How do I determine the K value from a cantilever beam deflection test?

AI Thread Summary
To determine the K value from a cantilever beam deflection test, the bending moment and stiffness need to be calculated accurately. The bending moment is correctly calculated as 1.225x10-3 Nm with a 4.9N point load applied at 0.25m from the hinge. The moment of inertia (I) for a rectangular beam is also correctly calculated, but the calculation of the distance (y) to the neutral axis is crucial for determining stress. The stiffness (K) can be found as the inverse of the deflection under a unit point load, which is related to the beam's dimensions and loading conditions. Accurate unit measurements and understanding of beam mechanics are essential for precise calculations.
Jason24
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Hi,

I am new to this type of material and am hoping that someone may be able to assist me.

In short I am putting a cantilever beam under test to determine its bending moment and stiffness (K value) in order to get a strain reading that can be related to an exact model in solid works.

The cantilever beam is 0.26m long and a weight is applied at 0.25m. It is obviously hinged at one end and has a point load of 4.9N (at 0.25m).

I have calculated a bending moment of 1.225x10-3 by summing -(0.0049)(0.25). I believe this is right?

From this I am trying to determine strain behaviour via M/I=Sigma/y

I have calculated I from bh3/12 as it is a rectangle giving me 43.94x10 6. Again I believe this is correct?

For the stress I assume I simply put the 4.9N that I applied? And I am unsure on how to calculate y?

Also how do i determine the K value from this?
It may also be worth mentioning that I have used a DTI to calculate a deflection of .11mm under loading

I appreciate any help, I am new to all of this and appreciate your patience

cheers,
Jason
 
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If this is a homework question you have posted in wrong forum. Deflection of a cantilever under a point load P applied a distance L from the fixed support can be found in tables or determined from the calculus, where the stiffness is the inverse of the deflection under a unit point load. Watch your units is the load in N or kN? What are the beam dimensions ? Max stress occurs at extreme outer fibers at fixed end and where y for max stress location is the distance to the neutral axis .
 
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