Vaik
Guest
Hello.
having searched for a long time on the web and on the forum itself regarding what is reported in the title, without finding any exhaustive answer, I write these lines. I will refer to the scheme I attach. also specific that when I write "an", I will mean "neutral axis".
My question is:
how can I determine the position of the neutral axis with which to calculate the second-order surface inertia module (i [mm^4] ) in a beam with carvings, section variations ?
My reasoning is as follows:
example a:
I start from the simple example of a constant section beam (for example rectangular bxh), fig1, stuck to an extreme and loaded with concentrated force to the extreme opposite. the neutral axis to which to calculate the moment of inertia izz, in this configuration, will coincide with the axis of symmetry z-z, fig6. No problem.
example b:
If I now add a slit as in fig9, removing material, I get, in correspondence of the cut I have operated, a section bxh', with h'<h. I have to think of the position of the neutral axis in this section I would be spontaneous to place it also in half-try and thus coincide with z'-z' (fig9 ).
considering now the whole beam of fig9 along its larger size and thus displaying the trajectory of the successive positions of the neutral axis for each section that compose it, I would get a broken line with a pattern similar to the lower edge of the same beam of fig9 which passes exactly for the half-points of each section leaving so much traction material above, as material in compression below (I did not prepare an image in the diagram... ).
d1) is this a correct and truthful result?
d2) or the above trajectory is, instead, that of fig.10 and fig11 ? or the trajectory of the neutral axis undergoes a δy variation, compared to the position obtained by calculating according to the example a, which places the neutral axis of the bxh section ( near the gap ) to a "half way" between the position of the neutral axis of example a and example b.
d3) if the question is affirmed d2, then the "throughway" how can one quantify? Could you approach the average position between those obtained by example a and example b?
I tried to give myself an answer by reproducing examples with the inventor fem, and I also looked for autocad plug-ins that calculated the position of the neutral axis, but nothing satisfactory.
If there are any engineers who can also only refer to a link (also sites in English) that explains exactly what they asked, I would be grateful!
in the calculation of the position of the an I have thought of the balance that the sections that stand above and below the neutral axis must respect, but still do not return anything.
having searched for a long time on the web and on the forum itself regarding what is reported in the title, without finding any exhaustive answer, I write these lines. I will refer to the scheme I attach. also specific that when I write "an", I will mean "neutral axis".
My question is:how can I determine the position of the neutral axis with which to calculate the second-order surface inertia module (i [mm^4] ) in a beam with carvings, section variations ?
My reasoning is as follows:
example a:
I start from the simple example of a constant section beam (for example rectangular bxh), fig1, stuck to an extreme and loaded with concentrated force to the extreme opposite. the neutral axis to which to calculate the moment of inertia izz, in this configuration, will coincide with the axis of symmetry z-z, fig6. No problem.
example b:
If I now add a slit as in fig9, removing material, I get, in correspondence of the cut I have operated, a section bxh', with h'<h. I have to think of the position of the neutral axis in this section I would be spontaneous to place it also in half-try and thus coincide with z'-z' (fig9 ).
considering now the whole beam of fig9 along its larger size and thus displaying the trajectory of the successive positions of the neutral axis for each section that compose it, I would get a broken line with a pattern similar to the lower edge of the same beam of fig9 which passes exactly for the half-points of each section leaving so much traction material above, as material in compression below (I did not prepare an image in the diagram... ).
d1) is this a correct and truthful result?
d2) or the above trajectory is, instead, that of fig.10 and fig11 ? or the trajectory of the neutral axis undergoes a δy variation, compared to the position obtained by calculating according to the example a, which places the neutral axis of the bxh section ( near the gap ) to a "half way" between the position of the neutral axis of example a and example b.
d3) if the question is affirmed d2, then the "throughway" how can one quantify? Could you approach the average position between those obtained by example a and example b?
I tried to give myself an answer by reproducing examples with the inventor fem, and I also looked for autocad plug-ins that calculated the position of the neutral axis, but nothing satisfactory.
If there are any engineers who can also only refer to a link (also sites in English) that explains exactly what they asked, I would be grateful!
in the calculation of the position of the an I have thought of the balance that the sections that stand above and below the neutral axis must respect, but still do not return anything.