59.214 | 1.102e+01 | 1.11e+00 | 35.105 | 10.83 | V | | 0.932 | 60.239 | 1.123e+01 | 1.17e+00 | 35.064 | 10.97 | V | | 0.965 | 62.428 | 1.156e+01 | 1.33e+00 | 35.199 | 11.24 | V | | 0.981 | 63.418 | 1.174e+01 | 1.41e+00 | 35.215 | 11.39 | V | | 1.009 | 65.236 | 1.193e+01 | 1.50e+00 | 35.244 | 11.65 | V | | 1.028 | 66.413 | 1.208e+01 | 1.56e+00 | 35.272 | 11.82 | V | | 1.055 | 68.223 | 1.225e+01 | 1.65e+00 | 35.282 | 12.06 | V | | 1.082 | 69.950 | 1.246e+01 | 1.76e+00 | 35.285 | 12.26 | V | | 1.115 | 72.032 | 1.323e+01 | 2.27e+00 | 35.168 | 12.54 | V | | 1.127 | 72.722 | 1.348e+01 | 2.38e+00 | 35.089 | 12.64 | V | | 1.150 | 74.259 | 1.366e+01 | 2.51e+00 | 35.200 | 12.82 | V | | 1.183 | 76.350 | 1.418e+01 | 2.88e+00 | 35.236 | 13.03 | V | | 1.209 | 77.916 | 1.645e+01 | 4.69e+00 | 34.789 | 13.22 | V | | 1.238 | 79.705 | 1.721e+01 | 5.14e+00 | 34.743 | 13.36 | V | | 1.255 | 80.785 | 1.744e+01 | 5.27e+00 | 35.168 | 13.43 | V | | 1.275 | 82.087 | 1.776e+01 | 5.48e+00 | 35.232 | 13.57 | V | | 1.286 | 82.740 | 1.793e+01 | 5.58e+00 | 35.227 | 13.64 | V | | 1.303 | 83.894 | 1.822e+01 | 5.79e+00 | 35.230 | 13.76 | V | | 1.312 | 84.447 | 1.841e+01 | 5.90e+00 | 35.212 | 13.82 | V | | 1.325 | 85.223 | 1.877e+01 | 6.14e+00 | 35.155 | 13.91 | V | | 1.337 | 85.988 | 1.925e+01 | 6.46e+00 | 35.082 | 13.99 | V | | 1.346 | 86.540 | 1.965e+01 | 6.74e+00 | 35.023 | 14.05 | V | | 1.357 | 87.262 | 2.007e+01 | 7.00e+00 | 35.042 | 14.13 | V | | 1.367 | 87.881 | 2.040e+01 | 7.23e+00 | 35.095 | 14.19 | V | | 1.377 | 88.522 | 2.075e+01 | 7.46e+00 | 35.111 | 14.26 | V | | 1.386 | 89.073 | 2.117e+01 | 7.76e+00 | 35.071 | 14.30 | V | | 1.394 | 89.537 | 2.191e+01 | 8.34e+00 | 34.850 | 14.34 | V | | 1.400 | 89.904 | 2.253e+01 | 8.73e+00 | 34.667 | 14.38 | V | | 1.409 | 90.443 | 2.312e+01 | 9.14e+00 | 34.777 | 14.44 | V | | 1.421 | 91.165 | 2.380e+01 | 9.59e+00 | 34.933 | 14.51 | V | | 1.426 | 91.472 | 2.417e+01 | 9.83e+00 | 34.936 | 14.54 | V | | 1.439 | 92.282 | 2.532e+01 | 1.07e+01 | 34.853 | 14.63 | V | | 1.449 | 92.898 | 2.598e+01 | 1.11e+01 | 34.886 | 14.67 | V | | 1.467 | 94.014 | 2.664e+01 | 1.16e+01 | 35.058 | 14.76 | V | | 1.482 | 94.968 | 2.727e+01 | 1.20e+01 | 35.145 | 14.83 | V | | 1.487 | 95.290 | 2.752e+01 | 1.22e+01 | 35.133 | 14.85 | V | | 1.501 | 96.131 | 2.802e+01 | 1.26e+01 | 35.150 | 14.93 | V | | 1.508 | 96.581 | 2.836e+01 | 1.28e+01 | 35.159 | 14.97 | V | | 1.518 | 97.203 | 2.871e+01 | 1.31e+01 | 35.174 | 15.02 | V | | 1.526 | 97.712 | 2.904e+01 | 1.34e+01 | 35.194 | 15.07 | V | Specified volume filled under velocity control. Switching to pressure control. | 1.531 | 98.005 | 2.929e+01 | 1.36e+01 | 35.162 | 15.09 | V/P | | 1.539 | 98.564 | 1.710e+01 | 9.81e+00 | 21.417 | 15.16 | P | | 1.541 | 98.638 | 1.464e+01 | 8.63e+00 | 6.361 | 15.33 | P | | 1.552 | 98.755 | 1.464e+01 | 7.30e+00 | 8.327 | 15.62 | P | | 1.578 | 99.335 | 1.464e+01 | 7.13e+00 | 12.115 | 16.14 | P | | 1.583 | 99.435 | 1.464e+01 | 7.43e+00 | 12.212 | 16.22 | P | | 1.592 | 99.640 | 1.464e+01 | 7.80e+00 | 11.147 | 16.38 | P | | 1.596 | 99.731 | 1.464e+01 | 7.96e+00 | 10.152 | 16.46 | P | | 1.603 | 99.856 | 1.464e+01 | 8.16e+00 | 9.466 | 16.58 | P | | 1.609 | 99.958 | 1.464e+01 | 8.35e+00 | 8.781 | 16.69 | P | | 1.613 | 100.000 | 1.464e+01 | 9.01e+00 | 7.625 | 16.78 | Filled| |----------------------------------------------------------------------| End of filling phase results summary : Current time from start of cycle = 1.6135 s Total mass = 86.5360 g Frozen volume = 16.7798 % Injection pressure = 14.6440 MPa Maximum Clamp force - during filling = 13.5597 tonne Time at velocity/pressure switch-over = 1.5308 s Injection pressure at velocity/pressure switch-over= 29.2880 MPa Volume filled at velocity/pressure switch-over = 98.0048 % End of filling. Packing will now commence. Pack Analysis |----------------------------------------------------------------------| | Time | Packing | Inj Press | Clamp F | Part Mass| Frozen | Status| | (s) | (%) | (MPa) | (tonne) | (g) | Vol (%)| | |----------------------------------------------------------------------| | 1.617 | 0.01 | 1.464e+01 | 9.22e+00 | 8.65e+01 | 16.79 | P | | 1.624 | 0.04 | 1.464e+01 | 9.45e+00 | 8.65e+01 | 16.85 | P | | 1.644 | 0.11 | 1.464e+01 | 9.81e+00 | 8.66e+01 | 17.03 | P | | 1.701 | 0.33 | 1.464e+01 | 1.01e+01 | 8.67e+01 | 17.67 | P | | 1.817 | 0.76 | 1.464e+01 | 1.01e+01 | 8.69e+01 | 19.19 | P | | 2.196 | 2.16 | 1.464e+01 | 9.74e+00 | 8.75e+01 | 24.49 | P | | 2.554 | 3.49 | 1.464e+01 | 9.26e+00 | 8.80e+01 | 29.75 | P | | 2.894 | 4.76 | 1.464e+01 | 7.58e+00 | 8.84e+01 | 34.98 | P | | 3.082 | 5.45 | 1.464e+01 | 4.86e+00 | 8.85e+01 | 38.13 | P | | 3.153 | 5.72 | 1.464e+01 | 2.84e+00 | 8.85e+01 | 39.54 | P | | 3.187 | 5.85 | 1.464e+01 | 1.64e+00 | 8.85e+01 | 40.30 | P | | 3.214 | 5.95 | 1.464e+01 | 7.41e-01 | 8.85e+01 | 40.86 | P | | 3.321 | 6.34 | 1.464e+01 | 6.40e-03 | 8.85e+01 | 42.75 | P | | 3.604 | 7.40 | 1.464e+01 | 3.86e-04 | 8.85e+01 | 46.54 | P | | 3.977 | 8.78 | 1.464e+01 | 1.27e-04 | 8.85e+01 | 51.16 | P | | 4.381 | 10.28 | 1.464e+01 | 8.76e-05 | 8.85e+01 | 56.18 | P | | 4.784 | 11.78 | 1.464e+01 | 4.21e-06 | 8.85e+01 | 61.27 | P | | 5.178 | 13.24 | 1.464e+01 | 2.62e-06 | 8.85e+01 | 66.25 | P | | 5.531 | 14.55 | 1.464e+01 | 2.62e-06 | 8.85e+01 | 70.45 | P | | 5.533 | 14.56 | 1.172e+01 | 0.00e+00 | 8.85e+01 | 70.48 | P | | 5.541 | 14.59 | 0.000e+00 | 0.00e+00 | 8.85e+01 | 70.56 | P | | 5.573 | 14.71 | 0.000e+00 | 0.00e+00 | 8.85e+01 | 70.92 | P | | 5.701 | 15.18 | 0.000e+00 | 0.00e+00 | 8.85e+01 | 72.37 | P | | 6.101 | 16.67 | 0.000e+00 | 0.00e+00 | 8.85e+01 | 76.58 | P | | 6.577 | 18.44 | 0.000e+00 | 0.00e+00 | 8.85e+01 | 80.83 | P | | 7.137 | 20.52 | 0.000e+00 | 0.00e+00 | 8.85e+01 | 85.07 | P | | 7.797 | 22.97 | 0.000e+00 | 0.00e+00 | 8.85e+01 | 89.15 | P | | 8.605 | 25.98 | 0.000e+00 | 0.00e+00 | 8.85e+01 | 92.67 | P | | 9.534 | 29.43 | 0.000e+00 | 0.00e+00 | 8.85e+01 | 95.24 | P | | 10.517 | 33.08 | 0.000e+00 | 0.00e+00 | 8.85e+01 | 96.86 | P | | 11.352 | 36.18 | 0.000e+00 | 0.00e+00 | 8.85e+01 | 97.73 | P | | 12.072 | 38.85 | 0.000e+00 | 0.00e+00 | 8.85e+01 | 98.27 | P | | 12.595 | 40.80 | 0.000e+00 | 0.00e+00 | 8.85e+01 | 98.55 | P | | 13.165 | 42.92 | 0.000e+00 | 0.00e+00 | 8.85e+01 | 98.79 | P | | 13.842 | 45.43 | 0.000e+00 | 0.00e+00 | 8.85e+01 | 99.02 | P | | 15.842 | 52.86 | 0.000e+00 | 0.00e+00 | 8.85e+01 | 99.51 | P | | 17.842 | 60.29 | 0.000e+00 | 0.00e+00 | 8.85e+01 | 99.79 | P | | 18.981 | 64.52 | 0.000e+00 | 0.00e+00 | 8.85e+01 | 99.87 | P | | 20.392 | 69.76 | 0.000e+00 | 0.00e+00 | 8.85e+01 | 99.93 | P | | 22.392 | 77.19 | 0.000e+00 | 0.00e+00 | 8.85e+01 | 99.97 | P | | 24.392 | 84.62 | 0.000e+00 | 0.00e+00 | 8.85e+01 | 100.00 | P | | 26.392 | 92.05 | 0.000e+00 | 0.00e+00 | 8.85e+01 | 100.00 | P | | 28.103 | 98.41 | 0.000e+00 | 0.00e+00 | 8.85e+01 | 100.00 | P | | 28.531 | 100.00 | 0.000e+00 | 0.00e+00 | 8.85e+01 | 100.00 | P | |----------------------------------------------------------------------| End of packing phase results summary : Current time from start of cycle = 28.5308 s Total mass = 88.5051 g Frozen volume = 100.0000 % Injection pressure = 0.0000 MPa Volumetric shrinkage - maximum = 13.1166 % Volumetric shrinkage - minimum = 1.8660 % Volumetric shrinkage - average = 6.6166 % Volumetric shrinkage - root-mean-square deviation = 3.4353 % Sink Mark Analysis Sink Mark Analysis completed Beginning weld line/air trap analysis... Preparing output data... Finished preparing output data Weld line/air trap analysis completed Execution time Analysis commenced at Fri Oct 25 17:38:39 2013 Analysis completed at Fri Oct 25 22:05:53 2013 CPU time used 63446.06 s equivalent to 17 hr, 37 min Elapsed wall clock time 16034.00 s equivalent to 4 hr, 27 min Copyright Autodesk, Inc. All rights reserved. (C)2009 2010 2011 2012 2013 Portions of this software are covered by U.S. Patent Numbers 5,287,408 and 6,096,088. Warp Analysis Version: ami2014-cerium_compile_windows-x64 (Build 13095-314) 64-bit build Analysis running on host: ALJIES64-47 Operating System: Windows 7 Service Pack 1 Processor type: GenuineIntel Intel64 Family 6 Model 44 Stepping 2 ~2664 MHz Number of Processors: 12 Total Physical Memory: 98287 MBytes Analysis commenced at Fri Oct 25 22:06:07 2013 Model file name: 3xx_c301311239_p00_63_rim_no_r02.udm Reading solver parameters... Reading mechanical property and shrinkage data... Generic shrinkage model is used. Read input tetra mesh: Total number of nodes: 564567 tetras: 3361102 ** WARNING 201412 ** The mesh aggregation option is used in the analysis. This option is recommended for typical thin-walled parts, but should not be used for chunky parts. Warp Analysis using a 2-layer aggregated 2nd-order tetrahedral mesh. Number of vertex nodes: 184203 Number of midside nodes: 1260537 Total number of nodes in Warp analysis: 1444740 Total number of elements in Warp analysis: 1029606 Estimated memory requirement: 5760 Mbytes. Mapping shrinkage and material property data... Defining anchor plane... Number of separate cavities = 1 Writing input file for structural analysis program... Launching structural analysis program... Reading structural analysis input file... ...finished reading structural analysis input file. Matrix solver used = AMG Number of threads for parallelization = Specify number of threads Number of threads used in the analysis = 6 Beginning load incrementation loop... Setting structure information... Assembling stiffness matrix... Solving finite element static equilibrium equations... -------------------------------------------------------- Kstep Kstra Nref Nite Node Ipos Rfac Displacement -------------------------------------------------------- 1 1 1 0 2675 1 1.000e+00 2.082e+00 Elapsed wall clock time in structural analysis: 864.52 secs. Read input tetra mesh: Total number of nodes: 564567 tetras: 3361102 Mapping warpage result... Minimum/maximum displacements at last step (unit: mm): Node Min. Node Max. ----------------------------------------------------- Trans-X 41025 -8.3183e-01 2675 1.3525e+00 Trans-Y 25978 -8.0151e-01 20336 6.5572e-01 Trans-Z 40934 -4.7962e-01 1563 5.0673e-01 ----------------------------------------------------- Writing result file... Execution time Analysis commenced at Fri Oct 25 22:15:32 2013 Analysis completed at Fri Oct 25 22:32:33 2013 CPU time used 3762.17 s Elapsed wall clock time 1021.00 s equivalent to 0 hr, 17 min Warp analysis has completed successfully.