Torque and Bending: How Force Affects Bending Length

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SUMMARY

The discussion focuses on the relationship between torque and bending in cantilever beams, specifically addressing how force affects bending length. It establishes that for small deflections, the maximum deflection of a cantilevered beam can be calculated using the formula δ_{max} = \frac{PL^3}{3EI}, where P is the load, L is the length, E is the modulus of elasticity, and I is the moment of inertia. The conversation highlights that while small deflections exhibit a linear relationship with applied force, larger deflections lead to non-linear behavior, necessitating strain calculations to determine the transition point.

PREREQUISITES
  • Understanding of classical beam theory
  • Familiarity with the modulus of elasticity (E)
  • Knowledge of moment of inertia (I) calculations
  • Basic principles of torque and force application
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  • Research the implications of large deflections in beam theory
  • Learn about the calculation of strain in materials under load
  • Explore non-linear beam theory and its applications
  • Study the effects of distributed loads on cantilever beams
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Engineers, physics students, and material scientists interested in structural analysis and the mechanics of materials will benefit from this discussion.

disgradius
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If I were to bend a cantilever by applying a certain amount of force at one end, would the distance it bends in a circle be linearly related to the torque resulting from the force? If not, would there be a measurable difference from being linear if I were to bend a, say, 0.5m long object with less than 20N? Thanks in advance! :D
 
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Its going to matter what the modulus of the material is, and what is the stress in relation to the yield strength. How is the beam supported, where are the loads, and a whole bunch of other factors.
 
For very small deflections, you can feel safe in assuming a linear relationship. However, there will be a fast approaching point that your deflection will be considered "large" in terms of classical beam theory in which case the problem become non-linear.

In classical beam theory, for small deflections, the equation for the maximum deflection of a cantilevered beam with the load applied to the very end is

\delta_{max}=\frac{PL^3}{3EI}

The deflection is linear with P, the load. This changes for a distributed load.

To determine what is a large deflection, the strains would have to be calculated. It does not take much to leave the realm of linear responses though.
 

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