Calculating Maximum Bending Stress in Beam w/Varying Cross Section

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SUMMARY

The discussion focuses on calculating the maximum bending stress in a beam with a varying cross section using the equation σ = M/Sx. The term Sx is identified as the section modulus, defined as Sx = I/ymax, where I is the moment of inertia and ymax is the distance from the neutral axis to the outermost fiber. Participants clarify that for beams with varying cross sections, the moment of inertia should be evaluated at the specific cross section of interest, as the maximum stress may not occur at the same location as the maximum bending moment.

PREREQUISITES
  • Understanding of bending stress and the equation σ = M/Sx
  • Familiarity with moment of inertia (I) and its calculation
  • Knowledge of the neutral axis in beam theory
  • Concept of section modulus and its application in structural engineering
NEXT STEPS
  • Research the calculation of moment of inertia for various cross-sectional shapes
  • Learn about the implications of varying cross sections on bending stress
  • Explore design rules involving section modulus in structural applications
  • Study the relationship between bending moment and stress distribution along beams
USEFUL FOR

Structural engineers, mechanical engineers, and students studying beam theory and stress analysis will benefit from this discussion, particularly those dealing with beams of varying cross sections.

zzinfinity
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Hi,
I'm trying to calculate the maximum bending stress in a beam with a varying cross section. I found a great resource (link below) that gives examples on how to do this but am a little confused. Basically the equation used is σ=M/Sx I know what σ and M are, but I haven't a clue what Sx is meant to be. Can anyone tell me what this is? It's kind of tough to figure our a way to google "S" and get meaningful results. Thanks!

http://www.aaronklapheck.com/Downloads/Engr112_Handouts/ENGR112%20Solutions/05-03ChapGere%5B1%5D.pdf

PS. What I'm trying to do, is calculate the maximum stress of a boat hull. I'm approximating it as a beam, but the cross section geometry is arbitrary. If anyone has any suggestions about a better way to do this, they are certainly welcome!
 
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The general formuila is $$\sigma = \frac{My}{I}$$ where y is the distance from the neutral axis.

It looks like he is combining ##I## and the maximum value of ##y## into $$S_x = \frac{I}{y_{\text{max}}}.$$ I've never seen that notation before, but then I learned how to stress beams a very long time ago!

Edit: in one of the problems in the PDF he gives it the name "section modulus". http://en.wikipedia.org/wiki/Section_modulus. Looking at the references on the Wiki page, maybe it's used more as a civil or structural engineering term than in general mech eng.
 
Last edited:
AlephZero said:
The general formuila is $$\sigma = \frac{My}{I}$$ where y is the distance from the neutral axis.

Thanks for you help. So if I have a beam with a varying cross section (and therefore a variable I) how do I deal with that? Can I just find I at the cross section I want to know the stress at? Or do I need to consider the moment of inertia at other portions of the beam as well?


Also wikipedia denotes the "First moment of Area" with an S. Do you think that could be what it is? http://en.wikipedia.org/wiki/First_moment_of_area

Thanks again.
 
zzinfinity said:
So if I have a beam with a varying cross section (and therefore a variable I) how do I deal with that? Can I just find I at the cross section I want to know the stress at?

Just consider I at that cross section.

But note that for a variable section beam, the maximum stress might not be at the same place as the maximum bending moment. For example I might decrease faster than M as you move along the beam, so M/I increases.

(For a constant cross section, y and I are the same everywhere along the beam so the maximum stress position is the same as the max bending moment position.)
 
Sx is the section modulus. This number is used in some design rules when sizing plating-stiffener combinations.
 

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