Calculating Euler Buckling of Open I Beam in 3 Point Bending

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SUMMARY

The discussion focuses on calculating Euler buckling for an open I beam subjected to three-point bending with a point load. The critical buckling load is defined by the formula Pcr = (π²)EI/L, applicable for columns with pinned ends. The conversation emphasizes the need to consider both bending stresses and axial compressive stresses, governed by relevant Steel Codes. The formula f_a/F_a + f_b/F_b ≤ 1.0 is introduced to ensure that the actual stresses do not exceed allowable limits, factoring in safety considerations.

PREREQUISITES
  • Understanding of Euler's buckling theory
  • Familiarity with I beam structural properties
  • Knowledge of bending stress and axial stress calculations
  • Awareness of relevant Steel Codes and design standards
NEXT STEPS
  • Study the application of the Euler buckling formula for different beam configurations
  • Learn about lateral-torsional buckling in I beams
  • Research the latest revisions of relevant Steel Codes for beam-column design
  • Explore software tools for structural analysis, such as SAP2000 or ANSYS
USEFUL FOR

Civil engineers, structural designers, and students studying mechanics of materials who are involved in the design and analysis of structural beams under various loading conditions.

THE 1
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Homework Statement



I want to find the euler buckling for a open I beam( middle section like a box) that is subjected to three point bending with a point load on top.
I am not so interest in a solution but explanation on how this could be worked out using the euler equation for buckling.



Homework Equations


Pcr=(PI^2)EI/L I am pretty sure this is for a column with pinned ends but don't know how to work out one for an i beam in 3 point bending


The Attempt at a Solution


Don't want a solution can put numbers in myself
 
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THE 1 said:

Homework Statement



I want to find the euler buckling for a open I beam( middle section like a box) that is subjected to three point bending with a point load on top.
I am not so interest in a solution but explanation on how this could be worked out using the euler equation for buckling.



Homework Equations


Pcr=(PI^2)EI/L I am pretty sure this is for a column with pinned ends but don't know how to work out one for an i beam in 3 point bending


The Attempt at a Solution


Don't want a solution can put numbers in myself
If you are talking about an I beam subject to both bending stresses and axial compressive stresses, then the beam-column design would be governed by the applicable Steel Code. Now mind you I haven't kept up with the latest Code revisions, but generally speaking, especially when the actual axial stress is small compared to the allowable axial stress, stresses would have to satisfy the following formula:
f_a/F_a + f_b/F_b <= 1.0 , where
f_a = actual design axial compressive stress
F_a = Allowable axial compressive stress as if there were no bending (this is generally the Euler buckling stress pi^2EI/KL^2(A) for K=1, with appropriate safety factors)
f_b = actual design compressive bending stress
F_b = Allowable compressive bending stress as if there were no axial load (this allowable stress must take into account lateral torsional buckling of the flange due to the compressive bending stresses, with appropriate safety factors).
 

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