Buckling length of column

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SUMMARY

The discussion focuses on the buckling length of a column under specific boundary conditions, including v(x=0)=0, v(x=L)=0, v'(x=0)=θB, and v'(x=L)=0. The user seeks assistance in expressing the governing equation in terms of ωL. The boundary conditions lead to a system of equations involving constants c1 and c2, which are derived from the conditions at both ends of the column. The equations incorporate parameters such as EI (flexural rigidity) and the moment MB, highlighting the relationship between the column's deflection and its buckling behavior.

PREREQUISITES
  • Understanding of differential equations and boundary value problems.
  • Familiarity with beam theory and Euler-Bernoulli beam equations.
  • Knowledge of flexural rigidity (EI) and its significance in structural analysis.
  • Basic concepts of vibration analysis, specifically relating to natural frequencies (ω).
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  • Study the derivation of the Euler-Bernoulli beam equation in detail.
  • Learn about solving boundary value problems using methods such as separation of variables.
  • Research the implications of flexural rigidity on buckling behavior in structural engineering.
  • Explore vibration analysis techniques for beams, focusing on natural frequency calculations.
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Structural engineers, mechanical engineers, and students studying mechanics of materials who are involved in analyzing column stability and buckling phenomena.

rc2008
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Homework Statement
I was given this question to find the buckling length of the non-sway frame of column AB.
Relevant Equations
The general equation is v" +## \omega\##^2 v = MB/EI + Vx/EI,
Taking B as origin, the boundary condition provided was ##v(x=0)= 0 , v(x=L)=0 , v'(x=0)= \theta B##
##v'(x=L)=0## , and also ##v'' (x=0) = M_B/ EI##

However, I had problem of expressing the equation in terms of ## \omega L##
Can anyone help ?

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## BC1: At x=0x = 0x=0, v=0v = 0v=0: c2+θBL=0c_2 + \frac{\theta_B}{L} = 0c2+LθB=0• BC2: At x=Lx = Lx=L, v=0v = 0v=0: c1sin⁡(ωL)+c2cos⁡(ωL)+VEIL+θBL=0c_1 \sin(\omega L) + c_2 \cos(\omega L) + \frac{V}{EI} L + \frac{\theta_B}{L} = 0c1sin(ωL)+c2cos(ωL)+EIVL+LθB=0• BC3: At x=0x = 0x=0, v′=θBv' = \theta_Bv′=θB: c1ω+VEI=θBc_1 \omega + \frac{V}{EI} = \theta_Bc1ω+EIV=θB• BC4: At x=Lx = Lx=L, v′=0v' = 0v′=0: c1ωcos⁡(ωL)−c2ωsin⁡(ωL)+VEI=0c_1 \omega \cos(\omega L) - c_2 \omega \sin(\omega L) + \frac{V}{EI} = 0c1ωcos(ωL)−c2ωsin(ωL)+EIV=0• BC5: At x=0x = 0x=0, Moment MB=EIv′′M_B = EI v''MB=EIv′′: −c2ω2=2EILθB-c_2 \omega^2 = \frac{2EI}{L} \theta_B−c2ω2=L2EθB##
 

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