Calculating Bending Stress for a Cantilever Beam

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SUMMARY

The discussion centers on calculating bending stress for a cantilever beam with a point mass of 347.4 oz. at its tip, a distance of 2 inches from the support, and a radius of 1/8 inch. The initial calculation using the formula for bending stress resulted in an implausible value of approximately 450,000 psi. The correct approach involves using the formula S = W*L/Z, where Z is the section modulus, yielding a maximum stress of 28,308.7 psi for the beam.

PREREQUISITES
  • Understanding of cantilever beam mechanics
  • Familiarity with bending stress calculations
  • Knowledge of section modulus and second moment of inertia
  • Basic principles of material strength
NEXT STEPS
  • Research the calculation of section modulus for different beam shapes
  • Learn about the significance of the second moment of inertia in structural engineering
  • Explore the effects of point loads on cantilever beams
  • Study advanced bending stress analysis techniques for various materials
USEFUL FOR

Mechanical engineers, structural engineers, and students studying beam mechanics will benefit from this discussion, particularly those focused on bending stress calculations in cantilever beams.

NuclearPink
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Hi, I'm trying to calculate bending stress for a cylindrical beam. I'd like to have my result double checked because I got an answer that doesn't make sense to me. All of this is personal research, so I'm not very confident in my answer.

It's a cantilever beam with a point mass of 347.4 oz. on its tip. The distance from the load to the other end is 2 in., and the beam has a radius of 1/8". This is the calculation I found for bending stress:

bending stress (psi) = bending moment (lbs. in.) * distance from load to edge (in.) / second moment of inertia (in^4)

I researched the second moment of inertia to be (pi/4)*r^4 for a solid cylinder. So I plugged that in...

((21.7125 lbs. * 2 in.) * 2in.) / (pi/4 * (1/8 in.)^4)

...and got a result of about 450,000 psi. This feels like way too high a number, so I'd like to know what I'm doing wrong here. Thank you!
 
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I am not sure why you doubled the load W and used the second moment of inertia.

What you will find in any engineering reference is that you should be using the formula S = W*L/Z for the max stress at the base attachment point where Z is the section modulus and for round bar Z = π*d^3 / 32 = π*(2*r)^3 / 32. By doing so you will get an answer of 28,308.7 psi.
 

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