Bending moments about two different axes

In summary, the conversation discusses the problem of solving a beam structure and the validity of including two different torques in the same expression. The concept of bending moments and their relationship to couples is also explored, with the conclusion that the internal forces on a cross-section can be decomposed into normal forces, shear forces, and a couple moment. There is also mention of the subtleties involved in mechanical engineering.
  • #1
etotheipi
I was reading through a set of notes and found something a little odd. The aim is to solve the beam structure shown below, which is massless and of length ##l##.

1589116434300.png


By considering the beam as a whole, we obtain ##A_y = P##, ##A_x = N## and by taking moments about A we see ##M_A = Pl##.

However, now we consider a segment of the beam up to a distance ##x## along its length. We define the reaction forces and internal bending moments at this point to be ##N_x##, ##V_x## and ##M_x## as shown. The ##\sum F_x## and ##\sum F_y## parts are fine, but I wonder how they justify their third equation?

As far as I am aware, the internal bending moment at any point in the beam is taken about an axis passing through that point (N.B. we can really define 3 bending moments, but in this problem we only need the 1), like this:

1589116812882.png


##M_A## is taken about one axis, and ##M_x## is taken about another parallel axis displaced from the first axis by a distance ##x##. But when balancing torques, it only makes sense to add torques about the same axis!

I wondered then, why they used two torques about different axes in the same expression? Thanks!
 
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  • #2
Imagine that the beam we have becomes only the x section and that a moment of magnitude P(L-x) is applied to that end, but not any force perpendicular to the beam, only the longitudinal N force.
We can achieve that by welding a lever to that end and applying two forces (which cancel each other) to it.
 
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  • #3
Lnewqban said:
Imagine that the beam we have becomes only the x section and that a moment of magnitude P(L-x) is applied to that end, but not any force perpendicular to the beam, only the longitudinal N force.
We can achieve that by welding a lever to that end and applying two forces (which cancel each other) to it.

I'm not sure I follow; I'm happy with considering a section of the beam and defining the internal forces at the cross section in the middle, I just don't see how the torque expression they give is valid. ##M_x## and ##M_A## are about different axes?

If we take moments about A, then the torque of the forces producing ##M_x## about an axis at ##x## will not be ##M_x## about an axis at A, since the lever arm of all of those forces have changed?
 
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  • #4
I also don't know whether or not I am being of any help, perhaps I did not understand your question.
What I am trying to say is that the location and magnitude of Mx is real, in both my example and the original configuration.
One way or another, Mx is the reason for the existence of Ma at the anchored end of the beam.
 
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  • #5
Right, sure, but ##M_x## is the torque about an axis passing through ##x## caused by uneven distribution of stress across a cross section at ##x##, whilst ##M_A## is the torque about an axis through ##A##.

They take moments about ##A##, but include ##M_x## in their expression. I would argue that the torque produced by the uneven distribution of stress at ##x## is not ##M_x## when taken about ##A##.
 
  • #6
It seems that you are back to the original idea. :smile:
If you don't mind, I would like to ask you to forget about the mathematical details for a minute.
Can you see the physical relationship between both moments?
 
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  • #7
I can see why there is a need for the bending moments on either side of the section of length ##x##. The ##M_x## arrow is really curling in the opposite direction.
 
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  • #8
Exactly!
The beam must "smile" if equilibrium exists.
If we replace the anchoring of the left end of the beam with a hinge we eliminate the possibility of a reactive moment at that point.
Then, the beam would rotate around that point A, same with force P applied at the right end or with Mx applied at point x.
 
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  • #9
I wonder, are bending moments always caused by couples?

The moment of a couple is indeed invariant for all parallel axes, which would be a resolution.
 
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  • #10
etotheipi said:
I wonder, are bending moments always caused by couples?

The moment of a couple is indeed invariant for all parallel axes, which would be a resolution.
I would venture to respond yes to your question.
"Pure moments" do not exist in nature, we always have a force and a lever involved in such abstract concept.
But it is a very useful concept, nevertheless.

What makes bending or flexing of members the worse scenario in most cases of resistence of material and structural problems is the huge ratio of internal forces to available lever distances compared to the external forces and dimensions (in other words, how many times is a beam long compared to its sectional height).
 
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  • #11
Ah, awesome, thank you @Lnewqban!

In that case for a prismatic member in pure bending, with bending moments on each side ##\vec{M}_A## and ##\vec{M}_B##, the total moment about ##A## is also ##\vec{M}_A + \vec{M}_B## since the moment of the couple producing ##\vec{M}_{B}## about ##B## is the same as about ##A##. I have the feeling that on any cross-section, the effect of the internal forces can always be decomposed into a normal forces and two shear forces, and at the same time can be decomposed into a couple of moment ##\vec{M}##.

I have much respect for anyone who has understood all of the quirks of mechanical engineering, I thought I'd try my hand at it and have bee slightly taken aback at how many subtleties there are to it...
 
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  • #12
You are very welcome, etotheipi :smile:
I am glad that I could help you clarifying your question.
 
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What is a bending moment?

A bending moment is a measure of the force applied to a structural element that causes it to bend. It is typically measured in units of force multiplied by distance, such as Newton-meters (Nm) or pound-feet (lb-ft).

How does the bending moment affect a structural element?

The bending moment causes the structural element to bend or deform. This can lead to stress and strain within the material, which can ultimately result in failure if the bending moment is too great.

What are the two different axes in bending moments?

The two different axes in bending moments refer to the two perpendicular directions in which the bending moment can act on a structural element. These are typically referred to as the x-axis and the y-axis.

How is the bending moment calculated?

The bending moment is calculated by multiplying the force applied to the structural element by the distance from the point of application to the point where the bending moment is being measured. This distance is known as the moment arm.

Why is it important to consider bending moments about two different axes?

Considering bending moments about two different axes allows for a more comprehensive understanding of the forces acting on a structural element. It also helps in designing and analyzing structures to ensure they can withstand forces from multiple directions.

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