<
From version < 30.1 >
edited by Hamid Richard Allili
on 2019/11/26 15:23
To version < 31.1 >
edited by Hamid Richard Allili
on 2019/11/26 15:44
>
Change comment: There is no comment for this version

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... ... @@ -106,7 +106,7 @@
106 106  
107 107  [[image:1574690365292-190.png||height="397" width="922"]]
108 108  
109 -It is worth to mention that in contrary with the non-laminated shells, the transverse shear stresses (Tau y'z' and Tau x'z') can be also displayed at the top and bottom of layers besides the center, as in case of some intermediate layer they are not necessarily zero (for non-laminated shells, due to the parabolic stress distribution the top and bottom values are always zero, only the center value can be selected from the shell stresses list).
109 +It is worth to mention that in contrary to the non-laminated shells, the transverse shear stresses (Tau y'z' and Tau x'z') can be also displayed at the top and bottom of layers besides the center, as in case of some intermediate layer they are not necessarily zero (for non-laminated shells, due to the parabolic stress distribution the top and bottom values are always zero, only the center value can be selected from the shell stresses list).
110 110  
111 111  ==== Stress detailed results ====
112 112  
... ... @@ -114,7 +114,7 @@
114 114  
115 115  ===== //Point based stress detailed result// =====
116 116  
117 -User can select an arbitrary point on the CLT/GLC panel, in the detailed result the geometry of the shell and the five stress components are displayed. As the whole section of the shell can be seen here, the coordinate system selector is supplemented with each layer's local system options. In case of maximum result (maximum of load combinations, etc.) plenty of maximum criteria available, which can be grouped by the following:
117 +User can select an arbitrary point on the CLT/GLC panel, in the detailed result the geometry of the shell and the five stress components are displayed. As the whole section of the shell can be seen here, the coordinate system selector is supplemented with each layer's local system options. In case of maximum result (maximum of load combinations, etc.) plenty of maximum criteria are available, which can be grouped by the following:
118 118  
119 119  • All components maximum (e.g. All components+): search for the combination(s) component by component which results the largest positive value of the stress component along all the layers at the selected point, on the stress figures the result of the combinations belonging to the components is displayed (note that there can be five different combination displayed in the detailed result)
120 120  
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