Braced column under compressive load

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SUMMARY

The discussion focuses on calculating the critical load for a braced column under compressive load using the formula P = EI π² / Leff². Key values identified include Ixx = 240.81 x 10^6 mm^4, Iyy = 71.9 x 10^6 mm^4, and an area A = 9600 mm². The effective lengths for the x-axis and y-axis are determined to be 4.2 m and 10 m, respectively, with the effective length factor k set to 1. The discussion emphasizes the importance of using the larger slenderness ratio to identify the weaker axis for buckling analysis.

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  • Knowledge of moment of inertia calculations
  • Experience with slenderness ratio concepts
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Structural engineers, civil engineering students, and professionals involved in the design and analysis of columns under compressive loads will benefit from this discussion.

sukibelle
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Homework Statement



Homework Equations



P = EI pi^2 / Leff radius of gyration: SQRT (I/A), slenderness ratio: Leff/r

The Attempt at a Solution



So I've found Ixx = 240.81 x 10^6 mm^4, Iyy = 71.9 x 10^6 A = 9600 finding the radiuses of gyration rx = 158.38, ry = 86.54
effective length of x-axis : (one end pinned, I'm assuming the buckling = fixeed and do i use the longer length?) 6*0.7 = 4.2
efective length of y: 10*1 (both ends pinned)
I'm not sure about the effective length part, I know I'm meant to find the larger slenderness ratio (which identifies the weaker axis) and then plug that into the P = EI pi^2 / Leff . I don't know how to address a column supported in this way. do I average the lengths or something?
 
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You should use k = 1 as the effective length factor in both cases, where L = 10 for major axis and L = 6 for minor axis. This is due to member rotation at the braced support at the buckling mode. See which controls. Also check your buckling formula the L should be squared, Pcr = pi^2 EI/L^2
 

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