Hi there,
Perform the analysis , Go to results..select Plate and shell results, in the results window RghtClick and select Tables and Columns and select whatever results you want for that wall and click Ok. For the extreme results, you can check the envelope tab that lies at the bottom.
Hope this is useful for you 🙂
Mind that for panels it is important to select the right layer depending on the kind of stress you are checking: top/bottom for bending; middle for shear.
hello;
i've a problem and i can not get the max and min stresses because all the result gives 00.00 as value,so can you explain more or have you a short video!
best regards
Mind that for loads acting in the plane of a panel the shear stresses (in the direction perpendicular to the panel) are 0s.
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Try to change the units to T/m2. I don't expect that yiu have forces large enough to generate 'significant' values for T/mm2 and you either need to change the units or increase the precision of the results display for the current one (0,123456789).
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Sorry for jumping on to this thread, but I have a related question.
You mentioned that Upper and Lower layer of stress are for bending and Middle layer for shear. What about for axial compression or tension?
For example, we have a shear wall under gravity load, when we design for axial compression in the wall should we be choosing middle layer instead of upper/lower? Note that sometimes upper/lower layer stress can be 20 to 30% larger than middle layer.
For pure tension/compression the layer doesn't matter. For combined axial force and bending check both top and bottom one.
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