Output File for Cantilever I-beam -- Analysis with 4 groups of shell finite elements along beam length.


*** DEFINE PROBLEM SPECIFIC PARAMETERS 

*** GENERATE GRID OF GEOMETRY FOR FE MODEL 

*** GENERATE GRID OF NODES FOR FE MODEL 

*** ATTACH ELEMENTS TO GRID OF NODES 

*** DEFINE ELEMENT, SECTION AND MATERIAL PROPERTIES 

*** SET UP BOUNDARY CONDITIONS 

*** APPLY EXTERNAL LOADS 


===================================
           PROFILE                 
===================================

node    dof1    dof2    dof3    dof4    dof5    dof6
----------------------------------------------------

   1 	  -1	  -2	  -3	  -4	  -5	  -6
   2 	  -7	  -8	  -9	 -10	 -11	 -12
   3 	 -13	 -14	 -15	 -16	 -17	 -18
   4 	 -19	 -20	 -21	 -22	 -23	 -24
   5 	 -25	 -26	 -27	 -28	 -29	 -30
   6 	 -31	 -32	 -33	 -34	 -35	 -36
   7 	   1	   2	   3	   4	   5	   6
   8 	   7	   8	   9	  10	  11	  12
   9 	  13	  14	  15	  16	  17	  18
  10 	  19	  20	  21	  22	  23	  24
  11 	  25	  26	  27	  28	  29	  30
  12 	  31	  32	  33	  34	  35	  36
  13 	  37	  38	  39	  40	  41	  42
  14 	  43	  44	  45	  46	  47	  48
  15 	  49	  50	  51	  52	  53	  54
  16 	  55	  56	  57	  58	  59	  60
  17 	  61	  62	  63	  64	  65	  66
  18 	  67	  68	  69	  70	  71	  72
  19 	  73	  74	  75	  76	  77	  78
  20 	  79	  80	  81	  82	  83	  84
  21 	  85	  86	  87	  88	  89	  90
  22 	  91	  92	  93	  94	  95	  96
  23 	  97	  98	  99	 100	 101	 102
  24 	 103	 104	 105	 106	 107	 108
  25 	 109	 110	 111	 112	 113	 114
  26 	 115	 116	 117	 118	 119	 120
  27 	 121	 122	 123	 124	 125	 126
  28 	 127	 128	 129	 130	 131	 132
  29 	 133	 134	 135	 136	 137	 138
  30 	 139	 140	 141	 142	 143	 144
----------------------------------------------------


===========================================================================
Title : DESCRIPTION OF FINITE ELEMENT MESH                                 
===========================================================================

=======================
Profile of Problem Size
=======================

   Dimension of Problem        =      3

   Number Nodes                =     30
   Degrees of Freedom per node =      6
   Max No Nodes Per Element    =      4

   Number Elements             =     20
   Number Element Attributes   =      1
   Number Loaded Nodes         =      2
   Number Loaded Elements      =      0


----------------------------------------------------------------------------------------------
Node#      X_coord          Y_coord          Z_coord        Dx    Dy    Dz    Rx    Ry    Rz
----------------------------------------------------------------------------------------------

    1    0.0000e+00 in   -5.0000e+00 in    2.5000e+00 in    -1    -2    -3    -4    -5    -6 
    2    0.0000e+00 in    0.0000e+00 in    2.5000e+00 in    -7    -8    -9   -10   -11   -12 
    3    0.0000e+00 in    5.0000e+00 in    2.5000e+00 in   -13   -14   -15   -16   -17   -18 
    4    0.0000e+00 in   -5.0000e+00 in   -2.5000e+00 in   -19   -20   -21   -22   -23   -24 
    5    0.0000e+00 in    0.0000e+00 in   -2.5000e+00 in   -25   -26   -27   -28   -29   -30 
    6    0.0000e+00 in    5.0000e+00 in   -2.5000e+00 in   -31   -32   -33   -34   -35   -36 
    7    1.0000e+01 in   -5.0000e+00 in    2.5000e+00 in     1     2     3     4     5     6 
    8    1.0000e+01 in    0.0000e+00 in    2.5000e+00 in     7     8     9    10    11    12 
    9    1.0000e+01 in    5.0000e+00 in    2.5000e+00 in    13    14    15    16    17    18 
   10    1.0000e+01 in   -5.0000e+00 in   -2.5000e+00 in    19    20    21    22    23    24 
   11    1.0000e+01 in    0.0000e+00 in   -2.5000e+00 in    25    26    27    28    29    30 
   12    1.0000e+01 in    5.0000e+00 in   -2.5000e+00 in    31    32    33    34    35    36 
   13    2.0000e+01 in   -5.0000e+00 in    2.5000e+00 in    37    38    39    40    41    42 
   14    2.0000e+01 in    0.0000e+00 in    2.5000e+00 in    43    44    45    46    47    48 
   15    2.0000e+01 in    5.0000e+00 in    2.5000e+00 in    49    50    51    52    53    54 
   16    2.0000e+01 in   -5.0000e+00 in   -2.5000e+00 in    55    56    57    58    59    60 
   17    2.0000e+01 in    0.0000e+00 in   -2.5000e+00 in    61    62    63    64    65    66 
   18    2.0000e+01 in    5.0000e+00 in   -2.5000e+00 in    67    68    69    70    71    72 
   19    3.0000e+01 in   -5.0000e+00 in    2.5000e+00 in    73    74    75    76    77    78 
   20    3.0000e+01 in    0.0000e+00 in    2.5000e+00 in    79    80    81    82    83    84 
   21    3.0000e+01 in    5.0000e+00 in    2.5000e+00 in    85    86    87    88    89    90 
   22    3.0000e+01 in   -5.0000e+00 in   -2.5000e+00 in    91    92    93    94    95    96 
   23    3.0000e+01 in    0.0000e+00 in   -2.5000e+00 in    97    98    99   100   101   102 
   24    3.0000e+01 in    5.0000e+00 in   -2.5000e+00 in   103   104   105   106   107   108 
   25    4.0000e+01 in   -5.0000e+00 in    2.5000e+00 in   109   110   111   112   113   114 
   26    4.0000e+01 in    0.0000e+00 in    2.5000e+00 in   115   116   117   118   119   120 
   27    4.0000e+01 in    5.0000e+00 in    2.5000e+00 in   121   122   123   124   125   126 
   28    4.0000e+01 in   -5.0000e+00 in   -2.5000e+00 in   127   128   129   130   131   132 
   29    4.0000e+01 in    0.0000e+00 in   -2.5000e+00 in   133   134   135   136   137   138 
   30    4.0000e+01 in    5.0000e+00 in   -2.5000e+00 in   139   140   141   142   143   144 


------------------------------------------------------------------------------------------
Element#     Type         node[1]   node[2]   node[3]   node[4]      Element_Attr_Name
------------------------------------------------------------------------------------------

       1   SHELL_4NQ            1         7         8         2      name_of_elmt_attr
       2   SHELL_4NQ            2         8         9         3      name_of_elmt_attr
       3   SHELL_4NQ            5        11         8         2      name_of_elmt_attr
       4   SHELL_4NQ            4        10        11         5      name_of_elmt_attr
       5   SHELL_4NQ            5        11        12         6      name_of_elmt_attr
       6   SHELL_4NQ            7        13        14         8      name_of_elmt_attr
       7   SHELL_4NQ            8        14        15         9      name_of_elmt_attr
       8   SHELL_4NQ           11        17        14         8      name_of_elmt_attr
       9   SHELL_4NQ           10        16        17        11      name_of_elmt_attr
      10   SHELL_4NQ           11        17        18        12      name_of_elmt_attr
      11   SHELL_4NQ           13        19        20        14      name_of_elmt_attr
      12   SHELL_4NQ           14        20        21        15      name_of_elmt_attr
      13   SHELL_4NQ           17        23        20        14      name_of_elmt_attr
      14   SHELL_4NQ           16        22        23        17      name_of_elmt_attr
      15   SHELL_4NQ           17        23        24        18      name_of_elmt_attr
      16   SHELL_4NQ           19        25        26        20      name_of_elmt_attr
      17   SHELL_4NQ           20        26        27        21      name_of_elmt_attr
      18   SHELL_4NQ           23        29        26        20      name_of_elmt_attr
      19   SHELL_4NQ           22        28        29        23      name_of_elmt_attr
      20   SHELL_4NQ           23        29        30        24      name_of_elmt_attr

--------------------- 
Element Attribute Data :        
--------------------- 


ELEMENT_ATTR No.   1  : name = "name_of_elmt_attr" 
                      : section = "mysection" 
                      : material = "ELASTIC" 
                      : type = SHELL_4NQ
                      : dof-mapping : gdof[0] =    1 : gdof[1] =    2 : gdof[2] =    3
                                      gdof[3] =    4 : gdof[4] =    5 : gdof[5] =    6
                      : Young's Modulus =  E =        1.000e+07 psi
                      : Poisson's ratio = nu =        3.000e-01   
                        
EXTERNAL NODAL LOADINGS 
--------------------------------------------------------------------------------------------
Node#       Fx (lbf)      Fy (lbf)     Fz (lbf)     Mx (lbf.in)    My (lbf.in)     Mz (lbf.in)
--------------------------------------------------------------------------------------------
   27        0.000    -1600.000        0.000        0.000        0.000        0.000
   28        0.000     1600.000        0.000        0.000        0.000        0.000

============= End of Finite Element Mesh Description ==============



*** COMPUTE STIFFNESS MATRICES 


------------------------------------------------------------------------------------------------------------------
 Node                                             Displacement
  No             displ-x           displ-y           displ-z             rot-x             rot-y             rot-z
------------------------------------------------------------------------------------------------------------------
 units               in                in                in               rad               rad               rad 
   1         0.00000e+00       0.00000e+00       0.00000e+00       0.00000e+00       0.00000e+00       0.00000e+00
   2         0.00000e+00       0.00000e+00       0.00000e+00       0.00000e+00       0.00000e+00       0.00000e+00
   3         0.00000e+00       0.00000e+00       0.00000e+00       0.00000e+00       0.00000e+00       0.00000e+00
   4         0.00000e+00       0.00000e+00       0.00000e+00       0.00000e+00       0.00000e+00       0.00000e+00
   5         0.00000e+00       0.00000e+00       0.00000e+00       0.00000e+00       0.00000e+00       0.00000e+00
   6         0.00000e+00       0.00000e+00       0.00000e+00       0.00000e+00       0.00000e+00       0.00000e+00
   7        -1.15985e-02      -1.37049e-02      -3.28007e-02       6.75552e-03       5.31289e-03      -2.42068e-03
   8        -4.42729e-06      -1.26893e-02      -1.07877e-06       5.83985e-03       2.04834e-07      -2.22032e-03
   9         1.16110e-02      -1.37026e-02       3.27987e-02       6.75552e-03      -5.31299e-03      -2.43215e-03
  10         1.16110e-02       1.37026e-02      -3.27987e-02       6.75552e-03       5.31299e-03       2.43215e-03
  11        -4.42729e-06       1.26893e-02       1.07877e-06       5.83985e-03      -2.04834e-07       2.22032e-03
  12        -1.15985e-02       1.37049e-02       3.28007e-02       6.75552e-03      -5.31289e-03       2.42068e-03
  13        -2.01536e-02      -4.66789e-02      -9.92201e-02       2.00632e-02       8.06653e-03      -3.88675e-03
  14         1.47267e-05      -4.62398e-02       1.00669e-06       1.91881e-02      -6.13953e-07      -4.19351e-03
  15         2.01303e-02      -4.67172e-02       9.92222e-02       2.00632e-02      -8.06695e-03      -3.85846e-03
  16         2.01303e-02       4.67172e-02      -9.92222e-02       2.00632e-02       8.06695e-03       3.85846e-03
  17         1.47267e-05       4.62398e-02      -1.00669e-06       1.91881e-02       6.13953e-07       4.19351e-03
  18        -2.01536e-02       4.66789e-02       9.92201e-02       2.00632e-02      -8.06653e-03       3.88675e-03
  19        -2.51655e-02      -9.34488e-02      -1.85174e-01       3.71516e-02       7.56330e-03      -5.16739e-03
  20        -2.75794e-05      -9.31491e-02       2.25876e-06       3.71082e-02       3.60377e-07      -4.90381e-03
  21         2.51541e-02      -9.32222e-02       1.85179e-01       3.71517e-02      -7.56308e-03      -5.18119e-03
  22         2.51541e-02       9.32222e-02      -1.85179e-01       3.71517e-02       7.56308e-03       5.18119e-03
  23        -2.75794e-05       9.31491e-02      -2.25876e-06       3.71082e-02      -3.60377e-07       4.90381e-03
  24        -2.51655e-02       9.34488e-02       1.85174e-01       3.71516e-02      -7.56330e-03       5.16739e-03
  25        -2.67685e-02      -1.46572e-01      -2.50528e-01       4.78582e-02       7.07525e-03      -5.17928e-03
  26        -2.21892e-05      -1.46735e-01      -1.73562e-06       5.43971e-02       4.38874e-07      -5.52920e-03
  27         2.72207e-02      -1.47599e-01       2.50525e-01       4.78584e-02      -7.07426e-03      -5.39516e-03
  28         2.72207e-02       1.47599e-01      -2.50525e-01       4.78584e-02       7.07426e-03       5.39516e-03
  29        -2.21892e-05       1.46735e-01       1.73562e-06       5.43971e-02      -4.38874e-07       5.52920e-03
  30        -2.67685e-02       1.46572e-01       2.50528e-01       4.78582e-02      -7.07525e-03       5.17928e-03


MEMBER FORCES 
------------------------------------------------------------------------------


 STRESS in Element No. 1,   Element: SHELL_4NQ;   Material: ELASTIC
 ==================================================================================
 coord = in,  stress = lbf/in,  moment = lbf*in/in,  curvtr = 1/in,  angle = rad

  x-coord   xx-stress   xy-stress   yy-stress    1-stress    2-stress     angle
  y-coord   xx-moment   xy-moment   yy-moment    1-moment    2-moment     angle
  z-coord   xx-strain   xy-strain   yy-strain   xx-curvtr   xy-curvtr   yy-curvtr
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
    5.000  -1.512e+03  -1.541e+02  -2.416e+02  -2.231e+02  -1.531e+03    -83.18
   -2.500  -4.194e+00   6.948e+00  -2.451e+00   3.681e+00  -1.033e+01     48.58
    2.500  -5.760e-04  -1.603e-04   8.486e-05  -2.657e-04   1.387e-03  -9.157e-05



 STRESS in Element No. 2,   Element: SHELL_4NQ;   Material: ELASTIC
 ==================================================================================
 coord = in,  stress = lbf/in,  moment = lbf*in/in,  curvtr = 1/in,  angle = rad

  x-coord   xx-stress   xy-stress   yy-stress    1-stress    2-stress     angle
  y-coord   xx-moment   xy-moment   yy-moment    1-moment    2-moment     angle
  z-coord   xx-strain   xy-strain   yy-strain   xx-curvtr   xy-curvtr   yy-curvtr
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
    5.000   1.513e+03  -1.520e+02   2.448e+02   1.531e+03   2.268e+02     -6.74
    2.500   4.194e+00   6.948e+00   2.450e+00   1.033e+01  -3.681e+00     41.42
    2.500   5.759e-04  -1.581e-04  -8.367e-05   2.656e-04   1.387e-03   9.157e-05



 STRESS in Element No. 3,   Element: SHELL_4NQ;   Material: ELASTIC
 ==================================================================================
 coord = in,  stress = lbf/in,  moment = lbf*in/in,  curvtr = 1/in,  angle = rad

  x-coord   xx-stress   xy-stress   yy-stress    1-stress    2-stress     angle
  y-coord   xx-moment   xy-moment   yy-moment    1-moment    2-moment     angle
  z-coord   xx-strain   xy-strain   yy-strain   xx-curvtr   xy-curvtr   yy-curvtr
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
    5.000  -1.389e+00  -6.276e-13  -8.709e-01  -8.709e-01  -1.389e+00    -90.00
    0.000  -4.775e-13   5.052e+00  -1.008e-13   5.052e+00  -5.052e+00     45.00
    0.000  -4.513e-07  -6.527e-19  -1.816e-07  -3.435e-17   1.009e-03   3.261e-18



 STRESS in Element No. 4,   Element: SHELL_4NQ;   Material: ELASTIC
 ==================================================================================
 coord = in,  stress = lbf/in,  moment = lbf*in/in,  curvtr = 1/in,  angle = rad

  x-coord   xx-stress   xy-stress   yy-stress    1-stress    2-stress     angle
  y-coord   xx-moment   xy-moment   yy-moment    1-moment    2-moment     angle
  z-coord   xx-strain   xy-strain   yy-strain   xx-curvtr   xy-curvtr   yy-curvtr
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
    5.000   1.513e+03   1.520e+02   2.448e+02   1.531e+03   2.268e+02      6.74
   -2.500  -4.194e+00   6.948e+00  -2.450e+00   3.681e+00  -1.033e+01     48.58
   -2.500   5.759e-04   1.581e-04  -8.367e-05  -2.656e-04   1.387e-03  -9.157e-05



 STRESS in Element No. 5,   Element: SHELL_4NQ;   Material: ELASTIC
 ==================================================================================
 coord = in,  stress = lbf/in,  moment = lbf*in/in,  curvtr = 1/in,  angle = rad

  x-coord   xx-stress   xy-stress   yy-stress    1-stress    2-stress     angle
  y-coord   xx-moment   xy-moment   yy-moment    1-moment    2-moment     angle
  z-coord   xx-strain   xy-strain   yy-strain   xx-curvtr   xy-curvtr   yy-curvtr
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
    5.000  -1.512e+03   1.541e+02  -2.416e+02  -2.231e+02  -1.531e+03     83.18
    2.500   4.194e+00   6.948e+00   2.451e+00   1.033e+01  -3.681e+00     41.42
   -2.500  -5.760e-04   1.603e-04   8.486e-05   2.657e-04   1.387e-03   9.157e-05



 STRESS in Element No. 6,   Element: SHELL_4NQ;   Material: ELASTIC
 ==================================================================================
 coord = in,  stress = lbf/in,  moment = lbf*in/in,  curvtr = 1/in,  angle = rad

  x-coord   xx-stress   xy-stress   yy-stress    1-stress    2-stress     angle
  y-coord   xx-moment   xy-moment   yy-moment    1-moment    2-moment     angle
  z-coord   xx-strain   xy-strain   yy-strain   xx-curvtr   xy-curvtr   yy-curvtr
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
   15.000  -1.047e+03  -1.442e+02   1.553e+02   1.724e+02  -1.064e+03    -83.25
   -2.500  -2.738e+00   1.327e+01  -3.153e+00   1.033e+01  -1.622e+01     44.55
    2.500  -4.374e-04  -1.500e-04   1.877e-04  -1.376e-04   2.650e-03  -1.791e-04



 STRESS in Element No. 7,   Element: SHELL_4NQ;   Material: ELASTIC
 ==================================================================================
 coord = in,  stress = lbf/in,  moment = lbf*in/in,  curvtr = 1/in,  angle = rad

  x-coord   xx-stress   xy-stress   yy-stress    1-stress    2-stress     angle
  y-coord   xx-moment   xy-moment   yy-moment    1-moment    2-moment     angle
  z-coord   xx-strain   xy-strain   yy-strain   xx-curvtr   xy-curvtr   yy-curvtr
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
   15.000   1.044e+03  -1.492e+02  -1.735e+02   1.062e+03  -1.915e+02     -6.89
    2.500   2.740e+00   1.327e+01   3.154e+00   1.622e+01  -1.033e+01     45.45
    2.500   4.383e-04  -1.552e-04  -1.946e-04   1.377e-04   2.650e-03   1.791e-04



 STRESS in Element No. 8,   Element: SHELL_4NQ;   Material: ELASTIC
 ==================================================================================
 coord = in,  stress = lbf/in,  moment = lbf*in/in,  curvtr = 1/in,  angle = rad

  x-coord   xx-stress   xy-stress   yy-stress    1-stress    2-stress     angle
  y-coord   xx-moment   xy-moment   yy-moment    1-moment    2-moment     angle
  z-coord   xx-strain   xy-strain   yy-strain   xx-curvtr   xy-curvtr   yy-curvtr
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
   15.000   5.231e+00  -6.445e-13   1.192e+00   5.231e+00   1.192e+00     -0.00
    0.000  -4.138e-13   1.361e+01  -1.104e-13   1.361e+01  -1.361e+01     45.00
    0.000   1.950e-06  -6.703e-19  -1.509e-07  -2.924e-17   2.717e-03   1.057e-18



 STRESS in Element No. 9,   Element: SHELL_4NQ;   Material: ELASTIC
 ==================================================================================
 coord = in,  stress = lbf/in,  moment = lbf*in/in,  curvtr = 1/in,  angle = rad

  x-coord   xx-stress   xy-stress   yy-stress    1-stress    2-stress     angle
  y-coord   xx-moment   xy-moment   yy-moment    1-moment    2-moment     angle
  z-coord   xx-strain   xy-strain   yy-strain   xx-curvtr   xy-curvtr   yy-curvtr
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
   15.000   1.044e+03   1.492e+02  -1.735e+02   1.062e+03  -1.915e+02      6.89
   -2.500  -2.740e+00   1.327e+01  -3.154e+00   1.033e+01  -1.622e+01     44.55
   -2.500   4.383e-04   1.552e-04  -1.946e-04  -1.377e-04   2.650e-03  -1.791e-04



 STRESS in Element No. 10,   Element: SHELL_4NQ;   Material: ELASTIC
 ==================================================================================
 coord = in,  stress = lbf/in,  moment = lbf*in/in,  curvtr = 1/in,  angle = rad

  x-coord   xx-stress   xy-stress   yy-stress    1-stress    2-stress     angle
  y-coord   xx-moment   xy-moment   yy-moment    1-moment    2-moment     angle
  z-coord   xx-strain   xy-strain   yy-strain   xx-curvtr   xy-curvtr   yy-curvtr
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
   15.000  -1.047e+03   1.442e+02   1.553e+02   1.724e+02  -1.064e+03     83.25
    2.500   2.738e+00   1.327e+01   3.153e+00   1.622e+01  -1.033e+01     45.45
   -2.500  -4.374e-04   1.500e-04   1.877e-04   1.376e-04   2.650e-03   1.791e-04



 STRESS in Element No. 11,   Element: SHELL_4NQ;   Material: ELASTIC
 ==================================================================================
 coord = in,  stress = lbf/in,  moment = lbf*in/in,  curvtr = 1/in,  angle = rad

  x-coord   xx-stress   xy-stress   yy-stress    1-stress    2-stress     angle
  y-coord   xx-moment   xy-moment   yy-moment    1-moment    2-moment     angle
  z-coord   xx-strain   xy-strain   yy-strain   xx-curvtr   xy-curvtr   yy-curvtr
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
   25.000  -6.399e+02  -1.474e+02  -1.261e+02  -8.678e+01  -6.792e+02    -75.07
   -2.500  -3.493e-02   1.753e+01  -1.206e+00   1.692e+01  -1.816e+01     44.04
    2.500  -2.408e-04  -1.533e-04   2.635e-05   2.511e-05   3.501e-03  -9.185e-05



 STRESS in Element No. 12,   Element: SHELL_4NQ;   Material: ELASTIC
 ==================================================================================
 coord = in,  stress = lbf/in,  moment = lbf*in/in,  curvtr = 1/in,  angle = rad

  x-coord   xx-stress   xy-stress   yy-stress    1-stress    2-stress     angle
  y-coord   xx-moment   xy-moment   yy-moment    1-moment    2-moment     angle
  z-coord   xx-strain   xy-strain   yy-strain   xx-curvtr   xy-curvtr   yy-curvtr
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
   25.000   6.459e+02  -1.356e+02   1.837e+02   6.827e+02   1.469e+02    -15.20
    2.500   3.313e-02   1.753e+01   1.206e+00   1.816e+01  -1.692e+01     45.96
    2.500   2.363e-04  -1.410e-04  -4.016e-06  -2.524e-05   3.501e-03   9.186e-05



 STRESS in Element No. 13,   Element: SHELL_4NQ;   Material: ELASTIC
 ==================================================================================
 coord = in,  stress = lbf/in,  moment = lbf*in/in,  curvtr = 1/in,  angle = rad

  x-coord   xx-stress   xy-stress   yy-stress    1-stress    2-stress     angle
  y-coord   xx-moment   xy-moment   yy-moment    1-moment    2-moment     angle
  z-coord   xx-strain   xy-strain   yy-strain   xx-curvtr   xy-curvtr   yy-curvtr
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
   25.000  -1.106e+01  -4.946e-13  -1.280e+00  -1.280e+00  -1.106e+01    -90.00
    0.000  -9.293e-14   1.915e+01   5.933e-14   1.915e+01  -1.915e+01     45.00
    0.000  -4.271e-06  -5.144e-19   8.155e-07  -8.504e-18   3.823e-03   6.697e-18



 STRESS in Element No. 14,   Element: SHELL_4NQ;   Material: ELASTIC
 ==================================================================================
 coord = in,  stress = lbf/in,  moment = lbf*in/in,  curvtr = 1/in,  angle = rad

  x-coord   xx-stress   xy-stress   yy-stress    1-stress    2-stress     angle
  y-coord   xx-moment   xy-moment   yy-moment    1-moment    2-moment     angle
  z-coord   xx-strain   xy-strain   yy-strain   xx-curvtr   xy-curvtr   yy-curvtr
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
   25.000   6.459e+02   1.356e+02   1.837e+02   6.827e+02   1.469e+02     15.20
   -2.500  -3.313e-02   1.753e+01  -1.206e+00   1.692e+01  -1.816e+01     44.04
   -2.500   2.363e-04   1.410e-04  -4.016e-06   2.524e-05   3.501e-03  -9.186e-05



 STRESS in Element No. 15,   Element: SHELL_4NQ;   Material: ELASTIC
 ==================================================================================
 coord = in,  stress = lbf/in,  moment = lbf*in/in,  curvtr = 1/in,  angle = rad

  x-coord   xx-stress   xy-stress   yy-stress    1-stress    2-stress     angle
  y-coord   xx-moment   xy-moment   yy-moment    1-moment    2-moment     angle
  z-coord   xx-strain   xy-strain   yy-strain   xx-curvtr   xy-curvtr   yy-curvtr
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
   25.000  -6.399e+02   1.474e+02  -1.261e+02  -8.678e+01  -6.792e+02     75.07
    2.500   3.493e-02   1.753e+01   1.206e+00   1.816e+01  -1.692e+01     45.96
   -2.500  -2.408e-04   1.533e-04   2.635e-05  -2.511e-05   3.501e-03   9.185e-05



 STRESS in Element No. 16,   Element: SHELL_4NQ;   Material: ELASTIC
 ==================================================================================
 coord = in,  stress = lbf/in,  moment = lbf*in/in,  curvtr = 1/in,  angle = rad

  x-coord   xx-stress   xy-stress   yy-stress    1-stress    2-stress     angle
  y-coord   xx-moment   xy-moment   yy-moment    1-moment    2-moment     angle
  z-coord   xx-strain   xy-strain   yy-strain   xx-curvtr   xy-curvtr   yy-curvtr
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
   35.000  -2.011e+02  -1.414e+02   1.018e+02   1.575e+02  -2.569e+02    -68.49
   -2.500   3.137e+00   1.247e+01   9.399e+00   1.912e+01  -6.585e+00     52.05
    2.500  -9.266e-05  -1.470e-04   6.485e-05   2.440e-05   2.489e-03   6.495e-04



 STRESS in Element No. 17,   Element: SHELL_4NQ;   Material: ELASTIC
 ==================================================================================
 coord = in,  stress = lbf/in,  moment = lbf*in/in,  curvtr = 1/in,  angle = rad

  x-coord   xx-stress   xy-stress   yy-stress    1-stress    2-stress     angle
  y-coord   xx-moment   xy-moment   yy-moment    1-moment    2-moment     angle
  z-coord   xx-strain   xy-strain   yy-strain   xx-curvtr   xy-curvtr   yy-curvtr
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
   35.000   2.026e+02  -1.497e+02  -2.592e+02   2.469e+02  -3.035e+02    -16.47
    2.500  -3.138e+00   1.247e+01  -9.399e+00   6.585e+00  -1.912e+01     37.95
    2.500   1.122e-04  -1.557e-04  -1.280e-04  -2.444e-05   2.489e-03  -6.495e-04



 STRESS in Element No. 18,   Element: SHELL_4NQ;   Material: ELASTIC
 ==================================================================================
 coord = in,  stress = lbf/in,  moment = lbf*in/in,  curvtr = 1/in,  angle = rad

  x-coord   xx-stress   xy-stress   yy-stress    1-stress    2-stress     angle
  y-coord   xx-moment   xy-moment   yy-moment    1-moment    2-moment     angle
  z-coord   xx-strain   xy-strain   yy-strain   xx-curvtr   xy-curvtr   yy-curvtr
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
   35.000   1.569e+00   1.043e-12   7.649e-01   1.569e+00   7.649e-01      0.00
    0.000  -1.137e-13   2.265e+01  -6.166e-14   2.265e+01  -2.265e+01     45.00
    0.000   5.357e-07   1.084e-18   1.177e-07  -7.314e-18   4.523e-03  -2.115e-18



 STRESS in Element No. 19,   Element: SHELL_4NQ;   Material: ELASTIC
 ==================================================================================
 coord = in,  stress = lbf/in,  moment = lbf*in/in,  curvtr = 1/in,  angle = rad

  x-coord   xx-stress   xy-stress   yy-stress    1-stress    2-stress     angle
  y-coord   xx-moment   xy-moment   yy-moment    1-moment    2-moment     angle
  z-coord   xx-strain   xy-strain   yy-strain   xx-curvtr   xy-curvtr   yy-curvtr
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
   35.000   2.026e+02   1.497e+02  -2.592e+02   2.469e+02  -3.035e+02     16.47
   -2.500   3.138e+00   1.247e+01   9.399e+00   1.912e+01  -6.585e+00     52.05
   -2.500   1.122e-04   1.557e-04  -1.280e-04   2.444e-05   2.489e-03   6.495e-04



 STRESS in Element No. 20,   Element: SHELL_4NQ;   Material: ELASTIC
 ==================================================================================
 coord = in,  stress = lbf/in,  moment = lbf*in/in,  curvtr = 1/in,  angle = rad

  x-coord   xx-stress   xy-stress   yy-stress    1-stress    2-stress     angle
  y-coord   xx-moment   xy-moment   yy-moment    1-moment    2-moment     angle
  z-coord   xx-strain   xy-strain   yy-strain   xx-curvtr   xy-curvtr   yy-curvtr
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
   35.000  -2.011e+02   1.414e+02   1.018e+02   1.575e+02  -2.569e+02     68.49
    2.500  -3.137e+00   1.247e+01  -9.399e+00   6.585e+00  -1.912e+01     37.95
   -2.500  -9.266e-05   1.470e-04   6.485e-05  -2.440e-05   2.489e-03  -6.495e-04


Developed in June 1996 by Lanheng Jin and Mark Austin
Last Modified September 28, 1996
Copyright © 1996, Lanheng Jin and Mark Austin, Department of Civil Engineering, University of Maryland