Output File for Cantilever Shear Beam (8x2 irregular mesh).


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


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

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

   Dimension of Problem        =      3

   Number Nodes                =     27
   Degrees of Freedom per node =      6
   Max No Nodes Per Element    =      4

   Number Elements             =     16
   Number Element Attributes   =      1
   Number Loaded Nodes         =      3
   Number Loaded Elements      =      0


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

    1    0.0000e+00 in    0.0000e+00 in    6.0000e+00 in    -1    -2    -3    -4    -5    -6 
    2    0.0000e+00 in    0.0000e+00 in    0.0000e+00 in    -7    -8    -9   -10   -11   -12 
    3    0.0000e+00 in    0.0000e+00 in   -6.0000e+00 in   -13   -14   -15   -16   -17   -18 
    4    6.0000e+00 in    0.0000e+00 in    6.0000e+00 in     1     2     3     4     5     6 
    5    7.0000e+00 in    0.0000e+00 in    0.0000e+00 in     7     8     9    10    11    12 
    6    8.0000e+00 in    0.0000e+00 in   -6.0000e+00 in    13    14    15    16    17    18 
    7    1.2000e+01 in    0.0000e+00 in    6.0000e+00 in    19    20    21    22    23    24 
    8    1.4000e+01 in    0.0000e+00 in    0.0000e+00 in    25    26    27    28    29    30 
    9    1.6000e+01 in    0.0000e+00 in   -6.0000e+00 in    31    32    33    34    35    36 
   10    1.8000e+01 in    0.0000e+00 in    6.0000e+00 in    37    38    39    40    41    42 
   11    1.8000e+01 in    0.0000e+00 in    0.0000e+00 in    43    44    45    46    47    48 
   12    1.8000e+01 in    0.0000e+00 in   -6.0000e+00 in    49    50    51    52    53    54 
   13    2.4000e+01 in    0.0000e+00 in    6.0000e+00 in    55    56    57    58    59    60 
   14    2.2000e+01 in    0.0000e+00 in    0.0000e+00 in    61    62    63    64    65    66 
   15    2.0000e+01 in    0.0000e+00 in   -6.0000e+00 in    67    68    69    70    71    72 
   16    3.0000e+01 in    0.0000e+00 in    6.0000e+00 in    73    74    75    76    77    78 
   17    2.7000e+01 in    0.0000e+00 in    0.0000e+00 in    79    80    81    82    83    84 
   18    2.4000e+01 in    0.0000e+00 in   -6.0000e+00 in    85    86    87    88    89    90 
   19    3.6000e+01 in    0.0000e+00 in    6.0000e+00 in    91    92    93    94    95    96 
   20    3.2000e+01 in    0.0000e+00 in    0.0000e+00 in    97    98    99   100   101   102 
   21    2.8000e+01 in    0.0000e+00 in   -6.0000e+00 in   103   104   105   106   107   108 
   22    4.2000e+01 in    0.0000e+00 in    6.0000e+00 in   109   110   111   112   113   114 
   23    4.0000e+01 in    0.0000e+00 in    0.0000e+00 in   115   116   117   118   119   120 
   24    3.8000e+01 in    0.0000e+00 in   -6.0000e+00 in   121   122   123   124   125   126 
   25    4.8000e+01 in    0.0000e+00 in    6.0000e+00 in   127   128   129   130   131   132 
   26    4.8000e+01 in    0.0000e+00 in    0.0000e+00 in   133   134   135   136   137   138 
   27    4.8000e+01 in    0.0000e+00 in   -6.0000e+00 in   139   140   141   142   143   144 


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

       1   SHELL_4NQ            2         5         4         1      name_of_elmt_attr
       2   SHELL_4NQ            3         6         5         2      name_of_elmt_attr
       3   SHELL_4NQ            5         8         7         4      name_of_elmt_attr
       4   SHELL_4NQ            6         9         8         5      name_of_elmt_attr
       5   SHELL_4NQ            8        11        10         7      name_of_elmt_attr
       6   SHELL_4NQ            9        12        11         8      name_of_elmt_attr
       7   SHELL_4NQ           11        14        13        10      name_of_elmt_attr
       8   SHELL_4NQ           12        15        14        11      name_of_elmt_attr
       9   SHELL_4NQ           14        17        16        13      name_of_elmt_attr
      10   SHELL_4NQ           15        18        17        14      name_of_elmt_attr
      11   SHELL_4NQ           17        20        19        16      name_of_elmt_attr
      12   SHELL_4NQ           18        21        20        17      name_of_elmt_attr
      13   SHELL_4NQ           20        23        22        19      name_of_elmt_attr
      14   SHELL_4NQ           21        24        23        20      name_of_elmt_attr
      15   SHELL_4NQ           23        26        25        22      name_of_elmt_attr
      16   SHELL_4NQ           24        27        26        23      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 =        3.000e+04 ksi
                      : Poisson's ratio = nu =        2.500e-01   
                        
EXTERNAL NODAL LOADINGS 
--------------------------------------------------------------------------------------------
Node#       Fx (lbf)      Fy (lbf)     Fz (lbf)     Mx (lbf.in)    My (lbf.in)     Mz (lbf.in)
--------------------------------------------------------------------------------------------
   25        0.000        0.000    10000.000        0.000        0.000        0.000
   27        0.000        0.000    10000.000        0.000        0.000        0.000
   26        0.000        0.000    20000.000        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        -1.46331e-02       0.00000e+00       1.05383e-02       0.00000e+00      -1.96223e-03       0.00000e+00
   5        -4.31491e-04       0.00000e+00       1.05926e-02       0.00000e+00      -2.46594e-03       0.00000e+00
   6         1.88403e-02       0.00000e+00       1.52738e-02       0.00000e+00      -4.03028e-03       0.00000e+00
   7        -2.77200e-02       0.00000e+00       3.20755e-02       0.00000e+00      -3.72629e-03       0.00000e+00
   8        -6.02127e-04       0.00000e+00       4.08947e-02       0.00000e+00      -5.54235e-03       0.00000e+00
   9         3.43711e-02       0.00000e+00       5.36208e-02       0.00000e+00      -5.85988e-03       0.00000e+00
  10        -3.79490e-02       0.00000e+00       6.58068e-02       0.00000e+00      -6.21430e-03       0.00000e+00
  11         6.72013e-05       0.00000e+00       6.53676e-02       0.00000e+00      -6.23740e-03       0.00000e+00
  12         3.81091e-02       0.00000e+00       6.63419e-02       0.00000e+00      -6.36806e-03       0.00000e+00
  13        -4.64591e-02       0.00000e+00       1.09866e-01       0.00000e+00      -8.31946e-03       0.00000e+00
  14         6.32852e-04       0.00000e+00       9.35229e-02       0.00000e+00      -6.89944e-03       0.00000e+00
  15         4.16223e-02       0.00000e+00       8.02943e-02       0.00000e+00      -6.46516e-03       0.00000e+00
  16        -5.35071e-02       0.00000e+00       1.62113e-01       0.00000e+00      -9.22191e-03       0.00000e+00
  17         8.43905e-04       0.00000e+00       1.34269e-01       0.00000e+00      -8.56397e-03       0.00000e+00
  18         4.74473e-02       0.00000e+00       1.10367e-01       0.00000e+00      -6.58844e-03       0.00000e+00
  19        -5.82725e-02       0.00000e+00       2.20414e-01       0.00000e+00      -1.01443e-02       0.00000e+00
  20         6.78115e-04       0.00000e+00       1.80344e-01       0.00000e+00      -9.10539e-03       0.00000e+00
  21         5.25396e-02       0.00000e+00       1.43784e-01       0.00000e+00      -8.15555e-03       0.00000e+00
  22        -6.13077e-02       0.00000e+00       2.82147e-01       0.00000e+00      -1.00130e-02       0.00000e+00
  23         4.01717e-05       0.00000e+00       2.60716e-01       0.00000e+00      -1.02499e-02       0.00000e+00
  24         6.03592e-02       0.00000e+00       2.39840e-01       0.00000e+00      -9.56628e-03       0.00000e+00
  25        -6.23475e-02       0.00000e+00       3.45517e-01       0.00000e+00      -1.04198e-02       0.00000e+00
  26        -1.69471e-04       0.00000e+00       3.45455e-01       0.00000e+00      -1.00979e-02       0.00000e+00
  27         6.29812e-02       0.00000e+00       3.45526e-01       0.00000e+00      -1.05463e-02       0.00000e+00


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
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
    3.250  -3.623e+04   5.325e+03  -5.363e+03  -4.470e+03  -3.713e+04     80.48
    0.000   0.000e+00   0.000e+00   0.000e+00   0.000e+00   0.000e+00     45.00
    3.000  -1.163e-03   4.438e-04   1.232e-04   0.000e+00   0.000e+00   0.000e+00



 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
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
    3.750   3.624e+04   1.527e+03   3.267e+03   3.631e+04   3.197e+03      2.65
    0.000   0.000e+00   0.000e+00   0.000e+00   0.000e+00   0.000e+00     45.00
   -3.000   1.181e-03   1.272e-04  -1.931e-04   0.000e+00   0.000e+00   0.000e+00



 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
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
    9.750  -3.067e+04   6.957e+03  -2.008e+02   1.313e+03  -3.218e+04     77.73
    0.000   0.000e+00   0.000e+00   0.000e+00   0.000e+00   0.000e+00     45.00
    3.000  -1.021e-03   5.798e-04   2.489e-04   0.000e+00   0.000e+00   0.000e+00



 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
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
   11.250   3.148e+04   5.670e+02  -4.238e+03   3.149e+04  -4.247e+03      0.91
    0.000   0.000e+00   0.000e+00   0.000e+00   0.000e+00   0.000e+00     45.00
   -3.000   1.085e-03   4.725e-05  -4.036e-04   0.000e+00   0.000e+00   0.000e+00



 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
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
   15.500  -2.503e+04   5.500e+03  -3.611e+02   8.094e+02  -2.620e+04     77.99
    0.000   0.000e+00   0.000e+00   0.000e+00   0.000e+00   0.000e+00     45.00
    3.000  -8.314e-04   4.583e-04   1.966e-04   0.000e+00   0.000e+00   0.000e+00



 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
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
   16.500   2.355e+04   3.103e+01   2.268e+03   2.355e+04   2.268e+03      0.08
    0.000   0.000e+00   0.000e+00   0.000e+00   0.000e+00   0.000e+00     45.00
   -3.000   7.661e-04   2.586e-06  -1.206e-04   0.000e+00   0.000e+00   0.000e+00



 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
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
   20.500  -2.218e+04   8.454e+02  -1.458e+02  -1.134e+02  -2.221e+04     87.81
    0.000   0.000e+00   0.000e+00   0.000e+00   0.000e+00   0.000e+00     45.00
    3.000  -7.381e-04   7.045e-05   1.800e-04   0.000e+00   0.000e+00   0.000e+00



 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
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
   19.500   2.068e+04   6.339e+03   2.218e+03   2.265e+04   2.517e+02     17.24
    0.000   0.000e+00   0.000e+00   0.000e+00   0.000e+00   0.000e+00     45.00
   -3.000   6.710e-04   5.282e-04  -9.841e-05   0.000e+00   0.000e+00   0.000e+00



 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
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
   25.750  -2.001e+04  -1.356e+03   1.304e+03   1.390e+03  -2.009e+04    -86.37
    0.000   0.000e+00   0.000e+00   0.000e+00   0.000e+00   0.000e+00     45.00
    3.000  -6.778e-04  -1.130e-04   2.102e-04   0.000e+00   0.000e+00   0.000e+00



 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
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
   23.250   1.939e+04   8.368e+03   2.213e+03   2.279e+04  -1.189e+03     22.13
    0.000   0.000e+00   0.000e+00   0.000e+00   0.000e+00   0.000e+00     45.00
   -3.000   6.279e-04   6.973e-04  -8.781e-05   0.000e+00   0.000e+00   0.000e+00



 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
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
   31.250  -1.364e+04  -1.247e+03   1.085e+03   1.190e+03  -1.374e+04    -85.19
    0.000   0.000e+00   0.000e+00   0.000e+00   0.000e+00   0.000e+00     45.00
    3.000  -4.637e-04  -1.039e-04   1.498e-04   0.000e+00   0.000e+00   0.000e+00



 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
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
   27.750   9.700e+03   8.272e+03   5.846e+03   1.627e+04  -7.208e+02     38.44
    0.000   0.000e+00   0.000e+00   0.000e+00   0.000e+00   0.000e+00     45.00
   -3.000   2.746e-04   6.894e-04   1.140e-04   0.000e+00   0.000e+00   0.000e+00



 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
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
   37.500  -1.015e+04   1.152e+03   1.665e+03   1.777e+03  -1.026e+04     84.48
    0.000   0.000e+00   0.000e+00   0.000e+00   0.000e+00   0.000e+00     45.00
    3.000  -3.522e-04   9.599e-05   1.401e-04   0.000e+00   0.000e+00   0.000e+00



 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
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
   34.500   1.035e+04   4.803e+03   7.690e+02   1.234e+04  -1.225e+03     22.54
    0.000   0.000e+00   0.000e+00   0.000e+00   0.000e+00   0.000e+00     45.00
   -3.000   3.385e-04   4.003e-04  -6.060e-05   0.000e+00   0.000e+00   0.000e+00



 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
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
   44.500  -2.710e+03   3.365e+03  -7.796e+01   2.220e+03  -5.007e+03     55.68
    0.000   0.000e+00   0.000e+00   0.000e+00   0.000e+00   0.000e+00     45.00
    3.000  -8.967e-05   2.804e-04   1.998e-05   0.000e+00   0.000e+00   0.000e+00



 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
 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
   43.500   3.215e+03   3.391e+03   2.282e+03   6.171e+03  -6.750e+02     41.08
    0.000   0.000e+00   0.000e+00   0.000e+00   0.000e+00   0.000e+00     45.00
   -3.000   8.814e-05   2.826e-04   4.927e-05   0.000e+00   0.000e+00   0.000e+00


Developed in June 1996 by Lanheng Jin and Mark Austin
Last Modified September 27, 1996
Copyright © 1996, Lanheng Jin and Mark Austin, Department of Civil Engineering, University of Maryland