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From version < 33.1 >
edited by Hamid Richard Allili
on 2019/11/27 08:49
To version < 34.1 >
edited by Hamid Richard Allili
on 2019/11/27 08:52
>
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... ... @@ -145,20 +145,24 @@
145 145  
146 146  The following design checking criteria are available:
147 147  
148 -- stress checks by EC5
149 - - tension/compression and bending in both grain and perpendicular to grain direction
150 - - transverse shear stresses and rolling shear.
151 - In case of CLT panels these checks are extended by performing them layer by layer (in the current layer's local system), at top and bottom or at parabola maximum in case of transverse shear stresses.
148 +* stress checks by EC5
149 +** tension/compression and bending in both grain and perpendicular to grain direction
150 +** transverse shear stresses and rolling shear.
152 152  
153 -- interaction checks
154 - - shear interaction
155 - - tension/compression and shear.
156 - As these are not included in EC5, in the calculation parameter of the CLT panelUser can specify whether to consider them during the design calculation or not.
152 + In case of CLT panels these checks are extended by performing them layer by layer (in the current layer's local system), at top and bottom or at parabola maximum in case of transverse shear stresses.
157 157  
158 -- shell buckling check
159 - It is performed only for those buckling regions, which has non-zero buckling factor, also for those layers, which are less than 45° from the buckling direction.
154 +* interaction checks
155 +** shear interaction
156 +** tension/compression and shear.
160 160  
161 -- torsional check
162 - It is typically applied for walls (in plane loaded structures), the "no glue at narrow sides" option must be checked in the application data.
158 + As these are not included in EC5, in the calculation parameter of the CLT panelUser can specify whether to consider them during the design calculation or not.
163 163  
160 +* shell buckling check
161 +
162 + It is performed only for those buckling regions, which has non-zero buckling factor, also for those layers, which are less than 45° from the buckling direction.
163 +
164 +* torsional check
165 +
166 + It is typically applied for walls (in plane loaded structures), the "no glue at narrow sides" option must be checked in the application data.
167 +
164 164  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.
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