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

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SUMMARY

The calculation of strain energy in beams using integral equations requires understanding the bending moment function M(s) with respect to the beam's length coordinate. The strain energy U is defined by the integral U = ∫(M²(s)/(2EI)) ds, where EI is the flexural rigidity. For accurate results, M(s) must be squared term-by-term based on the bending moment diagram, which varies along the length of the beam. The correct application of this method resolves discrepancies in calculated strain energy, as demonstrated in the discussion.

PREREQUISITES
  • Understanding of bending moment diagrams
  • Familiarity with integral calculus
  • Knowledge of beam theory and flexural rigidity (EI)
  • Ability to derive M(s) for different loading conditions
NEXT STEPS
  • Study the derivation of bending moment functions for various beam types
  • Learn how to construct and interpret bending moment diagrams
  • Explore advanced integral calculus techniques for evaluating definite integrals
  • Investigate the effects of varying load conditions on strain energy calculations
USEFUL FOR

Structural engineers, civil engineering students, and professionals involved in beam analysis and design will benefit from this discussion, particularly those focused on calculating strain energy in structural components.

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?
OcWeW.jpg
 
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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?
OcWeW.jpg

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:

cantilever1.JPG

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:

2000px-Shear_Moment_Diagram.svg.png

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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