Beam deflection and curvature radius formula doubts

In summary, the equation for deflection of a simple-supported beam with force applied in the middle is derived using two equations: the first is the curvature radius multiplied by the length of the beam, and the second is the cosine of the angle between the force vector and the beam's original direction.
  • #1
FEAnalyst
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TL;DR Summary
What is the source of this formula for beam deflection based on curvature radius?
Hi,

I am working with leaf springs and studying the derivation of the formula for the deflection of such a structure. The derivation is shown here:



My only doubt is how to obtain the following formula: $$\delta=\frac{L^{2}}{8R}$$ where: ##\delta## - deflection, ##L## - length of the beam, ##R## - curvature radius. The beam under consideration is simply-supported with force applied in the middle. I haven't found such a simple equation anywhere. How is it derived ?
 
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  • #2
It‘s geometry. There are two equations:
Rθ=L/2
(R-δ)/R=1-δ/R=cosθ≈1-θ2/2

Arc Length Dark2.png
 
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  • #3
Thank you for quick reply. Those equations indeed give the formula from my post: $$1- \frac{\delta}{R}=1-\frac{(\frac{L/2}{R})^{2}}{2}$$ But how to formulate them? The geometry is just this, right? https://wikipedia.org/wiki/Circular_segment
 
  • #4
I added a picture.
 
  • #5
So ##L## in your equations is arc length (length of a bent beam)? In my case, it’s chord length (length of a straight beam). How does it affect the formula from my first post?
 
  • #6
I haven’t done theory for a while, so it took me a while to figure it out.

Using your geometry
R2= (L/2)2 + (R-δ)2
neglect terms of δ2
 
  • #7
I’ve found a nice derivation in another YouTube video:

IMG_0309.jpeg


I just don’t get why ##\delta^{2}=0##.
 
  • #8
Another way is to make the assumption that R is large compared to L,δ (as opposed to δ is small compared to R, L)
If you do not neglect δ2, you get

δ/R=1±√(1-L2/4R2)
≈1±(1-L2/8R2)
The sum violates the assumption, the difference gives the answer.

I am not familiar enough with the system to figure out which assumption.
 
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  • #10
All right, so ##\delta^{2}## is just neglected as a small value (since we assume small deformations). Thank you very much for your help.
 
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  • #11
Unless I'm missing something, I don't think they can do what has been done for the entire leaf spring. I'm thinking it is for a single leaf, and it's not going to be a good predictor of the deflection entire leaf spring system.

Take for example the simple 2 leaf system:

1681481597766.png


We can apply Castigliano's Theorem to find the deflection at ##C##, which says in general:

$$ \delta = \int \frac{M}{EI}~\frac{\partial M}{ \partial P} ~dx \tag{1} $$

$$ \delta_C = \delta_{AC}+\delta_{BC} \tag{2} $$

Due to symmetry, we can say that the contributions to the deflection at C integrating from ##A \to C## and ##B \to C## are equal, hence:

$$ \delta_C = 2 \delta_{AC} $$

Let the spatial coordinate ##x## start from ##A##:

The moment as a function of ##x## is given by:

$$ M(x) = \frac{P}{2}x \tag{3} $$

$$ \implies \frac{\partial M}{ \partial P} = \frac{1}{2}x \tag{4} $$

Substitute (2),(3) and (4) into (1):

$$\delta_C = 2 \delta_{AC} = 2 \left[ \int_0^a \frac{ \frac{P}{2}x}{EI} ~\frac{1}{2}x ~dx + \int_a^{2a} \frac{ \frac{P}{2}x}{2EI} ~\frac{1}{2}x ~dx \right] $$

Simplifies to:

$$ \begin{aligned} \delta_C &= \frac{2P}{EI} \left[ \frac{1}{4} \int_0^a x^2 ~dx + \frac{1}{8} \int_a^{2a} x^2 ~dx \right] \\ \quad \\ &= \frac{2P}{EI} \left[ \frac{1}{12} \Bigg. x^3 \Bigg|_0^a + \frac{1}{24} \Bigg. x^3 \Bigg|_a^{2a} \right] \\ \quad \\ &= \frac{3Pa^3}{4EI} \end{aligned}$$

I'm sure there is a pattern to be found for ##n## leaves, but I didn't get that far.
 
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  • #12
I also wasn’t sure about the correctness of this formula but it gives good results when compared with FEA and even experiment (described in a Polish book about leaf springs). The derivation also makes sense to me. I think that the difference between it and other common approaches is that here initial curvature of the spring and force applied to "unbend" it is assumed.
 
  • #13
FEAnalyst said:
I also wasn’t sure about the correctness of this formula but it gives good results when compared with FEA and even experiment (described in a Polish book about leaf springs). The derivation also makes sense to me. I think that the difference between it and other common approaches is that here initial curvature of the spring and force applied to "unbend" it is assumed.
It’s hard to say why it works. In my opinion the theory being applied in those videos should not be sound for a generalization. It’s hard to tell what they are saying though as it seems to mostly in a language other than English.

For the following generalization with 3 leaf's I get (applying the theory above):

1681506949467.png


$$\delta_C = \frac{P}{2EI} \left( \frac{11}{18}a^3+ \frac{1}{72}l^3 \right) $$

I'm not seeing how they could be equivalent.
 
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  • #14
Do over.

I was little hasty in defining the moments of inertia for each section. The above analysis isn't wrong per-se ( as far as I can tell ), its just they don't represent leaf plates of the same height in each layer.

This should be more like what's encountered with the addition of the same rectangular plate in each layer:

1681515616682.png
$$\delta_C = \frac{P}{2EI} \left( \frac{37}{72}a^3+ \frac{1}{648}l^3 \right) $$

with the condition ##a < \frac{l}{4}##

Sorry if that caused any confusion.
 
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FAQ: Beam deflection and curvature radius formula doubts

What is the formula for beam deflection?

The formula for beam deflection depends on the type of beam and loading conditions. For a simply supported beam with a central point load, the maximum deflection (δ) can be calculated using δ = (P * L^3) / (48 * E * I), where P is the load, L is the length of the beam, E is the modulus of elasticity, and I is the moment of inertia.

How do you calculate the curvature radius of a beam?

The curvature radius (R) of a beam is related to its deflection and can be calculated using the formula R = EI / M, where E is the modulus of elasticity, I is the moment of inertia, and M is the bending moment. Alternatively, for small deflections, it can be approximated as R ≈ 1 / (d^2y/dx^2), where y is the deflection and x is the position along the beam.

What factors affect beam deflection?

Beam deflection is affected by several factors including the type and magnitude of the load applied, the length of the beam, the material properties (modulus of elasticity), and the geometric properties (moment of inertia) of the beam's cross-section.

How does the moment of inertia influence beam deflection?

The moment of inertia (I) is a measure of a beam's resistance to bending and is dependent on the cross-sectional shape and size of the beam. A higher moment of inertia indicates a stiffer beam that will deflect less under a given load, while a lower moment of inertia indicates a more flexible beam that will deflect more.

Can beam deflection be minimized, and if so, how?

Yes, beam deflection can be minimized by increasing the moment of inertia (e.g., by choosing a beam with a larger or more efficient cross-sectional shape), using a material with a higher modulus of elasticity, reducing the length of the beam, or distributing the load more evenly along the beam rather than concentrating it at a single point.

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