Deflection of a beam with non-uniform section

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Discussion Overview

The discussion focuses on how to determine deflections at force acting points in a non-uniform beam. Participants explore various methods and formulas related to beam deflection, particularly in the context of applying loads at multiple points on the beam.

Discussion Character

  • Technical explanation
  • Debate/contested
  • Mathematical reasoning

Main Points Raised

  • One participant inquires about the method for finding deflections in a non-uniform beam and provides a figure for context.
  • Another participant questions whether the inquiry is related to homework and suggests that understanding previous attempts would clarify the help needed.
  • A participant clarifies that the question is not homework and describes their attempts using formulas for uniform beams, detailing the deflection formulas used for loads applied at midspan.
  • One participant suggests looking into singularity functions and provides a link to an example involving a stepped shaft.
  • Another participant offers a method involving beam elements and discusses treating the non-uniform beam as two separate beam problems with constant cross sections, emphasizing the need for matching boundary conditions.

Areas of Agreement / Disagreement

Participants present multiple approaches to the problem, indicating that there is no consensus on a single method for solving the deflection of a non-uniform beam. The discussion remains unresolved with competing views on the best approach.

Contextual Notes

Participants have not fully explored the implications of using singularity functions or the complexities involved in matching boundary conditions between different beam sections. There may be additional assumptions or limitations not explicitly stated in the discussion.

vichu_vv
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Hello all,
How to find deflections at force acting points in a non-uniform beam?. Please look at the figure. Thank you.

Best regards
 

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Is this homework? We cannot ethically solve the problem for you, but knowing more about what you have tried already will help us see what you need help with.
 
No, this is not a homework. I have tried with uniform diameter to the whole length of the beam. I am applying loads simultaneously at positions of 1 and 2. I have gone thro the following formulas to find the deflections at 1 and 2 with only one force at a time.

fFi = fFi1 + fFi2

i - load position
1 - deflection at position 1
2 - deflection at position 2

Deflection formula when loads at midspan: (used uniform dia.)
y(x) = (Fx^2/6EI)*(3a-x) for 0<x<=a
y(x) = (Fa^276EI)*(3x-a) for a<x<=l

 
Thank you. Anymore links or supports from you to make me more clear. Thanks
 
The easy way to solve this problem is with beam elements. Failing that, the way to solve it is to consider two beam problems, where each beam is of constant cross section. The loads from the beam on the right can be transferred to produce and equivalent shear and moment at the interface to load the beam on the left. Then the boundary conditions between the two problems have to be matched to assure displacement and slope continuity across the interface. It is a messy problem, but it is entirely doable.
 

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