Bending Stress in Top of T-Beam

AI Thread Summary
The discussion focuses on calculating the maximum bending stress in a T-beam subjected to an 80 kg point load. Initial calculations yielded a bending stress of 2.573 GPa, which was deemed too high for steel, prompting a reevaluation. After correcting the moment arm and the moment of inertia, a new bending stress of 88.29 MPa was calculated. Participants emphasized the importance of ensuring calculations align with the material's allowable stress to avoid permanent deformation. The need for clarity regarding the load application and its eccentricity was also highlighted.
tsslaporte
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Homework Statement



T-Beam is Steel with E=200GPa

Find Max bending stress MC/I (right side where no glue)[/B]
MxcOwAK.png

80KG Load at Point "A" shown on the Top view

Blue stuff is glue, the right side has no Glue, so its just empty space

2. The attempt at a solution

I = BH^3/12 , where B = 0.04m H = 0.004
So I = 2.13 * 10^-10 m^4
C = 0.029m
M = 784.8 N * 0.024m = 18.8352 n-m

Solving that out I get 2.573 GPa which seems too high as steel can only see in MPa of stress.

So I'm not sure if the number I got is correct or I did something wrong with my calculation.
 
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MxcOwAK.png


The Beam is Supported in the center.

The Bending is happening not on the axis I assumed, the force is not in the center so

I = 0.08* 0.004^2 and C = 0.002

Now I get 88.29 MPa
 
tsslaporte said:
MxcOwAK.png


The Beam is Supported in the center.

The Bending is happening not on the axis I assumed, the force is not in the center so

I = 0.08* 0.004^2 and C = 0.002

Now I get 88.29 MPa

It's not clear what you are trying to do here. What is this point load and why is it applied to the flange of the beam?

Your expression for I seems to be incorrect, or at least it is unfamiliar to me. Have you checked to make sure the units make sense?

Your calculated bending stress values lack meaning if you don't know what stress the beam material is capable of withstanding without permanent deformation.
 
SteamKing said:
It's not clear what you are trying to do here. What is this point load and why is it applied to the flange of the beam?

Your expression for I seems to be incorrect, or at least it is unfamiliar to me. Have you checked to make sure the units make sense?

Your calculated bending stress values lack meaning if you don't know what stress the beam material is capable of withstanding without permanent deformation.

Hey,

The Beam is rigidly held in place except for the right side, so can assume a simple beam,(Square/rectangle) so I= BH^3/12 is correct.

I actually am still wrong, there is a moment in the y and x, I need to add them to find total bending stress.
 
tsslaporte said:
Hey,

The Beam is rigidly held in place except for the right side, so can assume a simple beam,(Square/rectangle) so I= BH^3/12 is correct.

I actually am still wrong, there is a moment in the y and x, I need to add them to find total bending stress.
I don't think I'd worry too much about the eccentric 'point' load a few mm off center in the y direction . I'd do it as you had in your original post after correcting the 'c' distance to .002m and checking your steel allowable stress for the material being used, as SteamKing noted .
 
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