A (hopefully) easy question to answer about cantilever beams

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SUMMARY

The discussion focuses on calculating the top surface stress of a standard rectangular cross-section cantilever beam subjected to a concentrated end load. The formula sigma = My/I is confirmed as applicable, where M represents the moment due to the end load multiplied by the distance from the load to the point of interest, y is half the depth of the beam, and I is the area moment of inertia. The conversation emphasizes that this formula holds true unless specific conditions such as short beam length, large deflections, or anisotropic materials are present, which may necessitate alternative approaches.

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ralphowilson
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Hi guys,

just wondering if you could help me out?

For a standard rectangular cross-section cantilever beam with a concentrated end load how do i work out the top surface stress at a point along the beam? do i just use sigma=My/I where y=half the depth of the beam and M=end load * distance from end load to point of interest ...?

This sounds right but I'm not certain..sorry, hope this is easy enough to answer.

thanks a lot!

Ralph
 
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What do you mean exactly?

If you want the flexionant stresses to the extreme fiber on compression (or tension) of the beam, M will be the corresponding moment at the distance (where you want the stresses) from the diagram (which in this case is a triangle), y will be half of the depth of the beam, and I the area moment of inertia of the beam in the axis of the acting moment.
 
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Sure, your standard formula will apply, unless there is something you didn't tell us about which means it does not apply.

For example if it is a short beam, or you want accurate stresses where a load or restraint is applied, or there are large deflections, or the material is anisotropic, or the loads are big enough to cause nonlinear material behavour, or ...
 

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