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