How Do You Calculate Strain Energy in Beams Using Integral Equations?

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smr101
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I can't work out the strain energy using the integral equation here, question (b)(i).

I've got the bending moment for the first beam as 400kN.

E and I are given, I'm guessing you can take '2EI' out of the integral and just integrate the M^2, is that correct?
Two beam diagrams for a strain energy problem: a cantilever 4 m long, fixed at the right, with a 100 kN downward load at its free left end; and a simply supported beam of 4 m span, pinned at the left and roller at the right, with a 100 kN downward load at midspan. Spans are labelled 2 m and 2 m.
 
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smr101 said:
I can't work out the strain energy using the integral equation here, question (b)(i).

I've got the bending moment for the first beam as 400kN.

E and I are given, I'm guessing you can take '2EI' out of the integral and just integrate the M^2, is that correct?
Two beam diagrams with 100 kN point loads: a cantilever 4 m long fixed at the right end, and a simply supported beam with 2 m spans on each side of the load. Labels include the strain energy formula U = integral from 0 to L of M^2/(2EI) ds.

To calculate the strain energy of the beams, you need to know the function of M w.r.t. the length coordinate of each beam, which is s here.

So the strain energy is more accurately represented by the following integral:

##U=\int_0^L \frac {M^2(s)}{2EI} \, ds##

If EI is a constant value over the length of the beam, it can be moved before the integral sign, like any other constant.
 
SteamKing said:
To calculate the strain energy of the beams, you need to know the function of M w.r.t. the length coordinate of each beam, which is s here.

So the strain energy is more accurately represented by the following integral:

##U=\int_0^L \frac {M^2(s)}{2EI} \, ds##

If EI is a constant value over the length of the beam, it can be moved before the integral sign, like any other constant.

This is what I thought would be the case, I did the following:

2EIU = M^2*s

U = 400,000^2 * 4 / (2 * 200x10^9 * 60.8x10^-6)

= 26.315 kJ

The solution states the answer is 8.772 kJ.

Which strangely enough is exactly a third of the answer I got it...
 
smr101 said:
This is what I thought would be the case, I did the following:

2EIU = M^2*s

U = 400,000^2 * 4 / (2 * 200x10^9 * 60.8x10^-6)

= 26.315 kJ

The solution states the answer is 8.772 kJ.

Which strangely enough is exactly a third of the answer I got it...

In each beam case, M(s) ≠ constant over the length of the beam.

Remember drawing shear and bending moment diagrams for beams with various loadings? The integral of the strain energy in bending is the area under those bending moment curves squared term-by-term, then divided by 2EI. That's the calculation you are supposed to do here.
 
SteamKing said:
In each beam case, M(s) ≠ constant over the length of the beam.

Remember drawing shear and bending moment diagrams for beams with various loadings? The integral of the strain energy in bending is the area under those bending moment curves squared term-by-term, then divided by 2EI. That's the calculation you are supposed to do here.

I'm not understand what you mean by 'squared term by term'. What terms?

Again, I've noticed for the second beam doing what I did in my last post and dividing by 3 gives the correct solution.
 
smr101 said:
I'm not understand what you mean by 'squared term by term'. What terms?
I meant point-by-point.
The bending moment curve for a cantilever beam loaded at the end is this:

Cantilever beam fixed at the left wall with a downward point load W at the free right end, span L; below it a triangular bending moment diagram labelled BMD, height WL at the wall, zero at the tip, marked -ve.

​
In order to evaluate the integral
##U=\int_0^L \frac {M^2(s)}{2EI} \, ds##
you must square the ordinates of the bending moment diagram.

Since the ordinates of this bending moment diagram vary linearly with the coordinate s, which runs along the length of the beam, you can find a symbolic expression for M(s) as a function of s and then square that expression and evaluate the integral for U.
Again, I've noticed for the second beam doing what I did in my last post and dividing by 3 gives the correct solution.

The bending moment diagram for the second beam is similar to the one below:

Three stacked diagrams of a simply supported beam with a central point load P: the beam with supports at each end and the load arrow at midspan, a blue shear diagram stepping from P/2 to -P/2, and a red bending moment diagram peaking at PL/4 at midspan.

​
Just as in the case of the cantilever beam, you can find a symbolic expression for M(s) for the simply-supported beam and use the square that expression for M(s) to evaluate the integral which gives U. In this case, it might be easier to split the integration interval 0 ≤ s ≤ L into two parts.
 
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