Deflection of a Beam using Double Integration

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Discussion Overview

The discussion revolves around determining the maximum deflection of a simply supported beam subjected to concentrated couples using the double integration method. Participants explore the formulation of the moment function and the application of boundary conditions in the context of beam deflection analysis.

Discussion Character

  • Homework-related
  • Mathematical reasoning
  • Technical explanation

Main Points Raised

  • One participant outlines the problem setup, indicating the beam's geometry and the application of couples, while expressing uncertainty about how to start the analysis.
  • Another participant suggests using shear and moment diagrams to calculate the moment function M(x), noting that there appears to be no shear along the beam and a constant moment between the applied couples.
  • A participant expresses confusion about deriving M(x) and mentions a known maximum deflection value of (5(C)(a^2))/(8EI), which they believe should be achievable through double integration.
  • Further clarification is provided regarding the moment function, with a breakdown of M(x) across different segments of the beam, emphasizing the importance of correctly applying boundary conditions for integration.
  • One participant references an external post that discusses the same problem, suggesting a potential overlap in solutions or approaches.

Areas of Agreement / Disagreement

Participants express differing views on the correct formulation of the moment function and the resulting maximum deflection. There is no consensus on the approach to take or the correctness of the derived values, indicating that multiple competing views remain.

Contextual Notes

Participants note challenges in deriving the moment function and applying boundary conditions correctly, with some expressing uncertainty about their calculus skills. The discussion reflects a reliance on previous examples and external resources, which may influence the understanding of the problem.

voodoonoodle
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Homework Statement



Need to determine the maximum deflection of the beam, by using double integration, and EI is constant.

...>...<
_______(_______)_______
^........o
|<--a-->|<--a-->|<--a-->|

Tried to draw this the best I could. It is a simply supported beam, with a concentrated couples of equal value (C) but opposite direction, with a distance between of (a).

Homework Equations



I pretty sure that my boundary conditions are: v=0 @ x=0 and v=0 @ x=3a

and my max. deflection will occur at x=(3/2)a

The Attempt at a Solution



My problem is that I don't know how to get started, all the examples show only one concentrated moment. I'm assuming I have no reactions, because when I sum the moments around either side, the moments cancel out.

I have tried using that M=C(x-a) and that didn't come out correct. So basically I'm looking for help in trying to get the moment function.

I have also tried M=C where I get the following

slope as a function of x = Cx/EI + C1
deflection as a function of x = Cx^2/2EI + C1x + C2

boundary conditions:
v=0 @ x=0 so C2 = 0
v=0 @ x=3a so C1 = (-3(C)(a))/(2EI)

so then I come up with an answer of (-9(C)(a^2))/(8EI) for the max deflection using x=(3/2)a
 
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Well, it's been way too long since I used the double integration method, but it does bring back some haunting memories. If you're looking at y" =M(x)/EI, my suggestion would be to calculate M(x) using shear and moment diagrams. Looks to me like you've got no shear at all anywher along the beam, and just a constant moment of c in between the two applied couples, and no moment on either side of those couples to the support points.
 
PhantomJay, that is correct. I'm just not sure how to come up with M(x). I have tried several things for it but still can't get the answer they give for Max Deflection. Which I know to be (5(C)(a^2))/(8EI).
 
voodoonoodle said:
PhantomJay, that is correct. I'm just not sure how to come up with M(x). I have tried several things for it but still can't get the answer they give for Max Deflection. Which I know to be (5(C)(a^2))/(8EI).
Well, M(x) =0 between 0 and a; M(x) = C between a and 2a; and M(x) = 0 between 2a and 3a. Now double integrate and use proper boundary conditions , which is probably what you're trying to do. I think the key is to deternine the boundary conditons. I've been relying on tables and charts, so my calculus is a bit rusty at this point.
 
What a coincidence, I found this post: http://forums.mathalino.com/general-engineering-sciences/strength-of-materials/beam-deflection-by-double-integration-method" . It is exactly the same problem as this one.
 
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