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To gather the related axial forces (specifically for the Strength Limit State), 1.Analyze the global model. Then, on the FEA tab, go to Composite Element Forces (Sectional).
 Navigate to the relevant stage for which you are interested in the results. The results can be viewed for the Construction Stages,
 ...or for Combination Cases, including LL cases, Composite/Non-composite cases, or for Limit States (max/min).   After specifying the case for viewing the reuslts results, the result results can be filetered filtered to see onlt bootom only the bottom flange results. For further clarification, refer to the video attached below. Results.mp4After specifying the case, the results at the position (station) where the access hole will be created can be obtained and applied to the access hole plate object.
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Fx on Each Side: Specify the Fx force to be applied to the plate. Refer to the Info Panel above for further information on extracting the related axial force from the global model.
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After defining the parameters for the Bottom Flange Access Hole Load object and analyzing the model, users can go to the FEA view. Image AddedSwitch to Surface Stresses. Image AddedVon Mises Stress: Image AddedTo obtain the desired FEM: Image Added Image Added |