Calculating Beam Deflection and Failure Load for Plywood Beam Design

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Homework Help Overview

The discussion revolves around calculating beam deflection and failure load for a plywood beam design in an engineering context. The original poster is tasked with determining how far a beam made of laminated plywood will deflect under a load and what load will cause it to fail, with specific dimensions and properties provided.

Discussion Character

  • Exploratory, Assumption checking, Conceptual clarification

Approaches and Questions Raised

  • The original poster attempts to apply formulas for deflection and moment of inertia but expresses uncertainty about how to find the load that causes failure. Some participants suggest looking up the material's maximum bending stress and using it to calculate the maximum moment, which can then be related back to the load.

Discussion Status

Participants are exploring different aspects of the problem, including the necessary material properties and the relationships between stress, moment, and load. Some guidance has been offered regarding the use of bending stress and moment calculations, but there is no explicit consensus on the approach to take.

Contextual Notes

The original poster mentions difficulty in finding the necessary formulas and material properties, indicating a potential gap in resources or understanding of the subject matter. There is also a note about waiting for a response from the professor, suggesting time constraints in the discussion.

sol_angel187
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Hey, this is my first post on this forum- I hope that someone can help me because I'm going crazy! I'm an architecture student taking a required engineering class, and it's pretty challenging for me. So anyway, here's my problem.

We were assigned to design a beam made of luam plywood out of a sheet 24" x 8" x 1/4". I decided to cut the plywood into (4) 2" pieces and use wood glue to glue them together so it's dimensions are 1"x2"x24". The assignment is to to say how far the beam will deflect, and what load will cause the beam to fail. We will test it in class on a machine. It will be simply supported on each end and a load will be placed in the center.

So, the formula I think I need to use for deflection is

D=P(L^3)/48EI

d= deflection
p= load
l= length
e= modulus of elasticity
I= moment of inertia

I=b(d^3)/12

b=base
d=depth

so I= (1)(2^3)/12=.667
I found the modulus of elasticity for luam plywood on the internet (after an hour of looking) and it is 1,500,000
L= 24

so I know I, E, and L, but I still have two unknowns, P and D. The problem is I don't know another fomula to figure out what P is. I'm going slightly crazy because I can't find it in the book, and I've been looking online for a long time. I'd really appreciate it if someone could point me in the right direction! thanx!
 
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anyone?

I emailed my professor this yesterday and he still hasn't emailed me back yet . . .
 
First, you have to know the stress 's' at which the material fails, which you have to simply look up. That's the maximum bending stress that the beam can take so put it into the famous formula M/I = E/R = s/y where 'y' is the distance from the neutral axis. Set this to be half the depth of the beam, i.e where the stress will be greatest. That'll tell you the maximum moment it can take. Calculate the value of the load P to generate such a moment and then put this into your equation for the deflection.
 
thanx for your help- i think i got it!
 

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