Calculating Euler Buckling of a Steel Rod: End Fixities & Failure Loads

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Discussion Overview

The discussion focuses on calculating the Euler buckling load of a steel rod, exploring different end fixity conditions, and examining the relationship between Euler buckling loads and true failure loads in practical applications. The scope includes theoretical calculations and conceptual explanations related to buckling behavior in structural engineering.

Discussion Character

  • Technical explanation
  • Mathematical reasoning
  • Conceptual clarification
  • Debate/contested

Main Points Raised

  • One participant presents a calculation for the Euler buckling load using the formula PE = π²EI/L, providing specific values for diameter and length, but requests verification of their result.
  • Another participant questions the units involved in the calculation and seeks clarification on the meaning of "n," which is later corrected to "π."
  • A third participant provides the general formula for critical force in buckling and outlines the effective length factor (K) for various end conditions, indicating how these affect the buckling load.
  • One participant discusses the discrepancies between Euler loads and actual buckling loads, attributing these to geometric and material imperfections, and shares personal experiences with experimental challenges in determining buckling loads.

Areas of Agreement / Disagreement

Participants express differing views on the calculation methods and the interpretation of results, particularly regarding the relationship between theoretical and actual buckling loads. The discussion remains unresolved with multiple competing perspectives on the accuracy and practical implications of Euler buckling theory.

Contextual Notes

Participants note potential limitations in the assumptions made during calculations, such as the idealized conditions of the Euler buckling model versus real-world imperfections in materials and geometries.

Who May Find This Useful

Readers interested in structural engineering, mechanics of materials, and the theoretical and practical aspects of buckling behavior in columns may find this discussion relevant.

thebest99
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a steel rod, 40mm in diameter and 1.00m long, is pinned at each end
i) calculate the euler buckling for the rod
ii) identify three other possible end fixity conditions for the rod and demonstrate how euler buckling load would be affected in each case
iii) explain the relation between the Euler Buckling load and the true failure load of a real strut

my attempt at i)

pie squared EI/L

π (40mm) ²

PE= π ² 210 x 10 cubed kN/mm²squared x 1.25 x 10 to the power of 5 mm power 4

= 259.1kN

Can some one check this thank you

And help me with question ii and iii
 
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thebest99 said:
a steel rod, 40mm in diameter and 1.00m long, is pinned at each end
i) calculate the euler buckling for the rod


pie squared EI/L

π (40mm) ²

Have you checked what the units would be for "pie squared EI/L"?
What is the meaning of "n"?
 
F=pi^2 EI/(KL)^2}

where

F = maximum or critical force (vertical load on column),
E = modulus of elasticity,
I = area moment of inertia,
L = unsupported length of column,
K = column effective length factor, whose value depends on the conditions of end support of the column, as follows.

For both ends pinned (hinged, free to rotate), K = 1.0.
For both ends fixed, K = 0.50.
For one end fixed and the other end pinned, K = 0.699...
For one end fixed and the other end free to move laterally, K = 2.0.

KL is the effective length of the column.

from http://en.wikipedia.org/wiki/Buckling
 
sorry that n is meant to be pie
 
"π (40mm) ²" gives you 4 x the cross-sectional area. is that what you meant?
For part iii, the main reasons for the differences between Euler loads and actual buckling loads is said to be a combination of geometric and material imperfections. But my personal view is that the buckling load is quite difficult to obtain experimentally. My understanding is that if a loaded strut is practically straight, and under load, you perturb it sideways, then buckling load has been reached if it remains in the perturbed position. When I have done experiments on timber struts, that definition never quite satisfied me, as it was hard to determine the accuracy with which it was obtained. The struts were never quite so well-behaved.
 
thank you pongo this is what i worked out
 

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