stresses in global x direction within shell element
stresses in global x direction within shell element
(OP)
Hi,
I'm trying to deduce the stresses in my shell element S4R in the global x-direction.
I requested S11 and S22 in history output but there are large differences for the positive (upper surface) and
negative (bottom surface). Can anyone explain what the correct procedure is?
I'm trying to deduce the stresses in my shell element S4R in the global x-direction.
I requested S11 and S22 in history output but there are large differences for the positive (upper surface) and
negative (bottom surface). Can anyone explain what the correct procedure is?





RE: stresses in global x direction within shell element
Afterwards you can create xy-data based on that new field.