Deflection at any point formula

In summary, RMXByker is seeking assistance on determining the precise stress at any point along a beam. They have the deflection at every point and are looking for an easy way to relate this back to stress. A discussion on the relationship between deflection and internal moment, as well as the difficulty of determining all stress at every point in the beam, ensues. A MathCAD sheet is attached to aid in solving the problem, but there is some difficulty in copying it to Physics Forums.
  • #1
RMXByker
1
0
Good Afternoon Everyone,

I am need of a little assistance. I am working on determing the precise stress at any point along a beam and would like a little help. I know the deflection at every point and would like an easy way to relate this back to stress. Any help?

[PLAIN]http://sphotos.ak.fbcdn.net/hphotos-ak-snc3/hs358.snc3/29503_523051459059_53800516_30961326_1066764_n.jpg

Let me know your thoughts,
RMX
 
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  • #3
Hey RMXByker,

It is a good question and Studiot provided you a good link talking about the relationship between deflection and internal moment. With this equation, however, you are assuming small angle deflection, so be sure you remember that everything I am about to say only applies for small angle deflection.

Also, to determine all stress at every point in the beam would be almost impossible. I am going to interrupt that you are looking for the bending stress distribution (ignoring all shear stresses). Please correct me on what you are looking for if this is wrong.

In the attached document (cause I can't seem to make the build in TeX to work), I have made up a little sheet for you. I hope it helps.
 

Attachments

  • PFhelp0001.pdf
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  • #5
I solve a very similar problem in this thread:

Did your formula in that thread come from MathCad?
I can't get it to work with PF
 
  • #6
Studiot said:
Did your formula in that thread come from MathCad?
I can't get it to work with PF

The last attachment I posted is basically a fully symbolic derviation of the beam bending formula using the integration procedure. MathCAD did all the heavy lifting for me in terms of symbolic manipulation, but it can at least give you an idea of what you're in for (a lot of work).

You'll end up having to split the beam into three sections, integrate three times for each section, and then solve a system of 9 equations with 9 unknowns at the end. It's not pretty. A pdf of the MathCAD sheet you'll be most interested in is attached to the following post:

https://www.physicsforums.com/showpost.php?p=1600375&postcount=19

The integration tree you'll need is as follows:

[tex]\nu''''=\frac{q(x)}{EI}[/tex]

[tex]\nu'''=\frac{V(x)}{EI}[/tex]

[tex]\nu''=\frac{M(x)}{EI}[/tex]

[tex]\nu'=\theta(x)[/tex]

[tex]\nu=\delta(x)[/tex]
 
  • #7
Thank you, I know how to solve a beam.

I was asking how to copy from MathCad to Physics Forums.
At present I use MathType, but this has no word processor or picture (graph) capabilities.
 
  • #8
One thing that will make your problem more difficult is you won't be able to make the assumption that your max deflection & bending moment will always be in the middle. You'll also have to think about what you want to do about cases where a is near one side of the beam or the other.
 
  • #9
Studiot said:
Thank you, I know how to solve a beam.

I was asking how to copy from MathCad to Physics Forums.
At present I use MathType, but this has no word processor or picture (graph) capabilities.

You can't directly copy MathCAD to PF, you have to print the MathCAD sheet to pdf and attach the pdf file.
 

FAQ: Deflection at any point formula

What is the formula for deflection at any point?

The formula for deflection at any point is given by: D = (Px^2)/2EI, where D is the deflection at any point, P is the applied load, x is the distance from the fixed support, E is the modulus of elasticity, and I is the moment of inertia.

How is the formula for deflection at any point derived?

The formula for deflection at any point is derived using the Euler-Bernoulli beam theory, which states that the deflection of a beam is directly proportional to the applied load and inversely proportional to the stiffness of the beam.

What are the units of measurement for the variables in the deflection formula?

The units of measurement for the variables in the deflection formula are as follows: D is measured in meters (m), P is measured in Newtons (N), x is measured in meters (m), E is measured in Pascals (Pa), and I is measured in meters to the fourth power (m^4).

Can the deflection formula be used for all types of beams?

The deflection formula can be used for most common types of beams, such as simply supported beams, cantilever beams, and fixed beams. However, for more complex beam designs or for beams made from non-uniform materials, the formula may need to be modified or other methods of analysis may need to be used.

How accurate is the deflection formula?

The deflection formula provides a good estimate of the deflection at any point on a beam, but it is not always exact. Factors such as material properties, beam geometry, and boundary conditions can affect the accuracy of the formula. It is always important to consider these factors and use appropriate safety factors when using the deflection formula in real-world applications.

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