<
From version < 41.1 >
edited by Hamid Richard Allili
on 2019/11/27 12:23
To version < 42.1 >
edited by Hamid Richard Allili
on 2019/11/27 12:23
>
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71 71  * All layer maximum by stress type (e.g. All layer, Sigma x+): search for the combination which results the largest positive x directional normal stress along all the layers at the selected point, on all the five stress figures the result of this combination is displayed
72 72  * Layer maximum by stress type (e.g. 2. layer, Sigma x+): search for the combination which results the largest positive x directional normal stress in the second layer at the selected point, on all the five stress figures the result of this combination is displayed
73 73  
74 +[[image:1574853829573-840.png||height="256" width="659"]]
74 74  
75 75  ===== //Shell based stress detailed result// =====
76 76  
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118 118   It is typically applied for walls (in plane loaded structures), the "no glue at narrow sides" option must be checked in the application data.
119 119  
120 120  These methods are based on different standards and scientific papers, further information about the detailed checking process can be found in the theory manual of this feature: Theory of Laminated Composite Shells - CLT application. In the detailed result of the CLT panel the performed design calculations together with a geometry figure showing the critical nodes are displayed.
122 +
123 +[[image:1574853711423-165.png]]
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