Deflection simply supported beam

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    Beam Deflection
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Discussion Overview

The discussion focuses on finding an expression for the deflection at midspan of a simply supported beam subjected to two triangular loads on each side. Participants explore the mathematical formulation and integration process involved in deriving the deflection equation.

Discussion Character

  • Homework-related
  • Mathematical reasoning

Main Points Raised

  • The initial poster presents an expression for deflection and describes their integration process for calculating midspan deflection.
  • One participant questions whether the initial poster should have multiplied their result by 2, suggesting that this is necessary for correctness.
  • The initial poster clarifies that they did not multiply by 2 but still arrived at what they believe is the correct answer, prompting further inquiry into their method.
  • Another participant points out potential errors in the expression for qx and notes discrepancies in the domains used for Mx and mx in the integration process.
  • The initial poster acknowledges corrections to their calculations, indicating an effort to clarify their approach.
  • A later reply affirms the correctness of the answer provided by the participant who questioned the initial poster's method.

Areas of Agreement / Disagreement

Participants express differing views on the correctness of the integration approach and the necessity of multiplying by 2. The discussion includes corrections and refinements but does not reach a consensus on the initial poster's method.

Contextual Notes

There are unresolved issues regarding the compatibility of the domains used in the integration process and the correctness of the expressions for the loads.

raymanmusic
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Homework Statement


How do I find an expression for the deflection at midspan of this beam? The beam is simply supported and there is two triangular loads on each side of the beam.

Illustration of problem: http://goo.gl/gk68Fl

Homework Equations


Deflection = \Delta = \int \frac{Mx*mx}{EI}
Elastic curve equation of the simply supported beam for this case:
\delta = \frac{Qx}{960LEI}(5L^2-4x^2)^2

The Attempt at a Solution


I found Mx and mx, and I integrate from \frac{L}{2} to L. My answer is: \frac{QL^4}{120EI}.
 
Last edited by a moderator:
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raymanmusic: After you integrated from 0.5*L to L, did you multiply by 2? You must multiply by 2, which I think you did, because your current answer in post 1 is correct.
 
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Actually I did not multiply by 2, but I still got the correct answer. What did I do wrong?

Attempt at a solution: http://goo.gl/qFYMoG
 
Last edited by a moderator:
raymanmusic: First, your expression for qx currently looks wrong.

Secondly, your domain (0.5*L, L) for mx looks different from your domain for Mx. But then you combine these two incompatible domains in your integral. Or are you seeing a novel approach I did not envision yet?
 
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Thanks! I've made some corrections to my calculations. I think it's easier to understand now.

Attempt at solution: http://goo.gl/qFYMoG
 
Last edited by a moderator:
Excellent work, raymanmusic. Your answer is correct.
 

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