Experimental Critical Buckling Load

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SUMMARY

The discussion focuses on determining the experimental critical buckling load of a pinned-ended strut, comparing predicted values from Euler buckling and Perry Robertson with experimental results. Participants emphasize that the critical buckling load is identified at the "knee" of the load versus axial displacement curve, rather than the highest recorded load. Accurate identification of the "knee" is crucial, especially when samples do not exhibit a clear transition. Additional information about material properties and specimen geometry is necessary for precise analysis.

PREREQUISITES
  • Understanding of Euler buckling theory
  • Familiarity with Perry Robertson's method for buckling analysis
  • Knowledge of axial load application and displacement measurement
  • Experience with data analysis and curve plotting techniques
NEXT STEPS
  • Research methods for accurately identifying the "knee" in load-displacement curves
  • Study the effects of material properties on buckling behavior
  • Learn about experimental setups for buckling tests
  • Explore advanced data analysis techniques for minimizing experimental errors
USEFUL FOR

Structural engineers, materials scientists, and researchers involved in experimental mechanics and buckling analysis will benefit from this discussion.

KevCah
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Hi guys,

I was wondering could I get some help with determining the experimental critical buckling load of a pinned ended strut. I am hoping to compare predicted values from Euler buckling and Perry Robertson to experimental values. I have carried out a experiment where by I applied a axial load to the strut and recorded both the horizontal and vertical displacement. From this data can I apply a formula to give me the critical buckling load? Or is the critical buckling load simply the highest value recorded in the experiment?

Thanks for any help!
 
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Assuming that your strut was initially straight (so that it would actually buckle rather than simply bend), then make a plot of load as a function of axial displacement. You should see a pronounced "knee" in the curve. That is the buckling load. It is not the highest load recorded because most post-buckled columns continue to support the load and the load rises slowly.
 
Thanks for the reply,

There is no clearly defined "knee" in some of my samples. Is there anymore accurate way to determine the "knee" rather then doing it by eye? I am just trying to keep my experimental errors to a minimum.

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KevCah said:
Thanks for the reply,

There is no clearly defined "knee" in some of my samples. Is there anymore accurate way to determine the "knee" rather then doing it by eye? I am just trying to keep my experimental errors to a minimum.

View attachment 77667
If you look at the test results for Sample 1, I would say the 'knee' is clearly defined when the test load is approx. 350-360 Newtons. Where the applied load is relatively constant, the test piece undergoes a measurable change in deflection, which suggests that some sort of inelastic behavior is occurring. The other two samples do not appear to exhibit the same behavior.

Of course, a lot of information about the test pieces and the test set up have not been disclosed.
 
What is the material and what is your geometry (length, width, etc. for the test specimens)?
Did your experiments result in a permanent set, or were they fully elastic? (Buckling is an elastic phenomenon; plastic deformation puts an end to all questions of buckling.)

I don't think we can help you very much without this data.
 

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