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Bending of plate with addition of stiffener

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BAGW

Structural
Jul 15, 2015
392
Hi,

Attached is the image below showing two scenarios. The first one is applying point load on the flange and the Beff that can be used for capacity calculation.

Mu = P x a
S = beff x t^2 / 6
Mc = phi x fy x S

Second image is the scenario with stiffener added. How do we calculate the capacity for such cases?
Document1_fpdxmg.jpg


Thanks
 
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I would do yield line assessment for both cases.

A stiffener acts as a support for yield line solution.
 
You won't have cantilever flange bending issue any more. The closer to the stiffener, the more two way plate action. I wouldn't bother to check the local stress, but to check the entire cross section.
 
Check SCI P398 [download from link], it has a method for evaluating the critical yieldline with/without influence of stiffeners that could be used.
 
If I couldn't get the stiffener more or less under/beside the load, I'd be inclined to not bother, at least not analytically. The difficulty with the yield line approach for a situation like this is that it assumes the plastic availability of longitudinal flange stresses that are simultaneously required for general flexure and warping torsion.
 
@ Agent666 which version are you referring to? I am looking at AISC 360 V15 and I cannot find it on the page you are referring to.
 
Why not put a stiffener on both sides of the load?

“Any idiot can build a bridge that stands, but it takes an engineer to build a bridge that barely stands.”
 
Do a search for SCI P398...

Rather than think climate change and the corona virus as science, think of it as the wrath of God. Feel any better?

-Dik
 
There is a link on the page I linked to to this file SCI P398.

While based on Eurocodes, the method can be applied to any other region/code.
 
A yield line method (like the others have suggested) would be good. AISC has a equation [i.e. J10-1 in the 13th ed.] for the allowable force on a flange for a beam. You have to keep in mind that force is for the full flange width....so you have to break out the % of that force meant for flange bending. I'd read the commentary for that part as well.

 
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