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📄 testa_pbar5.out

📁 matlab实例
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                              < M A T L A B >
                  Copyright 1984-2002 The MathWorks, Inc.
                      Version 6.5.0.180913a Release 13
                                Jun 18 2002

  Using Toolbox Path Cache.  Type "help toolbox_path_cache" for more info.
 
  To get started, type one of these: helpwin, helpdesk, or demo.
  For product information, visit www.mathworks.com.
 
*********************************************************************
* FEMjr v 2.0 - Finite Element Method junior - An FEM framework     *
*********************************************************************
Enter name of input data file: 
inputfile =

testa_pbar5.dat


<<<<---- Data File Echo ---->>>>

TITLE - Four bars in series; applied loads and displ's. Same as testa but using equivalent bars.
NODES - # of nodes: 17; # of dimensions: 1
  #      ID                x                 y              z
  1      1                 1
  2      2                 2
  3      3                 3
  4      4                 4
  5      5                 5
  6      6              1.25
  7      7               1.5
  8      8              1.75
  9      9              2.25
 10     10               2.5
 11     11              2.75
 12     12              3.25
 13     13               3.5
 14     14              3.75
 15     15              4.25
 16     16               4.5
 17     17              4.75
ELEMENTS - # of elements: 4
  #     ID   elemType   propID   connectivity
 17     1    pBar5        1        1        6        7        8        2
 17     2    pBar5        2        2        9       10       11        3
 17     3    pBar5        3        3       12       13       14        4
 17     4    pBar5        4        4       15       16       17        5
PROPERTIES - # of properties: 4
  #   ID     propType         properties
  1    1    MatpBar            25             1             0             0
  2    2    MatpBar            20             1             0             0
  3    3    MatpBar            40             1             0             0
  4    4    MatpBar            10             1             0             0
CONSTRAINTS - # of constraints: 2
  #       nodeID    dof     value
  1         2         1            0.2
  2         5         1              0
LOADS - # of loads: 3
  #       nodeID    dof     value
  1         1         1              2
  2         3         1             -3
  3         4         1             -1

ke =

  130.2910 -181.1640   80.6349  -38.9418    9.1799
 -181.1640  440.2116 -375.8730  155.7672  -38.9418
   80.6349 -375.8730  590.4762 -375.8730   80.6349
  -38.9418  155.7672 -375.8730  440.2116 -181.1640
    9.1799  -38.9418   80.6349 -181.1640  130.2910


fe =

     0
     0
     0
     0
     0


ke =

  104.2328 -144.9312   64.5079  -31.1534    7.3439
 -144.9312  352.1693 -300.6984  124.6138  -31.1534
   64.5079 -300.6984  472.3810 -300.6984   64.5079
  -31.1534  124.6138 -300.6984  352.1693 -144.9312
    7.3439  -31.1534   64.5079 -144.9312  104.2328


fe =

     0
     0
     0
     0
     0


ke =

  208.4656 -289.8624  129.0159  -62.3069   14.6878
 -289.8624  704.3386 -601.3968  249.2275  -62.3069
  129.0159 -601.3968  944.7619 -601.3968  129.0159
  -62.3069  249.2275 -601.3968  704.3386 -289.8624
   14.6878  -62.3069  129.0159 -289.8624  208.4656


fe =

     0
     0
     0
     0
     0


ke =

   52.1164  -72.4656   32.2540  -15.5767    3.6720
  -72.4656  176.0847 -150.3492   62.3069  -15.5767
   32.2540 -150.3492  236.1905 -150.3492   32.2540
  -15.5767   62.3069 -150.3492  176.0847  -72.4656
    3.6720  -15.5767   32.2540  -72.4656   52.1164


fe =

     0
     0
     0
     0
     0



Stiffness Matrix and Load Vector after assembly
kglobal =

  Columns 1 through 7 

  130.2910    9.1799         0         0         0 -181.1640   80.6349
    9.1799  234.5238    7.3439         0         0  -38.9418   80.6349
         0    7.3439  312.6984   14.6878         0         0         0
         0         0   14.6878  260.5820    3.6720         0         0
         0         0         0    3.6720   52.1164         0         0
 -181.1640  -38.9418         0         0         0  440.2116 -375.8730
   80.6349   80.6349         0         0         0 -375.8730  590.4762
  -38.9418 -181.1640         0         0         0  155.7672 -375.8730
         0 -144.9312  -31.1534         0         0         0         0
         0   64.5079   64.5079         0         0         0         0
         0  -31.1534 -144.9312         0         0         0         0
         0         0 -289.8624  -62.3069         0         0         0
         0         0  129.0159  129.0159         0         0         0
         0         0  -62.3069 -289.8624         0         0         0
         0         0         0  -72.4656  -15.5767         0         0
         0         0         0   32.2540   32.2540         0         0
         0         0         0  -15.5767  -72.4656         0         0

  Columns 8 through 14 

  -38.9418         0         0         0         0         0         0
 -181.1640 -144.9312   64.5079  -31.1534         0         0         0
         0  -31.1534   64.5079 -144.9312 -289.8624  129.0159  -62.3069
         0         0         0         0  -62.3069  129.0159 -289.8624
         0         0         0         0         0         0         0
  155.7672         0         0         0         0         0         0
 -375.8730         0         0         0         0         0         0
  440.2116         0         0         0         0         0         0
         0  352.1693 -300.6984  124.6138         0         0         0
         0 -300.6984  472.3810 -300.6984         0         0         0
         0  124.6138 -300.6984  352.1693         0         0         0
         0         0         0         0  704.3386 -601.3968  249.2275
         0         0         0         0 -601.3968  944.7619 -601.3968
         0         0         0         0  249.2275 -601.3968  704.3386
         0         0         0         0         0         0         0
         0         0         0         0         0         0         0
         0         0         0         0         0         0         0

  Columns 15 through 17 

         0         0         0
         0         0         0
         0         0         0
  -72.4656   32.2540  -15.5767
  -15.5767   32.2540  -72.4656
         0         0         0
         0         0         0
         0         0         0
         0         0         0
         0         0         0
         0         0         0
         0         0         0
         0         0         0
         0         0         0
  176.0847 -150.3492   62.3069
 -150.3492  236.1905 -150.3492
   62.3069 -150.3492  176.0847


load_vector =

     0
     0
     0
     0
     0
     0
     0
     0
     0
     0
     0
     0
     0
     0
     0
     0
     0


Load Vector after assembly of point loads
load_vector =

     2
     0
    -3
    -1
     0
     0
     0
     0
     0
     0
     0
     0
     0
     0
     0
     0
     0


Constrained Stiffness Matrix and Load Vector

 Stiffness and force terms only printed for small problems

<<<<---- Solution Results ---->>>>

SOLUTION VECTOR
 dof#      value
   1           0.28
   2            0.2
   3      0.0071429
   4      -0.014286
   5              0
   6           0.26
   7           0.24
   8           0.22
   9        0.15179
  10        0.10357
  11       0.055357
  12      0.0017857
  13     -0.0035714
  14     -0.0089286
  15      -0.010714
  16     -0.0071429
  17     -0.0035714

Strain Energy (assume homogeneous displacement BCs) = 9.471667
ELEMENTAL POSTPROCESSING
  ID         f_i                 Sxx(end nodes)          energy
   1        2 -4.44e-15 -3.55e-15 -2.13e-14       -2          -2      -2       0.08

stress_nd =

   -2.0000   -2.0000   -2.0000   -2.0000   -2.0000

  ID         f_i                 Sxx(end nodes)          energy
   2     3.86 3.77e-15 -6.11e-16 -1.33e-15    -3.86       -3.86   -3.86      0.372

stress_nd =

   -3.8571   -3.8571   -3.8571   -3.8571   -3.8571

  ID         f_i                 Sxx(end nodes)          energy
   3    0.857 1.11e-16        0 -8.88e-16   -0.857      -0.857  -0.857    0.00918

stress_nd =

   -0.8571   -0.8571   -0.8571   -0.8571   -0.8571

  ID         f_i                 Sxx(end nodes)          energy
   4   -0.143 -2.5e-16 1.11e-16 -2.22e-16    0.143       0.143   0.143    0.00102

stress_nd =

    0.1429    0.1429    0.1429    0.1429    0.1429


Strain Energy = 0.462143

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