What Could Have Caused an Error in Experimental Buckling Load Calculation?

In summary, the conversation discusses an experimental buckling load for a compressive axial load applied to a tube of circular cross section. The buckling load is found to be 2.34% larger than the theoretical buckling load, which is considered a success. The effect of knife edges on the overall buckling load is negligible, but other factors such as imperfections in material and geometry could have caused the error. The conversation also suggests going back to review the load application and measuring situation to further understand the anomaly.
  • #1
ads.
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Hi,
I have a problem with the experimental buckling load that I have deduced for a compressive axial load applied to a tube of circular cross section. The buckling load is 2.34% larger than the theoretical buckling load! The beam is connected to supports via knife edges; these are rigid bodies and so will increase the overall buckling load of the beam. However using the correction factor deduced by Karman and Biot (1940) for this beam the buckling load is 1.000005 x P(theoretical), so the effect of hte knife edges can be considered to be negligible. What else might have caused this error? Position of strain gauges? Data acquistion program?

thanks for any help.
 
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  • #2


ads. said:
I have a problem with the experimental buckling load that I have deduced for a compressive axial load applied to a tube of circular cross section. The buckling load is 2.34% larger than the theoretical buckling load!

Ha! If you're within 2.34% of the theoretical load, I would call your experiment a success.

ads. said:
The beam is connected to supports via knife edges; these are rigid bodies and so will increase the overall buckling load of the beam. However using the correction factor deduced by Karman and Biot (1940) for this beam the buckling load is 1.000005 x P(theoretical), so the effect of hte knife edges can be considered to be negligible. What else might have caused this error? Position of strain gauges? Data acquistion program?

You're fighting for atoms in one spot when you could be off by significant margins in others. My guess is your material is not "perfect" and is slightly off either in its mechanical properties or its geometry. Being off 2% is a very small margin when comparing theoretical results to experimental results. Things like paralellism of your knife blades will have an effect on your results as well.
 
  • #3


Lol, thanks. So it looks more like general experimental errors rather than anything in particular.
 
  • #4


You can introduce more error than 2% just in the lay up and connections of the strain gauges. I would pat myself on the back for having a correlation that good.
 
  • #5


I think you guys are missing the point. He said his measured result was ABOVE the theoretical value, and that is a true anomaly. I have made quite a few buckling measurements, and I have never, ever, gotten a measured result higher than the theoretical value. I think the question is an entirely valid question, and worthy of some serious consideration.

I have to suggest that you go back over your load application/load measuring situation. Are you measuring load right on the column itself, or are you measuring it on a ram that loads the column? If on a ram, could part of the load be shunted into the support by stiction?

You definitely have a strange result that ought to be explained.
 
  • #6


I'm sorry, but in all of my years in testing, I have been in very few situations where a measurement uncertainty could not be bilateral. Perhaps you can expand more on why the uncertainty in a measurement of force can not be more than the theoretical value?

I can think of a few scenarios off the top of my head that would explain that. I have already listed one.
 
  • #7


Dr.D said:
I think you guys are missing the point. He said his measured result was ABOVE the theoretical value, and that is a true anomaly. I have made quite a few buckling measurements, and I have never, ever, gotten a measured result higher than the theoretical value. I think the question is an entirely valid question, and worthy of some serious consideration.

I have to suggest that you go back over your load application/load measuring situation. Are you measuring load right on the column itself, or are you measuring it on a ram that loads the column? If on a ram, could part of the load be shunted into the support by stiction?

You definitely have a strange result that ought to be explained.
If the measurement of I, L, E, or the value of K, was off by over 2%, that would, in addition to other factors previously cited, explain a mere 2% plus or minus error, wouldn't it? Please clarify your response, thanks.
 
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  • #8


Dr.D said:
I think you guys are missing the point. He said his measured result was ABOVE the theoretical value, and that is a true anomaly. I have made quite a few buckling measurements, and I have never, ever, gotten a measured result higher than the theoretical value. I think the question is an entirely valid question, and worthy of some serious consideration.

I have to suggest that you go back over your load application/load measuring situation. Are you measuring load right on the column itself, or are you measuring it on a ram that loads the column? If on a ram, could part of the load be shunted into the support by stiction?

You definitely have a strange result that ought to be explained.

I don't find it strange at all. There are many reasons (some listed) that would cause such an error.

CS
 
  • #9


In an absolutely perfect setup, that is a perfect column with perfect loading, etc. -- no imperfections in geometry, material, anything, -- then presumably the column remains in place and the mode of deformation is axial compression until such time as that becomes a higher energy state than bending would require. At that point, axial compression becomes unstable and the column buckles. This is absolutely the highest possible buckling load for the column.

The sort of idealized state postulated in the previous paragraph never exists in reality. There are always imperfections, in the material, in the geometry of the column, in the geometry of the loading. All of these things combine to give an actual buckling load that is lower than the ideal buckling load in every case. In fact, what they almost always come down to is that the really is not an instability problem at all but simply a bending problem with a very tiny initial moment arm arising only from the geometric imperfections.

The bending problem always begins with at zero force - zero deflection and rises from there. The true buckling problem shows zero deflection until the critical load is reached at which point the load begins to increase. The bending curves are always below the buckling curve.
 
  • #10


Dr.D said:
In an absolutely perfect setup, that is a perfect column with perfect loading, etc. -- no imperfections in geometry, material, anything, -- then presumably the column remains in place and the mode of deformation is axial compression until such time as that becomes a higher energy state than bending would require. At that point, axial compression becomes unstable and the column buckles. This is absolutely the highest possible buckling load for the column.

The sort of idealized state postulated in the previous paragraph never exists in reality. There are always imperfections, in the material, in the geometry of the column, in the geometry of the loading. All of these things combine to give an actual buckling load that is lower than the ideal buckling load in every case. In fact, what they almost always come down to is that the really is not an instability problem at all but simply a bending problem with a very tiny initial moment arm arising only from the geometric imperfections.

The bending problem always begins with at zero force - zero deflection and rises from there. The true buckling problem shows zero deflection until the critical load is reached at which point the load begins to increase. The bending curves are always below the buckling curve.

This presupposes that one has actually measured the column particulars exactly correct, which is almost never the case. Hence, the "theoretical" critical load may certainly be lower than the actual.

CS
 
  • #11


So Stewartcs has proposed an explanation in that the dimensions, etc. were not correctly measured, i.e. that the experiment was not correctly performed and someone made measurement errors with a micrometer. This is a plausible explanation, I suppose. I have never seen it happen, but that does not mean that it could not happen.
 
  • #12


The uncertainty in ANY of the measurements you take can do it.
 
  • #13


Also note that a radius measurement error [itex]\epsilon[/itex] would result in a buckling load error [itex]>4\epsilon[/itex] because [itex]I\propto r^4[/itex].
 

1. What is experimental buckling load?

Experimental buckling load is the load at which a structure or material experiences buckling, which is a type of failure caused by compressive stress. It is determined through physical testing and can vary depending on factors such as geometry, material properties, and boundary conditions.

2. How is experimental buckling load determined?

Experimental buckling load is determined through laboratory testing, typically using a compression testing machine. The structure or material is subjected to increasing loads until it reaches the point of buckling, and the maximum load is recorded as the experimental buckling load.

3. What factors can affect the experimental buckling load?

The experimental buckling load can be affected by various factors, such as the geometry of the structure, the material properties, the boundary conditions, and the imperfections present in the structure. These factors can impact the stability and strength of the structure, leading to variations in the experimental buckling load.

4. How is experimental buckling load used in engineering?

The experimental buckling load is an important parameter in engineering design and analysis, as it helps determine the maximum load a structure can withstand before buckling occurs. This information is used to ensure that structures are designed to withstand expected loads and to prevent failure due to buckling.

5. Can the experimental buckling load be different from the theoretical buckling load?

Yes, the experimental buckling load can be different from the theoretical buckling load, which is calculated based on mathematical equations. This is because experimental testing takes into account real-world conditions and imperfections, while theoretical calculations assume ideal conditions. However, the two values should be relatively close and can help validate the accuracy of theoretical models.

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