Understanding the Equation for Measuring Strain on a Cantilever Beam

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    Measuring Strain
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SUMMARY

The discussion focuses on the equation used to measure strain on a cantilever beam, specifically when held stationary at one end. The key equation derived is strain = (3L1)(t)(deformation) / (2(L2)^3), where L1 is the length from the free end to the measurement point, L2 is the total length, and t is the thickness of the beam. The end deformation of a cantilever under load P is given by δ = PL^3 / (3EI), and the strain in bending mode is expressed as ε = My / EI = Mt / (2EI). Resources for further understanding include online coursework and specific texts on beam bending and elasticity.

PREREQUISITES
  • Understanding of cantilever beam mechanics
  • Familiarity with strain and deformation concepts
  • Knowledge of the moment of inertia (I) and Young's modulus (E)
  • Basic calculus for differential equations
NEXT STEPS
  • Study the derivation of the deformation equation in beam theory
  • Explore online courses on beam bending mechanics
  • Read "Mathematics Applied to Continuum Mechanics" by Segel
  • Investigate "Theory of Elasticity" by Landau and Lifshitz (vol. 7)
USEFUL FOR

Mechanical engineers, civil engineers, and students studying structural analysis or materials science will benefit from this discussion, particularly those focused on the mechanics of materials and beam theory.

JSBeckton
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I have a lab where we used the following equation to theroretically measure the strain on a cantilever beam heald stationary at the left end. Measuring back from the right side its length is L2 and the length from the free (right) end to the point where the strain gagues were was L1

(fixed end)________________________(free end)

L2=whole length
L1=length from free end to measured point.
t=thichness

strain=(3L1)(t)(deformation)
______ 2(L2)^3

I know the equation for strain is deformation over L2 but can't seem to wrap my head around how they derived this equation.

Any help would be greatly appreciated, thanks in advance.
 
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The end deformation of a cantilever loaded by force P is

\delta=\frac{PL^3}{3EI}

The strain on the surface of a beam in bending mode is

\epsilon=\frac{My}{EI}=\frac{Mt}{2EI}

where the moment M is

M=L_1P

Put these together and you'll have the equation you were trying to derive.
 
Thanks a lot, can't believe I didn't see that!
 
DO you know where I can find a derivation of the deformation equation?

Thanks
 
Lots of places. Try:

online course work:
http://www.clarkson.edu/class/es22201/
(chapter 9 is beam bending)

Mathematics applied to continuum mechanics, Segel
Theory of elasticity, Landau and Lif****z (vol. 7)

The original equation is a 4-th order inhomogeneous differential expression. After simplifying (thin rod, equilibrium deformation, etc), the equation is easily solved.
 
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I got it, thanks.
 

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